RU96123904A - THE COMBUSTION CHAMBER - Google Patents

THE COMBUSTION CHAMBER

Info

Publication number
RU96123904A
RU96123904A RU96123904/06A RU96123904A RU96123904A RU 96123904 A RU96123904 A RU 96123904A RU 96123904/06 A RU96123904/06 A RU 96123904/06A RU 96123904 A RU96123904 A RU 96123904A RU 96123904 A RU96123904 A RU 96123904A
Authority
RU
Russia
Prior art keywords
combustion chamber
evaporator
flame tube
chamber according
burner
Prior art date
Application number
RU96123904/06A
Other languages
Russian (ru)
Other versions
RU2133849C1 (en
Inventor
Зуттроп Фридеманн
Original Assignee
Даймлер-Бенц Эйроспейс Эйрбас ГмбХ
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
Priority claimed from DE19547515A external-priority patent/DE19547515A1/en
Application filed by Даймлер-Бенц Эйроспейс Эйрбас ГмбХ filed Critical Даймлер-Бенц Эйроспейс Эйрбас ГмбХ
Publication of RU96123904A publication Critical patent/RU96123904A/en
Application granted granted Critical
Publication of RU2133849C1 publication Critical patent/RU2133849C1/en

Links

Claims (4)

1. Камера сгорания с горелкой и жаровой трубой для работающей на водороде газовой турбины, отличающаяся тем, что испаритель (6) с входом (7) для жидкого водорода (LH2) и выходом (8) для газообразного водорода (GH2) установлен внутри жаровой трубы (3) и покрывает по меньшей мере часть внутренней поверхности жаровой трубы (3).1. A combustion chamber with a burner and a flame tube for a hydrogen gas turbine, characterized in that the evaporator (6) with an inlet (7) for liquid hydrogen (LH2) and an outlet (8) for hydrogen gas (GH2) is installed inside the flame tube (3) and covers at least a portion of the inner surface of the flame tube (3). 2. Камера сгорания по п.1, отличающаяся тем, что испаритель (6) выполнен в виде трубчатой спирали. 2. The combustion chamber according to claim 1, characterized in that the evaporator (6) is made in the form of a tubular spiral. 3. Камера сгорания по п.1, отличающаяся тем, что испаритель (6) выполнен в виде двойной стенки. 3. The combustion chamber according to claim 1, characterized in that the evaporator (6) is made in the form of a double wall. 4. Камера сгорания по п.1, отличающаяся тем, что выход (8) испарителя (6) для газообразного водорода соединен непосредственно с горелкой (2). 4. The combustion chamber according to claim 1, characterized in that the outlet (8) of the evaporator (6) for gaseous hydrogen is connected directly to the burner (2).
RU96123904A 1995-12-19 1996-12-18 Combustion chamber RU2133849C1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19547515A DE19547515A1 (en) 1995-12-19 1995-12-19 Combustion chamber
DE19547515.1 1995-12-19

Publications (2)

Publication Number Publication Date
RU96123904A true RU96123904A (en) 1999-02-20
RU2133849C1 RU2133849C1 (en) 1999-07-27

Family

ID=7780613

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96123904A RU2133849C1 (en) 1995-12-19 1996-12-18 Combustion chamber

Country Status (5)

Country Link
US (1) US5832718A (en)
EP (1) EP0780639B1 (en)
JP (2) JP4240549B2 (en)
DE (2) DE19547515A1 (en)
RU (1) RU2133849C1 (en)

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US6681749B2 (en) 2001-11-13 2004-01-27 Raymond B. Bushnell Vapor fueled engine
EP1398569A1 (en) * 2002-09-13 2004-03-17 Siemens Aktiengesellschaft Gas turbine
US6907866B2 (en) * 2003-11-11 2005-06-21 Vapor Fuel Technologies, Inc. Vapor fueled engine
US7028675B2 (en) * 2003-11-11 2006-04-18 Vapor Fuel Technologies, Inc. Vapor fueled engine
US7752848B2 (en) * 2004-03-29 2010-07-13 General Electric Company System and method for co-production of hydrogen and electrical energy
DE102005060704A1 (en) * 2005-12-19 2007-06-28 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor
US7631637B2 (en) 2006-06-01 2009-12-15 Vapor Fuel Technologies, Llc System for improving fuel utilization
US7802434B2 (en) * 2006-12-18 2010-09-28 General Electric Company Systems and processes for reducing NOx emissions
US20100314878A1 (en) * 2009-06-16 2010-12-16 Dewitt Monte Douglas Direct Generation of Steam Motive Flow by Water-Cooled Hydrogen/Oxygen Combustion
CA2771615A1 (en) * 2009-09-25 2011-03-31 Exponential Technologies, Inc. Pressure gain combustion heat generator
US9033670B2 (en) 2012-04-11 2015-05-19 Honeywell International Inc. Axially-split radial turbines and methods for the manufacture thereof
US9115586B2 (en) 2012-04-19 2015-08-25 Honeywell International Inc. Axially-split radial turbine
JP2016504523A (en) * 2012-12-28 2016-02-12 ゼネラル・エレクトリック・カンパニイ Turbine engine assembly including a cryogenic fuel system
US9476305B2 (en) 2013-05-13 2016-10-25 Honeywell International Inc. Impingement-cooled turbine rotor
EP3978807A3 (en) 2020-09-30 2022-07-06 Rolls-Royce plc Direct fuel injection system
US11674446B2 (en) * 2021-08-30 2023-06-13 Collins Engine Nozzles, Inc. Cooling for surface ignitors in torch ignition devices
US11952946B2 (en) * 2021-10-15 2024-04-09 Rtx Corporation Turbine engine with preheat of cryogenic fuel via intermediate fluid
US11661889B1 (en) * 2022-01-21 2023-05-30 Raytheon Technologies Corporation Hydrogen powered geared turbo fan engine with an off-set reduced core
US11946419B2 (en) 2022-02-23 2024-04-02 General Electric Company Methods and apparatus to produce hydrogen gas turbine propulsion

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2221477A (en) * 1939-04-29 1940-11-12 Cyclone Fence Company Fence hardware
US2621477A (en) * 1948-06-03 1952-12-16 Power Jets Res & Dev Ltd Combustion apparatus having valve controlled passages for preheating the fuel-air mixture
FR1104211A (en) * 1954-05-05 1955-11-17 Gen Thermique New thermal cycle and combustion device applying this cycle
US3237400A (en) * 1957-04-05 1966-03-01 United Aircraft Corp Turborocket engine
US4899538A (en) * 1987-11-20 1990-02-13 Sundstrand Corporation Hot gas generator
DE3836912A1 (en) * 1988-09-01 1990-03-15 Mtu Muenchen Gmbh METHOD FOR FUEL SUPPLY
DE4304559C1 (en) * 1993-02-16 1994-03-24 Deutsche Aerospace Cooled structure production method - forms tube wall of small pipes with covering layer thicker at mounting flange and spark-erodes openings in pipes for coolant at flange seat
DE4315256A1 (en) * 1993-05-07 1994-11-10 Mtu Muenchen Gmbh Device for distributing and supplying and removing a coolant to a wall of a turbo, in particular turbo ramjet engine

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