FR3008069B1 - Ensemble propulsif pour aeronef comprenant un moteur a helice et un mat monte en amont. - Google Patents

Ensemble propulsif pour aeronef comprenant un moteur a helice et un mat monte en amont.

Info

Publication number
FR3008069B1
FR3008069B1 FR1356700A FR1356700A FR3008069B1 FR 3008069 B1 FR3008069 B1 FR 3008069B1 FR 1356700 A FR1356700 A FR 1356700A FR 1356700 A FR1356700 A FR 1356700A FR 3008069 B1 FR3008069 B1 FR 3008069B1
Authority
FR
France
Prior art keywords
matt
aircraft assembly
propeller engine
propulsive
propulsive aircraft
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
FR1356700A
Other languages
English (en)
Other versions
FR3008069A1 (fr
Inventor
Steve Bedoin
Emmanuel Julliard
Magdi Omais
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1356700A priority Critical patent/FR3008069B1/fr
Publication of FR3008069A1 publication Critical patent/FR3008069A1/fr
Application granted granted Critical
Publication of FR3008069B1 publication Critical patent/FR3008069B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/04—Power-plant nacelles, fairings, or cowlings associated with 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • Y02T50/10—Drag reduction
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1356700A 2013-07-08 2013-07-08 Ensemble propulsif pour aeronef comprenant un moteur a helice et un mat monte en amont. Expired - Fee Related FR3008069B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1356700A FR3008069B1 (fr) 2013-07-08 2013-07-08 Ensemble propulsif pour aeronef comprenant un moteur a helice et un mat monte en amont.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1356700A FR3008069B1 (fr) 2013-07-08 2013-07-08 Ensemble propulsif pour aeronef comprenant un moteur a helice et un mat monte en amont.

Publications (2)

Publication Number Publication Date
FR3008069A1 FR3008069A1 (fr) 2015-01-09
FR3008069B1 true FR3008069B1 (fr) 2017-07-21

Family

ID=49293698

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1356700A Expired - Fee Related FR3008069B1 (fr) 2013-07-08 2013-07-08 Ensemble propulsif pour aeronef comprenant un moteur a helice et un mat monte en amont.

Country Status (1)

Country Link
FR (1) FR3008069B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3032942B1 (fr) 2015-02-19 2018-11-23 Safran Aircraft Engines Ensemble propulsif pour aeronef comprenant un turboreacteur a soufflante non carenee et un pylone d'accrochage

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1310943C (fr) * 1986-04-30 1992-12-01 Walter M. Presz, Jr. Organe a profil aerodynamique
DE102006043462A1 (de) * 2006-09-15 2008-03-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aerodynamisches Bauteil mit einer gewellten Hinterkante
EP2270312A1 (fr) * 2009-07-01 2011-01-05 PEM-Energy Oy Construction aréo- ou hydrodynamique

Also Published As

Publication number Publication date
FR3008069A1 (fr) 2015-01-09

Similar Documents

Publication Publication Date Title
SG11201402937TA (en) Geared turbofan engine with counter-rotating shafts
DK2599540T3 (da) Blandeelement til en statisk blander samt dettes anvendelse
CL2014001461S1 (es) Propulsor para mezclador hidrometalurgico
FR2960520B1 (fr) Aeronef comprenant un moteur de train
EP3052795A4 (fr) Turboréacteur à double flux efficace en poussée
GB201314527D0 (en) Thrust reverser unit
EP2821627A4 (fr) Dispositif de postcombustion et moteur d'aéronef
BR112014009939A2 (pt) dispositivo de reversão de empuxo para uma nacela de motor turbojato e nacela de um motor turbojato
BR112014028731A2 (pt) reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
CL2013002544A1 (es) Simulador de un motor y método para entrenamiento.
BR112015005181A2 (pt) dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
BR112014007961A2 (pt) conjunto de propulsão para aeronave e aeronave
EP2989313A4 (fr) Moteur de turbine à engrenages comportant un conduit en o et un inverseur de poussée
EP2971726A4 (fr) Moteur à double flux à poussée efficace
GB201515665D0 (en) Multiflow turbojet engine fan and turbojet engine fitted with such a fan
EP2971681A4 (fr) Procédés d'assemblage de moteur à double flux
ITTO20110234A1 (it) Dispositivo di contenimento di olio e motore provvisto di tale dispositivo.
BR112016001456A2 (pt) Dispositivo para distribuir levedura em uma padaria e sistema para distribuir levedura em uma padaria
BR112014028771A2 (pt) motor háptico.
EP2973270A4 (fr) Classement de résultats de saisie automatique d'après une cohorte d'entreprise
FR2980117B1 (fr) Engin volant a decollage et atterrissage vertical a rotor contrarotatif
CL2015002776A1 (es) Procedimiento para el aumento de contenido lipido intramuscular en peces de criadero y alimento relacionado.
FR3008069B1 (fr) Ensemble propulsif pour aeronef comprenant un moteur a helice et un mat monte en amont.
BR112015011506A2 (pt) dispositivo reversor de empuxo para nacela de motor turbojato e nacela de motor turbojato.
CO6990685A2 (es) Dispositivo y método para cubrir los paneles falsos de pared con un dispositivo de restauración.

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

ST Notification of lapse

Effective date: 20210305