FR3050720B1 - Aeronef a au moins un systeme propulsif auxiliaire - Google Patents

Aeronef a au moins un systeme propulsif auxiliaire Download PDF

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Publication number
FR3050720B1
FR3050720B1 FR1653766A FR1653766A FR3050720B1 FR 3050720 B1 FR3050720 B1 FR 3050720B1 FR 1653766 A FR1653766 A FR 1653766A FR 1653766 A FR1653766 A FR 1653766A FR 3050720 B1 FR3050720 B1 FR 3050720B1
Authority
FR
France
Prior art keywords
aircraft
propulsive system
auxiliary propulsive
auxiliary
propulsive
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.)
Active
Application number
FR1653766A
Other languages
English (en)
Other versions
FR3050720A1 (fr
Inventor
Marc Michel Curlier Augustin
Olivier BELMONTE
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1653766A priority Critical patent/FR3050720B1/fr
Publication of FR3050720A1 publication Critical patent/FR3050720A1/fr
Application granted granted Critical
Publication of FR3050720B1 publication Critical patent/FR3050720B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)
FR1653766A 2016-04-28 2016-04-28 Aeronef a au moins un systeme propulsif auxiliaire Active FR3050720B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1653766A FR3050720B1 (fr) 2016-04-28 2016-04-28 Aeronef a au moins un systeme propulsif auxiliaire

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1653766A FR3050720B1 (fr) 2016-04-28 2016-04-28 Aeronef a au moins un systeme propulsif auxiliaire
FR1653766 2016-04-28

Publications (2)

Publication Number Publication Date
FR3050720A1 FR3050720A1 (fr) 2017-11-03
FR3050720B1 true FR3050720B1 (fr) 2018-04-27

Family

ID=56322149

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1653766A Active FR3050720B1 (fr) 2016-04-28 2016-04-28 Aeronef a au moins un systeme propulsif auxiliaire

Country Status (1)

Country Link
FR (1) FR3050720B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11542840B2 (en) 2020-05-04 2023-01-03 Hamilton Sundstrand Corporation Hybrid power generation systems

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3194516A (en) * 1962-10-22 1965-07-13 Messerschmitt Ag Arrangement for jet engines at the tail end of aircraft
FR1472962A (fr) * 1964-08-08 1967-03-17 Dornier Werke Gmbh équipement moteur pour avions
US3997134A (en) * 1975-03-27 1976-12-14 The Boeing Company Fuselage tail jet engine thrust reverser
FR2826056B1 (fr) * 2001-06-14 2003-12-19 Snecma Moteurs Dispositif de propulsion a cycle variable par transmission mecanique pour avion supersonique
US6918244B2 (en) * 2001-08-17 2005-07-19 John Eugene Dickau Vertical takeoff and landing aircraft propulsion systems
GB201117692D0 (en) * 2011-10-13 2011-11-23 Rolls Royce Plc A distributed propulsion system and method of control

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11542840B2 (en) 2020-05-04 2023-01-03 Hamilton Sundstrand Corporation Hybrid power generation systems

Also Published As

Publication number Publication date
FR3050720A1 (fr) 2017-11-03

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