Location via proxy:   [ UP ]  
[Report a bug]   [Manage cookies]                
SlideShare a Scribd company logo
1 Copyright © 2019 by ASME
Presented Not Published June 29,
2017
Power & Energy Conference
Charlotte, North Carolina
Updated expanded July 26, 2019
Power Energy “2017-3191”
Analysis of Steam Zoning With Exhaust – Smoke Stack and Water Swirled Into Gas
Turbine Technology – Draft – Work in Progress
Leonard M. Andersen
Water Swirled Into Gas Turbine Tech
Caller Box 1529
New York, New York 10116, USA
914-237-7689
ABSTRACT
Two and a half years ago I prepared a paper “Power
Energy “2017-3191” -Analysis of Steam Zoning With
Exhaust – Smoke Stack and Water Swirled Into Gas
Turbine Technology and presented. It was not
published as part of the proceedings. The New
technology covered in PUB. APP. NO. 20170306843
“METHOD AND APPARATUS FOR INCREASING
USEFUL ENERGY/THRUST OF A GAS TURBINE
ENGINE BY ONE OR MORE ROTATING FLUID
MOVING (AGITATOR) PIECES DUE TO
FORMATION OF A DEFINED STEAM REGION”
Filed: February 27, 2017 published October 26,
2017 first action March 4, 2019 not part of the
presentation due to a request by the US
Government. The new technology has been
developed with water into a flow of hot gas in a
swirling pattern most recently with a focus on internal
combustion engines , fired boiler stacks and, water
swirled into gas turbines combined cycles for more
fuel efficiency. Beyond more fuel efficiency there is
pollution control of PM 2.5 and PM 10 particulate in
coal firing etc.. In electrical generation the latest
advance is to have a fluid mover of a paddle nature
moving a mass – volume of optimally positioned
spaced sized water droplets in hot gas outward from a
centerline into a tire / donut shaped volume space
where said goes to steam / pressurization. Such
pressurization happens making an extractive turbine
turn which is connected to an electrical generator. In
fired boilers and internal combustion engines the shaft
of the fluid mover would be vertical and the extractive
turbine would normally be horizontal. The horizontal
extractive turbine would have water drops and
combustion gas leaving at about 120 C with less
particulates exiting. The work in new combined cycle
gas turbines prior to this is my two patents is to at the
end of the power turbine through blades and/or a
mechanism to put water droplets into the hot thrust
gas of 350 – 500 C going to steam in concentrated
volume. Said volume goes in a steaming chamber. The
energy is converted from heat to steam pressurized
increase in volume. Increase in volume in the
steaming chamber acts on an extractive turbine
connected to an electrical generator. This could
benefit from aforementioned. The tire / donut shape
would be vertical. The maintenance and operation of
this is a fast moving subject with in exhaust – stack
gas plus 5 % per unit fuel and in the case of water
swirled into gas turbines 15 – 25%. The motivation
for the presentation is to get discussion going. A
speaker on coal fired with experience of use and,
second on internal combustion engines automotive /
ship propulsion and third on new combined cycle gas
turbine and a fourth on aircraft propulsion with the
new tech was sought. At this time there is one speaker.
This is a start !
NOMENCLATURE
2 Copyright © 2019 by ASME
BTU - British thermal unit
GTE - Gas Turbine Unit
Meg - Million Watt
Mock - Mock At sea level, mock 1 is 761 mph
Mph - Miles per hour
MW - Megawatt (MW) = 1,000 kilowatts
Rpm - Revolutions per minute
π - 3.14159
KEYWORDS – Natural Gas, Electrical Power
Generation , Electrical Generation , Fuel Efficiency,
Pollution , Boilers , Internal Combustion Engines,
Gas Turbine , Aircraft , Jet
Acknowledgments
Edward J. Ellis | Leason Ellis – Patent Attorney
914.821.9071 ellis@leasonellis.com
One Barker Avenue, Fifth Floor
White Plains, New York 10601-1526
Ones Sharing Knowledge With me at ASME
( www.asme.org ) and WPC “World Petroleum
Congress” ( www.world-petroleum.org ) events and
at www.asme.org online inter-activeness etc. .
REFERENCES
United States Patents 8,671,696 , 9,376,933 and one
pending PUB. APP. NO. 20170306843 “METHOD
AND APPARATUS FOR INCREASING USEFUL
ENERGY/THRUST OF A GAS TURBINE
ENGINE BY ONE OR MORE ROTATING
FLUID MOVING (AGITATOR) PIECES DUE
TO FORMATION OF A DEFINED STEAM
REGION” Len Andersen
Gas Turbine Engineering Handbook
Author(s): Meherwan P. Boyce 2011
INTRODUCTION
The presenter started career with a coal fired air
pollution project. At that time a third of a power plant
cost was scrubber and resulting sludge cost. My
technology is to a hot gas stream ( exhaust / stack /
thrust ) as indicated in my first patents ( water droplets
are added in optimal spacing positions with swirling
around main shaft ) . Said mass in the latest patent is
moved radially from center line to form a tire /donut
where the water form steam ( pressure energy ) . Said
moves extractive turbines or makes airplanes go.
In the case of steam move to sides the hot gas at a
higher than current off boiler tubes ( ~ 200 C ) and
have an optimally water droplets in hot gas mass
moved from center into a steam zone – space of donut
/ tire shape. Go to steam and move an extractive
turbine connected to an electrical generator. A parallel
is envisioned would be for internal combustion
engines. The area of gas turbines is more addressed
with many issues resolved. The concern we have is
having such happen more cost effectively. My
presentation is an answer that has been there since the
beginning; add water without wear on the internals of
the machine. In total it is the get the benefit in boilers
, internal combustion engines , and thrust per unit fuel
as with water being ingested into blower of furnace,
air intake of an internal combustion engine, water into
compressor and/or water injected into combustor of a
gas turbine engine with less wear .
WATER ADDED TO HOT STACK GAS -
EXHAUST - - TURBINE ENGINE THRUST GAS
EFFECTS ON PERFORMANCE gives a water
droplet to steam volume increase which has a boost
of performance per unit fuel. Note following
Figure One - New Tech Hot Gas To Electricity ,
Figure Two – Hot Stack- Exhaust Patent PUB.
APP. NO. 20170306843 particle – Pollution
Reduction , Figure Three – Latest Patent for Use
With Gas Turbines , Figures Four - Gas Turbine
with Rain Ingestion Sectioned , Figure Five -
Three Sections of Gas Turbine with Rain (
precipitation ) Drops to Stream Thrust
Enhancement , Figure Six - The Water Swirled
Into Gas Turbine Engine Shown Indicating the
Shifted of Rapid Near Instantaneous Water
Droplet to Steam Formation from Combustion
Section to After Turbine Section and Figure Seven
- Combines Gas Turbine Issued Patents Sketch of
3 Copyright © 2019 by ASME
a Steam Expansion Chamber
www.gasturbineandersen.com . All Figures are at
end of the Paper. In the case of gas turbines a
swirling mass of water droplets.
The way in which this is achieved is one or more of
the following
1. Put water and/or volatile through the main shaft of
a gas turbine and flow water of from turbine blades
/ end of main shaft.
2. And/or said liquid flowing out of a “stator” hitting
“pins” rotating on the main shaft creating small
droplets.
3. Beyond main shaft a rotating unit that is powered
by thrust gas flow or other way with said liquid
flowing through it and out of through flow points.
Such systems can be applied to fired systems ( boilers
etc. ) and internal combustion engines.
What has been told me is very positive. First
thermodynamic analysis is ANNEX A. My analysis
follows !
ANALYSIS
The analysis of the patent pending is the next
paper / presentation. My background is an engineer
who has had an electrical generation focus
interviewing for jobs in field , hearing presentation
about and having operational etc. with diesel
generators. This is a New Tech Combined Cycle Gas
Turbines (CCGT) technology. My focus will be
analyze / explain the technology and in the electrical
power grid context explore fits, factors and
extrapolations. Made presentation of my technology
to a large gas turbine manufacturer and got where is
the analysis of gas turbine first two patents on claims
of heard by me of
1. Twelve % gas , fourteen % liquid up in fuel to
electricity or mechanical energy output compared to
combined cycle now in use !
2. Low capital cost combined cycle units, smaller and
in greater numbers.
3. The efficiency of gas turbine electrical generator
units 1 to 400 MW is nearly the same which would
greatly reduce electrical distribution losses. Much
lower startup shut down cost !
Before latest Patent Pending ! The analysis of the
aforementioned is not easily done and has commercial
interest. Note end of paper resume ANNEX B. As an
engineer member of IGTI with plus twenty years
experience having since June 2009 focused on gas
turbine combined cycle I left quietly with, “I will get
back to you!”. What is Water Swirled Into Gas
Turbine Technology ?
It is New Combine Cycle US Patents 8,671,696 &
9,376,933 & PUB. APP. NO. 20170306843
“METHOD AND APPARATUS FOR
INCREASING USEFUL ENERGY/THRUST OF
A GAS TURBINE ENGINE BY ONE OR MORE
ROTATING FLUID MOVING (AGITATOR)
PIECES DUE TO FORMATION OFA DEFINED
STEAM REGION” published October 26, 2017 !
The Technology is to have water droplets into the hot
end part of the gas turbine with the droplets of water
traveling in a curved pattern after the combustion
section.
THERMODYNAMIC ANALYSIS
First thermodynamic analysis is to determine if said
water introduced into a gas turbine after the
combustor in the turbine and/or end of turbine and/or
in the nozzle or connector to extractive turbine
“section” yields more thrust energy – electrical energy
per unit fuel. Said preliminary analysis is positive and
ANNEX A. It says water to steam would increase
thrust. There is noted in a Gas Turbine Handbook the
adding of water offshore as spray to the connector
between the turbine and the extractive turbine is
beneficial.
A - SIZE OF DROPS
The second analysis is mechanical – fluid dynamics
of water flow as described in patent.
A. Size of drops -
1. Size of Water Droplets Created by Nozzle
Parameters &/or Impingement Design Detail
4 Copyright © 2019 by ASME
&/or rotational design
a. http://www.efm.leeds.ac.uk/CIVE/FluidsLe
vel1/Unit03/T6.html - An Introduction To Fluid
Mechanics : CIVE1400 SCHOOL OF CIVIL
ENGINEERING Leeds University UK Pelton
wheel blade
Application of the Momentum Equation
In this section we will consider the following
examples:
1. Force due to the flow of fluid round a pipe
bend.
2. Force on a nozzle at the outlet of a pipe.
3. Impact of a jet on a plane surface.
4. Force due to flow round a curved vane.
5. A curved vane on a Pelton wheel turbine.
“The above analysis of impact of jets on
vanes can be extended and applied to
analysis of pins of US Patent 9,376,933 “
6. Impact of a jet on an angled plane surface
Papers ANNEX C - Size of Droplets Etc.
B. SPACING OF DROPLETS
Spacing of droplets – Evenly spaced across the
cross section is a design issue !
C – INTERACTIVENESS OF VAPORIZATION /
TEMPERATURE GAS – LIQUID / COOLING OF
MASS / TURBULENCE
Pertaining to Inter-activeness of vaporization visa vi
temperature gas - liquid visa vi cooling of mass visa
vi turbulence
Found International Journal of Heat and Mass
Transfer. April 2016, Experimental investigation of
consecutive water droplets falling down through
high-temperature gas zone Authors R.S. Volkov, G.V.
Kuznetsov, J.C. Legros, P.A. Strizhak saying
exploding water droplet with 830 degrees Celsius.
Friend asked, “Where is a start point beyond add
heat gets steam analysis of water swirled into gas
turbine technology?” ! Approximation of Water
Droplets Speed With Get Turbine ( Jet Engine ) J47
36000 Produced 1949 to 1956 8000 RPM
Speed of Drop = ( Rotational Rate RPM ) ( π D ) =
X
Part of assembly with main shaft centerlines line of
rotation around O.5 foot from said centerline droplet
origination
X = ( 8000 ) ( 3.14 ) ( 1.0 )
X = 25120 feet / minute
Droplet Speed Out of nozzle = ( 25120 feet / minute
) × ( 60 minutes / hour ) ÷ 5280 feet
Droplet Speed Out of nozzle =~ 280 mph ( miles per
hour )
Droplet Speed As A Point On A Turbine Blade Six
Inches from centerline of main shaft
Thrust gas at 1.3 mock =1100 mph
My view of start point is water droplet(s) circular
motion around main shaft at ~280 mph with mock
one point three thrust gas parallel to main shaft
temperature from 600–910 degrees Celsius to 150
steaming phenomena ! In larger electrical power
units ( Siemens SGT – 500 / 19.1 MW Exhaust 370
degrees Celsius.
The technology is to put water in droplet form
into the hot end of the gas turbine. The “plumbing
etc.” of water to droplet form is covered in three
patents as concept. The design details lend
themselves to models and/or experimentation. The
experimentation could be
1. Buying or Designing / Manufacture Rotary
Spray Nozzle and installing at the hot end of
a gas turbine engine.
2. Operate and take the data.
3. Analyze the data and design better
equipment!
5 Copyright © 2019 by ASME
Alternatively or as parallel effort hand calculation or
model. From there finite element analysis with
factors of Size of Water Droplets Created by Nozzle
Parameters &/or Impingement Design Detail &/or
rotational design, Spacing of droplets, Inter-
activeness of vaporization visa vi temperature gas -
liquid visa vi cooling of mass visa vi turbulence, etc.
Work in progress !
There are start points. The two that appear to
be most productive are rain ( precipitation ) into
the combustor in a uniform across the cross
section way which is covered for gas turbine
aircraft propulsion and for electric power
combustor sections of gas turbines. The other is
extensive study / modeling of the combustors.
Rain ( precipitation ) comes in a range of droplet
sizes , intensity and by the action of compressor
part of the gas turbine engine made uniform and
smaller diameter.
Rain ( precipitation ) ingestion into gas turbine
engines go back 120 years. It rains and better power
output.
It is covered with papers , models , thesis ,
reports -
“Parametric Analysis of the Exergoeconomic
Operation Costs, Environmental and Human Toxicity
Indexes of the MF501F3 Gas Turbine” Entropy. Aug
2016, Vol. 18 Issue 8, p1-26. 26p.
Development and Integration of rain Ingestion
Effects in Engine Performance Simulations, Authors:
Roumeliotis, I. , Journal of Engineering for Gas
Turbines & Power, Apr 2015, Vol. 137 Issue 4
The thesis is
WATER INGESTION EFFECTS ON GAS
TURBINE ENGINE
PERFORMANCE Supervisor: P. Pilidis
October
2008 https://core.ac.uk/download/pdf/138838.pdf
A report is
NORTH ATLANTIC TREATY ORGANISATION ,
RESEARCH AND
TECHNOLOGYORGANISATION RTO
TECHNICAL REPORT TR-AVT-036 2007
Performance Prediction and Simulation of Gas
Turbine Engine Operation for Aircraft , Marine ,
Vehicular , and Power Generation.
START POINT TWO COMBUSTOR MODEL
PATENTS AND PAPERS
Gas turbine engine and corresponding operating
method
EP 2476880 A1
A gas turbine engine has in flow series: a compressor
section, a combustor, and a turbine section. The
engine further has a steam generator, and a water and
steam delivery system. During an engine start-up
period, the delivery system delivers liquid water to
the combustor and mixes the delivered water in its
liquid state with working gas in the combustor. After
the start-up period, the delivery system accepts
steam from the steam generator, delivers the steam to
the combustor and mixes the delivered steam in its
gaseous state with the working gas in the combustor.
Papers
ANNEX D – Papers on Combustion Models
OTHER FACTORS IN THE ANANLYSIS
1. Rotational speed and flow of thrust gas
Siemens SGT-500
Turbine speed 3,450 RPM
Mitsubishi M501F
Turbine speed 3,600 RPM
US Military J47 36000 Produced 8000 rpm
747 Gas Turbine JT9D exhaust speed 811 mph
TRADE OFF’S – OPTIMIZATIONS
Water Pressure Into System
High
1. Mist –Diesel Injector Analysis
2. Cost Higher Beyond practicality
6 Copyright © 2019 by ASME
3. Possibly used on aircraft after burner
applications
4. Seal Concerns
5. Impinging patent possible fit
Low
1. Exploding water drops 1200 degrees Celsius
at less than 5 mph mist maker ?
2. “Only” way with seals with rotation through
shaft ( main shaft ) / pressure happening
through main shaft approximately 30 psi
cooling air for turbine blades and lubricating
oil.
Efficiency – Weight – Uses - Combo
1. Impinging on pins – lighter aircraft / less
expensive
2. Through main shaft aircraft / power
generation
3. After main shaft heavier aircraft / larger
power generation
4. Combo’s of the Above ?
Power Generation Grid context explore fits , factors
and extrapolations
 Grid modification – Currently 500 Meg units
to “convenient” 5 Meg units ?
 Change plans with more local generation use.
The steam engine use prior to grid analogy
 Trade offs Electrical Transmission loss
against gas line installation – delivery cost
 Cheaper electricity
 Extrapolation one Meg power and up future.
Heard it is happening !
COMMENTS AND REPLIES -– ANNEX E
CONCLUSIONS
A) Models using finite element analysis
available for start point water droplet evenly
distributed with different size etc.
B) Using engineering and adequate and adopting
model(s) the elements of the patents (
mechanical pieces ) an optimum space round
center line of the main shaft with a thickness
having an even water droplet density could
be achieved.
C) The potential of the invention ( three patents
) water swirled into gas turbine technology
could be enhanced with analysis.
SUMMARY - A start of the analysis of water swirled
into gas turbine technology is presented .
PRESENTER
Leonard M. Andersen Engineer
len@lenandersen.com ( HP SecureMail voltage
connected ) POB 1529 New York, New York 10116 (
+$1299 per year Caller Box ) 914-536-7101 Cell
Phone / 914-237-7689 Home / 800-428-4801
www.gasturbineandersen.com
www.lenandersen.com
7 Copyright © 2019 by ASME
Figure One - New Tech Hot Gas To Electricity
8 Copyright © 2019 by ASME
9 Copyright © 2019 by ASME
10 Copyright © 2019 by ASME
11 Copyright © 2019 by ASME
12 Copyright © 2019 by ASME
13 Copyright © 2019 by ASME
Figure Seven - Combines Gas Turbine Issued
Patents Sketch of a Steam Expansion Chamber
www.gasturbineandersen.com
14 Copyright © 2019 by ASME
ANNEX A
The basis of the analysis is one unit of fuel per one unit of water on weight. * 19,000 BTU’s per
pound of fuel ( Jet A ) * It takes 0.24 BTU’s to heat one pound air one degree Fahrenheit * 970
BTU’s per pound of water to create steam * Steam from one pound of water creates 27 cubic
feet of one atmosphere steam * Air Fuel Ratio ( AFR ) is 150 to 1 * Thrust gas enters system at
1200 degrees Fahrenheit * Thrust gas volume per unit volume is directly proportional to gas
volume which equals cooling effect of vaporization shrinkage and made larger by steam
increase volume It follows water thrust gas ratio 150 to one therefore 970 BTU – Pound / 150
Pound = 6.4 BTU / Pound And 0.24 BTU per degree temperature change therefore 27 degree F
temperature drop , volume decrease of 1-2 percent.
Steam volume as partial of thrust per pound fuel equals 19000 / 970 = 18.5 pounds steam 18.5
pound x 28.8 cubic foot / pound = 500 cubic feet Total thrust gas volume = 150 pounds / 0.075
pound-cubic foot 2000.
Net Thrust Gas Volume Increase about = 25-2 = 23 %
Answer yes as preliminary analysis
ANNEX B
Resume of Presenter for Leonard M. Andersen – Gas Turbine Engineer
len@lenandersen.com ( HP SecureMail voltage connected ) water-gas-
turbine@lenandersen.com
914-536-7101 Cell Phone / 914-237-7689 Home / 800-428-4801
POB 1529 New York , New York 10116 ( +$1299 per year Caller Box / Most Secure Service At
Large Post Office USA ) / 46 Alexander Av , Yonkers NY
www.gasturbineandersen.com
15 Copyright © 2019 by ASME
www.lenandersen.com
Professional Experience
Ten years focus on Water Swirled into In Gas Turbine Technology work including
attending IGTI ASME events , making technical presentations inTexas / Kingdom
of Saudi Arabia / Qatar / Russia. The work has resulted in two patents issued
and one patent pending . I attended at the Turbo Expo Pheonix 2019 / OSLO
2018 and attended many ASME Gas Turbine Technical Chapter Meetings
www.asmegttc.org . I attended day long work shops “Design, Operation and
Maintenance Considerations for Cogeneration and Combined Cycle Systems” at the Turbo
Expo / Power Energy event 2017 , at the Turbo Expo Montreal in June 2015 took a
short course “Gas Turbine Aerothermodynamics and Performance Calculations”
and at Gas Turbine Users Symposium (GTUS) with Texas A&M’s Turbo
machinery Symposium, 2010 Houston attended short course “Combined Cycle
and Cogeneration Power Plants”!
Welding Inspection Engineering New York , Connecticut , Ohio August 2014 to Present
 Journalist World Petroleum Congress Istanbul ( www.22wpc.com ) July 2017
Welding Inspector CWI / Construction Project Manager / Engineer Employed October
2000 to May 2014 New York City Department of Transportation - Division of Bridges.
Spoke Chinese every day at work.
Worked in Spanish language in Mexico, Spain etc., and Arabic in the Kingdom of Saudi
Arabia for near a year, Norwegian in Norway etc. for about six months and worked in the
Russian language. In journalism I covered the World Petroleum Congress www.world-
petroleum.org events 2002 Rio de Janeiro Brazil , 2005 Johannesburg South Africa ,
2008 Madrid Spain , 2011 Doha Qatar and Moscow Russia 2014 as an accredited
journalist. Fellow journalist mentioned at the last one, "You know everyone". Inventing
one patent issued in Lubricating / Motor Oil , two and pending in Power Generation / Gas
Turbine Technology which I wrote. Pursuant to such I attended STLE ( www.stle.org )
events and International Gas Turbine Institute (IGTI) ASME events.
Education –
16 Copyright © 2019 by ASME
 Registered Representative www.sec.gov ( Stock Broker ) Securities Training Corporation
New York , New York
 BSChE Chemical Engineering Degree, University of Arizona, Tucson, Arizona
Published Works – Welding Journal - one and Society of Petroleum Engineers 30994 &
Patents
 “METHOD AND APPARATUS FOR INCREASING USEFUL ENERGY/THRUST OF A
GAS TURBINE ENGINE BY ONE OR MORE ROTATING FLUID MOVING
(AGITATOR) PIECES DUE TO FORMATION OF A DEFINED STEAM REGION” ,
published October 26, 2017
 Gas Turbine Thrust Fuel Efficiency Enhancement System Water (Volatile)
Introduction Arrangement Method and Means 9,376,933
 METHOD AND APPARATUS FOR INCREASING THRUST OR OTHER
USEFUL ENERGY OUTPUT OF A DEVICE WITH A ROTATING ELEMENT
8,671,696
 Lubricating/sealing oil-based composition and method of manufacture thereof -
6,358,891
Additionally Five patents in welding , two in petroleum extraction
Active Memberships in Engineering and Technical Societies
International Gas Turbine Institute ( IGTI ) events – Presentation at Power Energy 2017 and
attending week long events 2010 / 2015 / 2017 / 2018 ! The Metropolitan Section of the
American Society of Mechanical Engineers (ASME) in New York City attends meetings as a
member metsection@asme.org / www.asmemetsection.org
Society of Tribologists and Lubrication Engineers www.stle.org & SPE & AIChE & ASCE &
AWS
ANNEX C
Size of Droplets Etc.
Droplet impact cavity film thickness measurements versus time after drop impact and cavity
radius for thin static residual liquid layer thicknesses.
17 Copyright © 2019 by ASME
By: Kuhlman, John M.; Hillen, Nicholas L. Experimental Thermal & Fluid Science. Oct 2016,
Subjects: Liquid films; Thickness measurement; Reynolds number; Heat flux; Drops
Optimization study on pin tip diameter of an impact-pin nozzle at high pressure ratio.
By: Kumar, C.; Lee, Kwon; Park, Tae; Cha, Bong; Kim, Heuy. Journal of Mechanical Science
& Technology. Sep 2016, Subjects: Gas turbines; MATHEMATICAL models; High pressure
(Technology); Compressors; Jet impingement; Pump and compressor manufacturing; Industrial
Machinery and Equipment Merchant Wholesalers; Air and Gas Compressor Manufacturing;
Turbine and Turbine Generator Set Units Manufacturing; All Other Plastics Product
Manufacturing; All other plastic product manufacturing; Nozzles
Numerical and experimental investigation on droplet dynamics and dispersion of a jet engine
injector.
By: Keller, J.; Gebretsadik, M.; Habisreuther, P.; Turrini, F.; Zarzalis, N.; Trimis, D.
International Journal of Multiphase Flow. Oct 2015, Subjects: Numerical analysis; Hypodermic
jet injectors; Combustion chambers; Hydraulic turbines; Liquid fuels; Solid Waste Combustors
and Incinerators; Waste treatment and disposal; Conventional oil and gas extraction; Turbine
and Turbine Generator Set Units Manufacturing
Three-Dimensional Mass Fraction Distribution of a Spray Measured by X-Ray Computed
Tomography.
By: Coletti, Filippo; Benson, Michael J.; Sagues, Alexander L.; Miller, Benjamin H.; Fahrig,
Rebecca; Eaton, John K. Journal of Engineering for Gas Turbines & Power. May2014
Subjects: RESEARCH; X-ray computed microtomography; Other Basic Inorganic Chemical
Manufacturing; All other basic inorganic chemical manufacturing; Atomization; Spray
combustion; Pressure; Iodine
"Numerical Analysis on Spray Cooling of Gas Turbine Exhaust Gas" By: HAN, D.
International Journal of Transport Phenomena. 2014, Subjects: Spray cooling; Gas turbines --
Exhaust gas; Mass transfer; Turbulence -- Mathematical models; Numerical analysis; Particle
size distribution
ANNEX D
Papers on Combustion Models
Influence of Main Swirler Vane Angle on the Ignition Performance of TeLESS-II Combustor
Bo Wang, Chi Zhang, Yuzhen Lin, Xin Hui and Jibao Li
Bo Wang Eng. Gas Turbines Power 139(1), 011501 (Aug 16, 2016)
18 Copyright © 2019 by ASME
Unsteady Computational Fluid Dynamics Investigation of Effusion Cooling Process in a Lean
Burn Aero-Engine Combustor
L. Mazzei, A. Picchi, A. Andreini, B. Facchini and I. Vitale
Eng. Gas Turbines Power 139(1), 011502 (Aug 16, 2016)
Detached-Eddy Simulations (DES) of a complex swirl stabilized gas turbine model combustor.
By: Ali, Ahlem Ben Sik; Kriaa, Wassim; Mhiri, Hatem; Bournot, Philippe. International Journal
of Energy & Environment. 2016, Subjects: GAS turbines; COMBUSTION chambers;
SWIRLING flow; SHEARING force; TURBULENCE; Conventional oil and gas extraction;
Waste treatment and disposal; Solid Waste Combustors and Incinerators; Turbine and Turbine
Generator Set Units Manufacturing
Numerical Analysis of Turbulent Combustion in a Model Swirl Gas Turbine Combustor. By:
Benim, Ali Cemal; Iqbal, Sohail; Joos, Franz; Wiedermann, Alexander “Journal of
Combustion” 9/15/2016,
Subjects: COMBUSTION gases -- Analysis; GAS turbines -- Combustion chambers;
NUMERICAL analysis; NATURAL gas -- Measurement; REYNOLDS stress; FLUE gases --
Measurement; SYNTHESIS gas; Natural Gas Distribution
ANNEX E
Comments and Replies –
What are you talking about ?
1. Excitement on a new on a new combine cycle system with fewer parts and less heat loss
surface more efficiency. The system is water swirled into gas turbine section or behind it
to get more electricity from fuel.
2. Start a discussion is the immediate goal.
3. Outcome so far is a lot of “looks good etc.” words heard !
Where does an engineer go with this ?
1. Act on the quick numbers indicate a low end of 10 % less fuel per unit electricity
A. And “Today” precipitation happens more electricity come out of gas turbine units. Big
rain drops; hail erodes the internals of gas turbine. Water into gas turbines goes to work
done by the Air Force in 1944 to develop war emergency “afterburner” like system.
19 Copyright © 2019 by ASME
B. And the use of water into gas turbines for electrical generation before the turbine section
is being done and is not included in the presentation. Such could be used with the
technology presented.
Impact and future ?
1. Cut electricity cost in some grids by half is a guess.
2. Follow-up development for twenty years is my view.
Great benefit ?
Heard it is so with few details a hundred times.

More Related Content

New power energy new patent ap 7 26-19 --

  • 1. 1 Copyright © 2019 by ASME Presented Not Published June 29, 2017 Power & Energy Conference Charlotte, North Carolina Updated expanded July 26, 2019 Power Energy “2017-3191” Analysis of Steam Zoning With Exhaust – Smoke Stack and Water Swirled Into Gas Turbine Technology – Draft – Work in Progress Leonard M. Andersen Water Swirled Into Gas Turbine Tech Caller Box 1529 New York, New York 10116, USA 914-237-7689 ABSTRACT Two and a half years ago I prepared a paper “Power Energy “2017-3191” -Analysis of Steam Zoning With Exhaust – Smoke Stack and Water Swirled Into Gas Turbine Technology and presented. It was not published as part of the proceedings. The New technology covered in PUB. APP. NO. 20170306843 “METHOD AND APPARATUS FOR INCREASING USEFUL ENERGY/THRUST OF A GAS TURBINE ENGINE BY ONE OR MORE ROTATING FLUID MOVING (AGITATOR) PIECES DUE TO FORMATION OF A DEFINED STEAM REGION” Filed: February 27, 2017 published October 26, 2017 first action March 4, 2019 not part of the presentation due to a request by the US Government. The new technology has been developed with water into a flow of hot gas in a swirling pattern most recently with a focus on internal combustion engines , fired boiler stacks and, water swirled into gas turbines combined cycles for more fuel efficiency. Beyond more fuel efficiency there is pollution control of PM 2.5 and PM 10 particulate in coal firing etc.. In electrical generation the latest advance is to have a fluid mover of a paddle nature moving a mass – volume of optimally positioned spaced sized water droplets in hot gas outward from a centerline into a tire / donut shaped volume space where said goes to steam / pressurization. Such pressurization happens making an extractive turbine turn which is connected to an electrical generator. In fired boilers and internal combustion engines the shaft of the fluid mover would be vertical and the extractive turbine would normally be horizontal. The horizontal extractive turbine would have water drops and combustion gas leaving at about 120 C with less particulates exiting. The work in new combined cycle gas turbines prior to this is my two patents is to at the end of the power turbine through blades and/or a mechanism to put water droplets into the hot thrust gas of 350 – 500 C going to steam in concentrated volume. Said volume goes in a steaming chamber. The energy is converted from heat to steam pressurized increase in volume. Increase in volume in the steaming chamber acts on an extractive turbine connected to an electrical generator. This could benefit from aforementioned. The tire / donut shape would be vertical. The maintenance and operation of this is a fast moving subject with in exhaust – stack gas plus 5 % per unit fuel and in the case of water swirled into gas turbines 15 – 25%. The motivation for the presentation is to get discussion going. A speaker on coal fired with experience of use and, second on internal combustion engines automotive / ship propulsion and third on new combined cycle gas turbine and a fourth on aircraft propulsion with the new tech was sought. At this time there is one speaker. This is a start ! NOMENCLATURE
  • 2. 2 Copyright © 2019 by ASME BTU - British thermal unit GTE - Gas Turbine Unit Meg - Million Watt Mock - Mock At sea level, mock 1 is 761 mph Mph - Miles per hour MW - Megawatt (MW) = 1,000 kilowatts Rpm - Revolutions per minute π - 3.14159 KEYWORDS – Natural Gas, Electrical Power Generation , Electrical Generation , Fuel Efficiency, Pollution , Boilers , Internal Combustion Engines, Gas Turbine , Aircraft , Jet Acknowledgments Edward J. Ellis | Leason Ellis – Patent Attorney 914.821.9071 ellis@leasonellis.com One Barker Avenue, Fifth Floor White Plains, New York 10601-1526 Ones Sharing Knowledge With me at ASME ( www.asme.org ) and WPC “World Petroleum Congress” ( www.world-petroleum.org ) events and at www.asme.org online inter-activeness etc. . REFERENCES United States Patents 8,671,696 , 9,376,933 and one pending PUB. APP. NO. 20170306843 “METHOD AND APPARATUS FOR INCREASING USEFUL ENERGY/THRUST OF A GAS TURBINE ENGINE BY ONE OR MORE ROTATING FLUID MOVING (AGITATOR) PIECES DUE TO FORMATION OF A DEFINED STEAM REGION” Len Andersen Gas Turbine Engineering Handbook Author(s): Meherwan P. Boyce 2011 INTRODUCTION The presenter started career with a coal fired air pollution project. At that time a third of a power plant cost was scrubber and resulting sludge cost. My technology is to a hot gas stream ( exhaust / stack / thrust ) as indicated in my first patents ( water droplets are added in optimal spacing positions with swirling around main shaft ) . Said mass in the latest patent is moved radially from center line to form a tire /donut where the water form steam ( pressure energy ) . Said moves extractive turbines or makes airplanes go. In the case of steam move to sides the hot gas at a higher than current off boiler tubes ( ~ 200 C ) and have an optimally water droplets in hot gas mass moved from center into a steam zone – space of donut / tire shape. Go to steam and move an extractive turbine connected to an electrical generator. A parallel is envisioned would be for internal combustion engines. The area of gas turbines is more addressed with many issues resolved. The concern we have is having such happen more cost effectively. My presentation is an answer that has been there since the beginning; add water without wear on the internals of the machine. In total it is the get the benefit in boilers , internal combustion engines , and thrust per unit fuel as with water being ingested into blower of furnace, air intake of an internal combustion engine, water into compressor and/or water injected into combustor of a gas turbine engine with less wear . WATER ADDED TO HOT STACK GAS - EXHAUST - - TURBINE ENGINE THRUST GAS EFFECTS ON PERFORMANCE gives a water droplet to steam volume increase which has a boost of performance per unit fuel. Note following Figure One - New Tech Hot Gas To Electricity , Figure Two – Hot Stack- Exhaust Patent PUB. APP. NO. 20170306843 particle – Pollution Reduction , Figure Three – Latest Patent for Use With Gas Turbines , Figures Four - Gas Turbine with Rain Ingestion Sectioned , Figure Five - Three Sections of Gas Turbine with Rain ( precipitation ) Drops to Stream Thrust Enhancement , Figure Six - The Water Swirled Into Gas Turbine Engine Shown Indicating the Shifted of Rapid Near Instantaneous Water Droplet to Steam Formation from Combustion Section to After Turbine Section and Figure Seven - Combines Gas Turbine Issued Patents Sketch of
  • 3. 3 Copyright © 2019 by ASME a Steam Expansion Chamber www.gasturbineandersen.com . All Figures are at end of the Paper. In the case of gas turbines a swirling mass of water droplets. The way in which this is achieved is one or more of the following 1. Put water and/or volatile through the main shaft of a gas turbine and flow water of from turbine blades / end of main shaft. 2. And/or said liquid flowing out of a “stator” hitting “pins” rotating on the main shaft creating small droplets. 3. Beyond main shaft a rotating unit that is powered by thrust gas flow or other way with said liquid flowing through it and out of through flow points. Such systems can be applied to fired systems ( boilers etc. ) and internal combustion engines. What has been told me is very positive. First thermodynamic analysis is ANNEX A. My analysis follows ! ANALYSIS The analysis of the patent pending is the next paper / presentation. My background is an engineer who has had an electrical generation focus interviewing for jobs in field , hearing presentation about and having operational etc. with diesel generators. This is a New Tech Combined Cycle Gas Turbines (CCGT) technology. My focus will be analyze / explain the technology and in the electrical power grid context explore fits, factors and extrapolations. Made presentation of my technology to a large gas turbine manufacturer and got where is the analysis of gas turbine first two patents on claims of heard by me of 1. Twelve % gas , fourteen % liquid up in fuel to electricity or mechanical energy output compared to combined cycle now in use ! 2. Low capital cost combined cycle units, smaller and in greater numbers. 3. The efficiency of gas turbine electrical generator units 1 to 400 MW is nearly the same which would greatly reduce electrical distribution losses. Much lower startup shut down cost ! Before latest Patent Pending ! The analysis of the aforementioned is not easily done and has commercial interest. Note end of paper resume ANNEX B. As an engineer member of IGTI with plus twenty years experience having since June 2009 focused on gas turbine combined cycle I left quietly with, “I will get back to you!”. What is Water Swirled Into Gas Turbine Technology ? It is New Combine Cycle US Patents 8,671,696 & 9,376,933 & PUB. APP. NO. 20170306843 “METHOD AND APPARATUS FOR INCREASING USEFUL ENERGY/THRUST OF A GAS TURBINE ENGINE BY ONE OR MORE ROTATING FLUID MOVING (AGITATOR) PIECES DUE TO FORMATION OFA DEFINED STEAM REGION” published October 26, 2017 ! The Technology is to have water droplets into the hot end part of the gas turbine with the droplets of water traveling in a curved pattern after the combustion section. THERMODYNAMIC ANALYSIS First thermodynamic analysis is to determine if said water introduced into a gas turbine after the combustor in the turbine and/or end of turbine and/or in the nozzle or connector to extractive turbine “section” yields more thrust energy – electrical energy per unit fuel. Said preliminary analysis is positive and ANNEX A. It says water to steam would increase thrust. There is noted in a Gas Turbine Handbook the adding of water offshore as spray to the connector between the turbine and the extractive turbine is beneficial. A - SIZE OF DROPS The second analysis is mechanical – fluid dynamics of water flow as described in patent. A. Size of drops - 1. Size of Water Droplets Created by Nozzle Parameters &/or Impingement Design Detail
  • 4. 4 Copyright © 2019 by ASME &/or rotational design a. http://www.efm.leeds.ac.uk/CIVE/FluidsLe vel1/Unit03/T6.html - An Introduction To Fluid Mechanics : CIVE1400 SCHOOL OF CIVIL ENGINEERING Leeds University UK Pelton wheel blade Application of the Momentum Equation In this section we will consider the following examples: 1. Force due to the flow of fluid round a pipe bend. 2. Force on a nozzle at the outlet of a pipe. 3. Impact of a jet on a plane surface. 4. Force due to flow round a curved vane. 5. A curved vane on a Pelton wheel turbine. “The above analysis of impact of jets on vanes can be extended and applied to analysis of pins of US Patent 9,376,933 “ 6. Impact of a jet on an angled plane surface Papers ANNEX C - Size of Droplets Etc. B. SPACING OF DROPLETS Spacing of droplets – Evenly spaced across the cross section is a design issue ! C – INTERACTIVENESS OF VAPORIZATION / TEMPERATURE GAS – LIQUID / COOLING OF MASS / TURBULENCE Pertaining to Inter-activeness of vaporization visa vi temperature gas - liquid visa vi cooling of mass visa vi turbulence Found International Journal of Heat and Mass Transfer. April 2016, Experimental investigation of consecutive water droplets falling down through high-temperature gas zone Authors R.S. Volkov, G.V. Kuznetsov, J.C. Legros, P.A. Strizhak saying exploding water droplet with 830 degrees Celsius. Friend asked, “Where is a start point beyond add heat gets steam analysis of water swirled into gas turbine technology?” ! Approximation of Water Droplets Speed With Get Turbine ( Jet Engine ) J47 36000 Produced 1949 to 1956 8000 RPM Speed of Drop = ( Rotational Rate RPM ) ( π D ) = X Part of assembly with main shaft centerlines line of rotation around O.5 foot from said centerline droplet origination X = ( 8000 ) ( 3.14 ) ( 1.0 ) X = 25120 feet / minute Droplet Speed Out of nozzle = ( 25120 feet / minute ) × ( 60 minutes / hour ) ÷ 5280 feet Droplet Speed Out of nozzle =~ 280 mph ( miles per hour ) Droplet Speed As A Point On A Turbine Blade Six Inches from centerline of main shaft Thrust gas at 1.3 mock =1100 mph My view of start point is water droplet(s) circular motion around main shaft at ~280 mph with mock one point three thrust gas parallel to main shaft temperature from 600–910 degrees Celsius to 150 steaming phenomena ! In larger electrical power units ( Siemens SGT – 500 / 19.1 MW Exhaust 370 degrees Celsius. The technology is to put water in droplet form into the hot end of the gas turbine. The “plumbing etc.” of water to droplet form is covered in three patents as concept. The design details lend themselves to models and/or experimentation. The experimentation could be 1. Buying or Designing / Manufacture Rotary Spray Nozzle and installing at the hot end of a gas turbine engine. 2. Operate and take the data. 3. Analyze the data and design better equipment!
  • 5. 5 Copyright © 2019 by ASME Alternatively or as parallel effort hand calculation or model. From there finite element analysis with factors of Size of Water Droplets Created by Nozzle Parameters &/or Impingement Design Detail &/or rotational design, Spacing of droplets, Inter- activeness of vaporization visa vi temperature gas - liquid visa vi cooling of mass visa vi turbulence, etc. Work in progress ! There are start points. The two that appear to be most productive are rain ( precipitation ) into the combustor in a uniform across the cross section way which is covered for gas turbine aircraft propulsion and for electric power combustor sections of gas turbines. The other is extensive study / modeling of the combustors. Rain ( precipitation ) comes in a range of droplet sizes , intensity and by the action of compressor part of the gas turbine engine made uniform and smaller diameter. Rain ( precipitation ) ingestion into gas turbine engines go back 120 years. It rains and better power output. It is covered with papers , models , thesis , reports - “Parametric Analysis of the Exergoeconomic Operation Costs, Environmental and Human Toxicity Indexes of the MF501F3 Gas Turbine” Entropy. Aug 2016, Vol. 18 Issue 8, p1-26. 26p. Development and Integration of rain Ingestion Effects in Engine Performance Simulations, Authors: Roumeliotis, I. , Journal of Engineering for Gas Turbines & Power, Apr 2015, Vol. 137 Issue 4 The thesis is WATER INGESTION EFFECTS ON GAS TURBINE ENGINE PERFORMANCE Supervisor: P. Pilidis October 2008 https://core.ac.uk/download/pdf/138838.pdf A report is NORTH ATLANTIC TREATY ORGANISATION , RESEARCH AND TECHNOLOGYORGANISATION RTO TECHNICAL REPORT TR-AVT-036 2007 Performance Prediction and Simulation of Gas Turbine Engine Operation for Aircraft , Marine , Vehicular , and Power Generation. START POINT TWO COMBUSTOR MODEL PATENTS AND PAPERS Gas turbine engine and corresponding operating method EP 2476880 A1 A gas turbine engine has in flow series: a compressor section, a combustor, and a turbine section. The engine further has a steam generator, and a water and steam delivery system. During an engine start-up period, the delivery system delivers liquid water to the combustor and mixes the delivered water in its liquid state with working gas in the combustor. After the start-up period, the delivery system accepts steam from the steam generator, delivers the steam to the combustor and mixes the delivered steam in its gaseous state with the working gas in the combustor. Papers ANNEX D – Papers on Combustion Models OTHER FACTORS IN THE ANANLYSIS 1. Rotational speed and flow of thrust gas Siemens SGT-500 Turbine speed 3,450 RPM Mitsubishi M501F Turbine speed 3,600 RPM US Military J47 36000 Produced 8000 rpm 747 Gas Turbine JT9D exhaust speed 811 mph TRADE OFF’S – OPTIMIZATIONS Water Pressure Into System High 1. Mist –Diesel Injector Analysis 2. Cost Higher Beyond practicality
  • 6. 6 Copyright © 2019 by ASME 3. Possibly used on aircraft after burner applications 4. Seal Concerns 5. Impinging patent possible fit Low 1. Exploding water drops 1200 degrees Celsius at less than 5 mph mist maker ? 2. “Only” way with seals with rotation through shaft ( main shaft ) / pressure happening through main shaft approximately 30 psi cooling air for turbine blades and lubricating oil. Efficiency – Weight – Uses - Combo 1. Impinging on pins – lighter aircraft / less expensive 2. Through main shaft aircraft / power generation 3. After main shaft heavier aircraft / larger power generation 4. Combo’s of the Above ? Power Generation Grid context explore fits , factors and extrapolations  Grid modification – Currently 500 Meg units to “convenient” 5 Meg units ?  Change plans with more local generation use. The steam engine use prior to grid analogy  Trade offs Electrical Transmission loss against gas line installation – delivery cost  Cheaper electricity  Extrapolation one Meg power and up future. Heard it is happening ! COMMENTS AND REPLIES -– ANNEX E CONCLUSIONS A) Models using finite element analysis available for start point water droplet evenly distributed with different size etc. B) Using engineering and adequate and adopting model(s) the elements of the patents ( mechanical pieces ) an optimum space round center line of the main shaft with a thickness having an even water droplet density could be achieved. C) The potential of the invention ( three patents ) water swirled into gas turbine technology could be enhanced with analysis. SUMMARY - A start of the analysis of water swirled into gas turbine technology is presented . PRESENTER Leonard M. Andersen Engineer len@lenandersen.com ( HP SecureMail voltage connected ) POB 1529 New York, New York 10116 ( +$1299 per year Caller Box ) 914-536-7101 Cell Phone / 914-237-7689 Home / 800-428-4801 www.gasturbineandersen.com www.lenandersen.com
  • 7. 7 Copyright © 2019 by ASME Figure One - New Tech Hot Gas To Electricity
  • 8. 8 Copyright © 2019 by ASME
  • 9. 9 Copyright © 2019 by ASME
  • 10. 10 Copyright © 2019 by ASME
  • 11. 11 Copyright © 2019 by ASME
  • 12. 12 Copyright © 2019 by ASME
  • 13. 13 Copyright © 2019 by ASME Figure Seven - Combines Gas Turbine Issued Patents Sketch of a Steam Expansion Chamber www.gasturbineandersen.com
  • 14. 14 Copyright © 2019 by ASME ANNEX A The basis of the analysis is one unit of fuel per one unit of water on weight. * 19,000 BTU’s per pound of fuel ( Jet A ) * It takes 0.24 BTU’s to heat one pound air one degree Fahrenheit * 970 BTU’s per pound of water to create steam * Steam from one pound of water creates 27 cubic feet of one atmosphere steam * Air Fuel Ratio ( AFR ) is 150 to 1 * Thrust gas enters system at 1200 degrees Fahrenheit * Thrust gas volume per unit volume is directly proportional to gas volume which equals cooling effect of vaporization shrinkage and made larger by steam increase volume It follows water thrust gas ratio 150 to one therefore 970 BTU – Pound / 150 Pound = 6.4 BTU / Pound And 0.24 BTU per degree temperature change therefore 27 degree F temperature drop , volume decrease of 1-2 percent. Steam volume as partial of thrust per pound fuel equals 19000 / 970 = 18.5 pounds steam 18.5 pound x 28.8 cubic foot / pound = 500 cubic feet Total thrust gas volume = 150 pounds / 0.075 pound-cubic foot 2000. Net Thrust Gas Volume Increase about = 25-2 = 23 % Answer yes as preliminary analysis ANNEX B Resume of Presenter for Leonard M. Andersen – Gas Turbine Engineer len@lenandersen.com ( HP SecureMail voltage connected ) water-gas- turbine@lenandersen.com 914-536-7101 Cell Phone / 914-237-7689 Home / 800-428-4801 POB 1529 New York , New York 10116 ( +$1299 per year Caller Box / Most Secure Service At Large Post Office USA ) / 46 Alexander Av , Yonkers NY www.gasturbineandersen.com
  • 15. 15 Copyright © 2019 by ASME www.lenandersen.com Professional Experience Ten years focus on Water Swirled into In Gas Turbine Technology work including attending IGTI ASME events , making technical presentations inTexas / Kingdom of Saudi Arabia / Qatar / Russia. The work has resulted in two patents issued and one patent pending . I attended at the Turbo Expo Pheonix 2019 / OSLO 2018 and attended many ASME Gas Turbine Technical Chapter Meetings www.asmegttc.org . I attended day long work shops “Design, Operation and Maintenance Considerations for Cogeneration and Combined Cycle Systems” at the Turbo Expo / Power Energy event 2017 , at the Turbo Expo Montreal in June 2015 took a short course “Gas Turbine Aerothermodynamics and Performance Calculations” and at Gas Turbine Users Symposium (GTUS) with Texas A&M’s Turbo machinery Symposium, 2010 Houston attended short course “Combined Cycle and Cogeneration Power Plants”! Welding Inspection Engineering New York , Connecticut , Ohio August 2014 to Present  Journalist World Petroleum Congress Istanbul ( www.22wpc.com ) July 2017 Welding Inspector CWI / Construction Project Manager / Engineer Employed October 2000 to May 2014 New York City Department of Transportation - Division of Bridges. Spoke Chinese every day at work. Worked in Spanish language in Mexico, Spain etc., and Arabic in the Kingdom of Saudi Arabia for near a year, Norwegian in Norway etc. for about six months and worked in the Russian language. In journalism I covered the World Petroleum Congress www.world- petroleum.org events 2002 Rio de Janeiro Brazil , 2005 Johannesburg South Africa , 2008 Madrid Spain , 2011 Doha Qatar and Moscow Russia 2014 as an accredited journalist. Fellow journalist mentioned at the last one, "You know everyone". Inventing one patent issued in Lubricating / Motor Oil , two and pending in Power Generation / Gas Turbine Technology which I wrote. Pursuant to such I attended STLE ( www.stle.org ) events and International Gas Turbine Institute (IGTI) ASME events. Education –
  • 16. 16 Copyright © 2019 by ASME  Registered Representative www.sec.gov ( Stock Broker ) Securities Training Corporation New York , New York  BSChE Chemical Engineering Degree, University of Arizona, Tucson, Arizona Published Works – Welding Journal - one and Society of Petroleum Engineers 30994 & Patents  “METHOD AND APPARATUS FOR INCREASING USEFUL ENERGY/THRUST OF A GAS TURBINE ENGINE BY ONE OR MORE ROTATING FLUID MOVING (AGITATOR) PIECES DUE TO FORMATION OF A DEFINED STEAM REGION” , published October 26, 2017  Gas Turbine Thrust Fuel Efficiency Enhancement System Water (Volatile) Introduction Arrangement Method and Means 9,376,933  METHOD AND APPARATUS FOR INCREASING THRUST OR OTHER USEFUL ENERGY OUTPUT OF A DEVICE WITH A ROTATING ELEMENT 8,671,696  Lubricating/sealing oil-based composition and method of manufacture thereof - 6,358,891 Additionally Five patents in welding , two in petroleum extraction Active Memberships in Engineering and Technical Societies International Gas Turbine Institute ( IGTI ) events – Presentation at Power Energy 2017 and attending week long events 2010 / 2015 / 2017 / 2018 ! The Metropolitan Section of the American Society of Mechanical Engineers (ASME) in New York City attends meetings as a member metsection@asme.org / www.asmemetsection.org Society of Tribologists and Lubrication Engineers www.stle.org & SPE & AIChE & ASCE & AWS ANNEX C Size of Droplets Etc. Droplet impact cavity film thickness measurements versus time after drop impact and cavity radius for thin static residual liquid layer thicknesses.
  • 17. 17 Copyright © 2019 by ASME By: Kuhlman, John M.; Hillen, Nicholas L. Experimental Thermal & Fluid Science. Oct 2016, Subjects: Liquid films; Thickness measurement; Reynolds number; Heat flux; Drops Optimization study on pin tip diameter of an impact-pin nozzle at high pressure ratio. By: Kumar, C.; Lee, Kwon; Park, Tae; Cha, Bong; Kim, Heuy. Journal of Mechanical Science & Technology. Sep 2016, Subjects: Gas turbines; MATHEMATICAL models; High pressure (Technology); Compressors; Jet impingement; Pump and compressor manufacturing; Industrial Machinery and Equipment Merchant Wholesalers; Air and Gas Compressor Manufacturing; Turbine and Turbine Generator Set Units Manufacturing; All Other Plastics Product Manufacturing; All other plastic product manufacturing; Nozzles Numerical and experimental investigation on droplet dynamics and dispersion of a jet engine injector. By: Keller, J.; Gebretsadik, M.; Habisreuther, P.; Turrini, F.; Zarzalis, N.; Trimis, D. International Journal of Multiphase Flow. Oct 2015, Subjects: Numerical analysis; Hypodermic jet injectors; Combustion chambers; Hydraulic turbines; Liquid fuels; Solid Waste Combustors and Incinerators; Waste treatment and disposal; Conventional oil and gas extraction; Turbine and Turbine Generator Set Units Manufacturing Three-Dimensional Mass Fraction Distribution of a Spray Measured by X-Ray Computed Tomography. By: Coletti, Filippo; Benson, Michael J.; Sagues, Alexander L.; Miller, Benjamin H.; Fahrig, Rebecca; Eaton, John K. Journal of Engineering for Gas Turbines & Power. May2014 Subjects: RESEARCH; X-ray computed microtomography; Other Basic Inorganic Chemical Manufacturing; All other basic inorganic chemical manufacturing; Atomization; Spray combustion; Pressure; Iodine "Numerical Analysis on Spray Cooling of Gas Turbine Exhaust Gas" By: HAN, D. International Journal of Transport Phenomena. 2014, Subjects: Spray cooling; Gas turbines -- Exhaust gas; Mass transfer; Turbulence -- Mathematical models; Numerical analysis; Particle size distribution ANNEX D Papers on Combustion Models Influence of Main Swirler Vane Angle on the Ignition Performance of TeLESS-II Combustor Bo Wang, Chi Zhang, Yuzhen Lin, Xin Hui and Jibao Li Bo Wang Eng. Gas Turbines Power 139(1), 011501 (Aug 16, 2016)
  • 18. 18 Copyright © 2019 by ASME Unsteady Computational Fluid Dynamics Investigation of Effusion Cooling Process in a Lean Burn Aero-Engine Combustor L. Mazzei, A. Picchi, A. Andreini, B. Facchini and I. Vitale Eng. Gas Turbines Power 139(1), 011502 (Aug 16, 2016) Detached-Eddy Simulations (DES) of a complex swirl stabilized gas turbine model combustor. By: Ali, Ahlem Ben Sik; Kriaa, Wassim; Mhiri, Hatem; Bournot, Philippe. International Journal of Energy & Environment. 2016, Subjects: GAS turbines; COMBUSTION chambers; SWIRLING flow; SHEARING force; TURBULENCE; Conventional oil and gas extraction; Waste treatment and disposal; Solid Waste Combustors and Incinerators; Turbine and Turbine Generator Set Units Manufacturing Numerical Analysis of Turbulent Combustion in a Model Swirl Gas Turbine Combustor. By: Benim, Ali Cemal; Iqbal, Sohail; Joos, Franz; Wiedermann, Alexander “Journal of Combustion” 9/15/2016, Subjects: COMBUSTION gases -- Analysis; GAS turbines -- Combustion chambers; NUMERICAL analysis; NATURAL gas -- Measurement; REYNOLDS stress; FLUE gases -- Measurement; SYNTHESIS gas; Natural Gas Distribution ANNEX E Comments and Replies – What are you talking about ? 1. Excitement on a new on a new combine cycle system with fewer parts and less heat loss surface more efficiency. The system is water swirled into gas turbine section or behind it to get more electricity from fuel. 2. Start a discussion is the immediate goal. 3. Outcome so far is a lot of “looks good etc.” words heard ! Where does an engineer go with this ? 1. Act on the quick numbers indicate a low end of 10 % less fuel per unit electricity A. And “Today” precipitation happens more electricity come out of gas turbine units. Big rain drops; hail erodes the internals of gas turbine. Water into gas turbines goes to work done by the Air Force in 1944 to develop war emergency “afterburner” like system.
  • 19. 19 Copyright © 2019 by ASME B. And the use of water into gas turbines for electrical generation before the turbine section is being done and is not included in the presentation. Such could be used with the technology presented. Impact and future ? 1. Cut electricity cost in some grids by half is a guess. 2. Follow-up development for twenty years is my view. Great benefit ? Heard it is so with few details a hundred times.