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FR2697289B1 - Turboréacteur à double flux avec système de réchauffement d'air sur la tuyère primaire. - Google Patents

Turboréacteur à double flux avec système de réchauffement d'air sur la tuyère primaire.

Info

Publication number
FR2697289B1
FR2697289B1 FR9212798A FR9212798A FR2697289B1 FR 2697289 B1 FR2697289 B1 FR 2697289B1 FR 9212798 A FR9212798 A FR 9212798A FR 9212798 A FR9212798 A FR 9212798A FR 2697289 B1 FR2697289 B1 FR 2697289B1
Authority
FR
France
Prior art keywords
double
heating system
air heating
primary nozzle
flow turbojet
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 - Fee Related
Application number
FR9212798A
Other languages
English (en)
Other versions
FR2697289A1 (fr
Inventor
Francis Forest
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR9212798A priority Critical patent/FR2697289B1/fr
Priority to GB9321483A priority patent/GB2272025A/en
Publication of FR2697289A1 publication Critical patent/FR2697289A1/fr
Application granted granted Critical
Publication of FR2697289B1 publication Critical patent/FR2697289B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F02C7/16—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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9212798A 1992-10-28 1992-10-28 Turboréacteur à double flux avec système de réchauffement d'air sur la tuyère primaire. Expired - Fee Related FR2697289B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9212798A FR2697289B1 (fr) 1992-10-28 1992-10-28 Turboréacteur à double flux avec système de réchauffement d'air sur la tuyère primaire.
GB9321483A GB2272025A (en) 1992-10-28 1993-10-18 Air heating system for turbojet bypass engines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9212798A FR2697289B1 (fr) 1992-10-28 1992-10-28 Turboréacteur à double flux avec système de réchauffement d'air sur la tuyère primaire.

Publications (2)

Publication Number Publication Date
FR2697289A1 FR2697289A1 (fr) 1994-04-29
FR2697289B1 true FR2697289B1 (fr) 1994-12-09

Family

ID=9434888

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9212798A Expired - Fee Related FR2697289B1 (fr) 1992-10-28 1992-10-28 Turboréacteur à double flux avec système de réchauffement d'air sur la tuyère primaire.

Country Status (2)

Country Link
FR (1) FR2697289B1 (fr)
GB (1) GB2272025A (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2889298B1 (fr) * 2005-07-28 2010-11-26 Airbus France Echangeur thermique, ensemble propulseur, et aeronef comportant un tel ensemble propulseur
FR2896276B1 (fr) * 2006-01-19 2008-02-15 Airbus France Sas Turbomoteur a double flux pourvu d'un prerefroidisseur.
FR2896275B1 (fr) * 2006-01-19 2010-05-28 Airbus France Turbomoteur a double flux pourvu d'un prerefroidisseur.
FR2902830B1 (fr) * 2006-06-27 2008-08-08 Airbus France Sas Turboreacteur pour aeronef
GB0822639D0 (en) 2008-12-12 2009-01-21 Rolls Royce Plc By virtue of section 39(1)(a) of the Patents Act 1977
US20110179766A1 (en) * 2009-10-27 2011-07-28 Fly Steam, LLC Heat recovery system
FR3138671B1 (fr) * 2022-08-02 2025-06-27 Safran Nacelles Système d’échappement pour turbomachine comprenant un échangeur de chaleur

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578263A (en) * 1941-11-07 1946-06-21 Asiatic Petroleum Co Ltd Improvements in or relating to jet propulsion apparatus
GB716145A (en) * 1952-02-19 1954-09-29 Ernest Lagelbauer Improvements in aircraft jet propulsion engines including a ducted fan
BE541588A (fr) * 1954-09-27
GB949585A (en) * 1961-04-11 1964-02-12 Entwicklungsbau Pirna Veb Improvements in axial flow type gas turbines
US3307355A (en) * 1961-10-31 1967-03-07 Gen Electric Augmentation system for reaction engine using liquid fuel for cooling
GB1090586A (en) * 1966-02-03 1967-11-08 Rolls Royce Improvements relating to jet engines
US4187675A (en) * 1977-10-14 1980-02-12 The United States Of America As Represented By The Secretary Of The Air Force Compact air-to-air heat exchanger for jet engine application
US4333309A (en) * 1980-01-30 1982-06-08 Coronel Paul D Steam assisted gas turbine engine
GB2164706B (en) * 1984-09-25 1988-06-08 United Technologies Corp Pressurized nacelle compartment for active clearance controlled gas turbine engines

Also Published As

Publication number Publication date
GB9321483D0 (en) 1993-12-08
FR2697289A1 (fr) 1994-04-29
GB2272025A (en) 1994-05-04

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
CD Change of name or company name
ST Notification of lapse

Effective date: 20060630