FR3063771B1 - THRUST INVERTER FOR UNDERGROUND TURBOREACTOR UNIT - Google Patents

THRUST INVERTER FOR UNDERGROUND TURBOREACTOR UNIT Download PDF

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Publication number
FR3063771B1
FR3063771B1 FR1751856A FR1751856A FR3063771B1 FR 3063771 B1 FR3063771 B1 FR 3063771B1 FR 1751856 A FR1751856 A FR 1751856A FR 1751856 A FR1751856 A FR 1751856A FR 3063771 B1 FR3063771 B1 FR 3063771B1
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FR
France
Prior art keywords
turbojet
thrust
fuselage
door
turboreactor
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
FR1751856A
Other languages
French (fr)
Other versions
FR3063771A1 (en
Inventor
Philippe Gerard Chanez
Jackie Raymond Julien Prouteau
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR1751856A priority Critical patent/FR3063771B1/en
Publication of FR3063771A1 publication Critical patent/FR3063771A1/en
Application granted granted Critical
Publication of FR3063771B1 publication Critical patent/FR3063771B1/en
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/16—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant
    • 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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Inverseur (15) de poussée monté sur un aéronef (1) pourvu d'un fuselage (3) pour dévier le flux de gaz d'un turboréacteur (2) au moins partiellement enterré équipant cet aéronef (1), ce turboréacteur (2) étant solidaire du fuselage (3) et s'étendant selon un axe (P) de poussée longitudinal, cet inverseur (15) de poussée comprenant une porte (16) montée articulée par rapport au fuselage (3) en aval du turboréacteur (2) entre une position escamotée dans laquelle la porte (16) s'étend longitudinalement pour permettre la circulation des gaz selon l'axe (P) de poussée, et une position déployée dans laquelle la porte (16) s'étend transversalement en regard d'un échappement (14) du turboréacteur (2) pour dévier les gaz de l'axe (P) de poussée (16).Thrust reverser (15) mounted on an aircraft (1) provided with a fuselage (3) for diverting the gas flow from an at least partially buried turbojet (2) equipping this aircraft (1), this turbojet (2) being integral with the fuselage (3) and extending along a longitudinal thrust axis (P), this thrust reverser (15) comprising a door (16) mounted articulated with respect to the fuselage (3) downstream of the turbojet (2) between a retracted position in which the door (16) extends longitudinally to allow the circulation of gases along the thrust axis (P), and a deployed position in which the door (16) extends transversely facing an exhaust (14) from the turbojet (2) to deflect the gases from the thrust axis (P) (16).

FR1751856A 2017-03-07 2017-03-07 THRUST INVERTER FOR UNDERGROUND TURBOREACTOR UNIT Active FR3063771B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1751856A FR3063771B1 (en) 2017-03-07 2017-03-07 THRUST INVERTER FOR UNDERGROUND TURBOREACTOR UNIT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1751856 2017-03-07
FR1751856A FR3063771B1 (en) 2017-03-07 2017-03-07 THRUST INVERTER FOR UNDERGROUND TURBOREACTOR UNIT

Publications (2)

Publication Number Publication Date
FR3063771A1 FR3063771A1 (en) 2018-09-14
FR3063771B1 true FR3063771B1 (en) 2021-04-02

Family

ID=59153027

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1751856A Active FR3063771B1 (en) 2017-03-07 2017-03-07 THRUST INVERTER FOR UNDERGROUND TURBOREACTOR UNIT

Country Status (1)

Country Link
FR (1) FR3063771B1 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3013751A (en) * 1959-12-01 1961-12-19 Ryan Aeronautical Co Combination aerodynamic brake and thrust reverser for jet aircraft
FR1472962A (en) * 1964-08-08 1967-03-17 Dornier Werke Gmbh engine equipment for airplanes
US3997134A (en) * 1975-03-27 1976-12-14 The Boeing Company Fuselage tail jet engine thrust reverser
FR2627806B1 (en) * 1988-02-29 1990-07-20 Fage Etienne DRIVE INVERTER FOR REACTION ENGINE
FR2931799B1 (en) * 2008-05-30 2010-12-24 Airbus France AIRPLANE WITH REAR REACTORS.

Also Published As

Publication number Publication date
FR3063771A1 (en) 2018-09-14

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