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FR1104211A - New thermal cycle and combustion device applying this cycle - Google Patents

New thermal cycle and combustion device applying this cycle

Info

Publication number
FR1104211A
FR1104211A FR1104211DA FR1104211A FR 1104211 A FR1104211 A FR 1104211A FR 1104211D A FR1104211D A FR 1104211DA FR 1104211 A FR1104211 A FR 1104211A
Authority
FR
France
Prior art keywords
cycle
combustion device
device applying
new thermal
thermal cycle
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
French (fr)
Inventor
Gabriel Brola
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GEN THERMIQUE
Original Assignee
GEN THERMIQUE
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 GEN THERMIQUE filed Critical GEN THERMIQUE
Application granted granted Critical
Publication of FR1104211A publication Critical patent/FR1104211A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/12—Injection-induction jet engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1104211D 1954-05-05 1954-05-05 New thermal cycle and combustion device applying this cycle Expired FR1104211A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1104211T 1954-05-05

Publications (1)

Publication Number Publication Date
FR1104211A true FR1104211A (en) 1955-11-17

Family

ID=9622654

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1104211D Expired FR1104211A (en) 1954-05-05 1954-05-05 New thermal cycle and combustion device applying this cycle

Country Status (1)

Country Link
FR (1) FR1104211A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1155941B (en) * 1959-01-02 1963-10-17 Garrett Corp Engine
DE1192876B (en) * 1960-02-02 1965-05-13 Gen Electric Burner arrangement for a jet engine, the combustion chamber of which is surrounded by a heat exchanger
DE1199542B (en) * 1959-06-24 1965-08-26 United Aircraft Corp Device for fuel supply for liquid rockets
DE1209809B (en) * 1959-04-08 1966-01-27 Paul Sommer Continuously working jet engine
US5832718A (en) * 1995-12-19 1998-11-10 Daimler-Benz Aerospace Airbus Gmbh Combustion chamber especially for a gas turbine engine using hydrogen as fuel
US6092590A (en) * 1996-05-03 2000-07-25 Daimlerchrysler Aerospace Airbus Gmbh Method and evaporator device for evaporating a low temperature liquid medium
WO2011131493A2 (en) * 2010-04-20 2011-10-27 Rolls-Royce Plc Air breathing reaction propulsion engine

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1155941B (en) * 1959-01-02 1963-10-17 Garrett Corp Engine
DE1209809B (en) * 1959-04-08 1966-01-27 Paul Sommer Continuously working jet engine
DE1199542B (en) * 1959-06-24 1965-08-26 United Aircraft Corp Device for fuel supply for liquid rockets
DE1192876B (en) * 1960-02-02 1965-05-13 Gen Electric Burner arrangement for a jet engine, the combustion chamber of which is surrounded by a heat exchanger
US5832718A (en) * 1995-12-19 1998-11-10 Daimler-Benz Aerospace Airbus Gmbh Combustion chamber especially for a gas turbine engine using hydrogen as fuel
US6092590A (en) * 1996-05-03 2000-07-25 Daimlerchrysler Aerospace Airbus Gmbh Method and evaporator device for evaporating a low temperature liquid medium
US6263678B1 (en) 1996-05-03 2001-07-24 Daimlerchrysler Aerospace Airbus Gmbh Method of evaporating a low temperature liquid medium
WO2011131493A2 (en) * 2010-04-20 2011-10-27 Rolls-Royce Plc Air breathing reaction propulsion engine
WO2011131493A3 (en) * 2010-04-20 2012-03-08 Rolls-Royce Plc Air breathing reaction propulsion engine

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