PL4095369T3 - Architektura silnika wodorowego z podwójnym cyklem i chłodzeniem międzystopniowym - Google Patents

Architektura silnika wodorowego z podwójnym cyklem i chłodzeniem międzystopniowym

Info

Publication number
PL4095369T3
PL4095369T3 PL22175943.4T PL22175943T PL4095369T3 PL 4095369 T3 PL4095369 T3 PL 4095369T3 PL 22175943 T PL22175943 T PL 22175943T PL 4095369 T3 PL4095369 T3 PL 4095369T3
Authority
PL
Poland
Prior art keywords
intercooled
hydrogen engine
engine architecture
dual cycle
dual
Prior art date
Application number
PL22175943.4T
Other languages
English (en)
Inventor
Scott Smith
Original Assignee
Pratt & Whitney Canada Corp.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Pratt & Whitney Canada Corp. filed Critical Pratt & Whitney Canada Corp.
Publication of PL4095369T3 publication Critical patent/PL4095369T3/pl

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/263—Control of fuel supply by means of fuel metering valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/211—Heat transfer, e.g. cooling by intercooling, e.g. during a compression cycle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
PL22175943.4T 2021-05-27 2022-05-27 Architektura silnika wodorowego z podwójnym cyklem i chłodzeniem międzystopniowym PL4095369T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US17/331,942 US11542869B2 (en) 2021-05-27 2021-05-27 Dual cycle intercooled hydrogen engine architecture

Publications (1)

Publication Number Publication Date
PL4095369T3 true PL4095369T3 (pl) 2025-06-23

Family

ID=81851082

Family Applications (1)

Application Number Title Priority Date Filing Date
PL22175943.4T PL4095369T3 (pl) 2021-05-27 2022-05-27 Architektura silnika wodorowego z podwójnym cyklem i chłodzeniem międzystopniowym

Country Status (6)

Country Link
US (3) US11542869B2 (pl)
EP (2) EP4600471A1 (pl)
CN (1) CN115405424A (pl)
BR (1) BR102022010304A2 (pl)
CA (1) CA3160735A1 (pl)
PL (1) PL4095369T3 (pl)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11542869B2 (en) 2021-05-27 2023-01-03 Pratt & Whitney Canada Corp. Dual cycle intercooled hydrogen engine architecture
US12351337B2 (en) 2021-11-19 2025-07-08 General Electric Company Sub-coolers for refueling onboard cryogenic fuel tanks and methods for operating the same
US11946419B2 (en) * 2022-02-23 2024-04-02 General Electric Company Methods and apparatus to produce hydrogen gas turbine propulsion
US20230399986A1 (en) * 2022-06-09 2023-12-14 General Electric Company Monitoring systems for hydrogen fueled aircraft
US11862781B1 (en) * 2022-08-15 2024-01-02 Hamilton Sundstrand Corporation Auxiliary power generation and cooling systems on liquid hydrogen fueled aircraft
US11905884B1 (en) * 2022-09-16 2024-02-20 General Electric Company Hydrogen fuel system for a gas turbine engine
US12435664B2 (en) 2023-06-16 2025-10-07 Pratt & Whitney Canada Corp. Gas turbine engine with water recovery system
US12209535B2 (en) 2023-06-16 2025-01-28 Pratt & Whitney Canada Corp. Turbine engine compressor intercooler
US12486803B2 (en) 2023-06-16 2025-12-02 Pratt & Whitney Canada Corp. Gas turbine engine system with fuel driven turbine
GB202317415D0 (en) * 2023-11-14 2023-12-27 Rolls Royce Plc Propulsion system comprising a hydrogen-burning gas turbine engine
GB202317413D0 (en) * 2023-11-14 2023-12-27 Rolls Royce Plc Propulsion system comprising a hydrogen-burning gas turbine engine

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH391375A (de) 1962-02-26 1965-04-30 Sulzer Ag Verfahren zum Betrieb einer Kolbenbrennkraftmaschine mit gasförmigem Brennstoff und Kolbenbrennkraftmaschine zur Ausübung des Verfahrens
DE2413507A1 (de) * 1974-03-20 1975-10-02 Motoren Turbinen Union Gasturbine fuer kryogenen kraftstoff
JPH02289135A (ja) 1989-04-25 1990-11-29 Howa Mach Ltd 紡機の清掃装置
US5154051A (en) * 1990-10-22 1992-10-13 General Dynamics Corporation Air liquefier and separator of air constituents for a liquid air engine
US5347806A (en) 1993-04-23 1994-09-20 Cascaded Advanced Turbine Limited Partnership Cascaded advanced high efficiency multi-shaft reheat turbine with intercooling and recuperation
US6405522B1 (en) * 1999-12-01 2002-06-18 Capstone Turbine Corporation System and method for modular control of a multi-fuel low emissions turbogenerator
US7246482B2 (en) * 2004-07-16 2007-07-24 Honeywell International, Inc. Gas turbine engine bleed air power assist system and method
US8146370B2 (en) * 2008-05-21 2012-04-03 Honeywell International Inc. Turbine drive system with lock-up clutch and method
US8291715B2 (en) * 2008-06-11 2012-10-23 Honeywell International Inc. Bi-modal turbine assembly and starter / drive turbine system employing the same
US8572974B2 (en) * 2009-07-31 2013-11-05 Hamilton Sundstrand Corporation Variable speed and displacement electric fluid delivery system for a gas turbine engine
US8984856B2 (en) * 2010-04-12 2015-03-24 Hamilton Sundstrand Corporation Flexible fuel system
US9249723B2 (en) 2014-06-13 2016-02-02 Bechtel Power Corporation Turbo-compound reheat combined cycle power generation
GB2531775B (en) * 2014-10-30 2018-05-09 Rolls Royce Plc A gas turbine using cryogenic fuel passed through a fuel turbine
EP3301278A1 (en) 2016-09-30 2018-04-04 Siemens Aktiengesellschaft Gas turbine arrangement with controlled bleed air injection into combustor, and method of operation
US10989117B2 (en) * 2018-09-14 2021-04-27 Raytheon Technologies Corporation Hybrid expander cycle with pre-compression cooling and turbo-generator
US11047307B2 (en) * 2018-09-14 2021-06-29 Raytheon Technologies Corporation Hybrid expander cycle with intercooling and turbo-generator
US11041439B2 (en) * 2018-09-14 2021-06-22 Raytheon Technologies Corporation Hybrid expander cycle with turbo-generator and cooled power electronics
US10704461B2 (en) * 2018-09-27 2020-07-07 Garrett Transportation I Inc. Turbocharged internal combustion engine with a portion of exhaust gases from engine bypassing turbocharger turbine for rapid catalyst light-off without waste gate performance penalty in turbine
GB2582356B (en) 2019-03-21 2021-09-22 Intelligent Energy Ltd Evaporatively cooled fuel cell systems with turbine boost by exhaust streams
US20210340908A1 (en) * 2020-05-01 2021-11-04 Raytheon Technologies Corporation Gas turbine engines having cryogenic fuel systems
US11448133B2 (en) * 2020-05-05 2022-09-20 Raytheon Technologies Corporation Moderate pressure liquid hydrogen storage for hybrid-electric propulsion system
EP3978737B1 (en) * 2020-09-30 2024-04-17 Rolls-Royce plc Complex cycle gas turbine engine
US11542869B2 (en) * 2021-05-27 2023-01-03 Pratt & Whitney Canada Corp. Dual cycle intercooled hydrogen engine architecture
GB202114829D0 (en) * 2021-10-18 2021-12-01 Rolls Royce Plc Aircraft propulsion system
US11692491B1 (en) * 2022-05-05 2023-07-04 Raytheon Technologies Corporation Transmission and method for control of boost spool

Also Published As

Publication number Publication date
US12037946B2 (en) 2024-07-16
US20220381183A1 (en) 2022-12-01
EP4095369A3 (en) 2023-03-01
EP4095369A2 (en) 2022-11-30
US11542869B2 (en) 2023-01-03
CN115405424A (zh) 2022-11-29
BR102022010304A2 (pt) 2022-12-06
US20230133397A1 (en) 2023-05-04
EP4600471A1 (en) 2025-08-13
CA3160735A1 (en) 2022-11-27
US20240328355A1 (en) 2024-10-03
EP4095369B1 (en) 2025-04-16
US12421899B2 (en) 2025-09-23

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