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FR2958624B1 - Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence - Google Patents

Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence

Info

Publication number
FR2958624B1
FR2958624B1 FR1052653A FR1052653A FR2958624B1 FR 2958624 B1 FR2958624 B1 FR 2958624B1 FR 1052653 A FR1052653 A FR 1052653A FR 1052653 A FR1052653 A FR 1052653A FR 2958624 B1 FR2958624 B1 FR 2958624B1
Authority
FR
France
Prior art keywords
turbohomoting
aircraft
machine
rear flap
incoming mobile
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
FR1052653A
Other languages
English (en)
Other versions
FR2958624A1 (fr
Inventor
Lionel Diochon
Steve Bedoin
Damien Prat
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 FR1052653A priority Critical patent/FR2958624B1/fr
Priority to US13/078,460 priority patent/US8579230B2/en
Publication of FR2958624A1 publication Critical patent/FR2958624A1/fr
Application granted granted Critical
Publication of FR2958624B1 publication Critical patent/FR2958624B1/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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/04—Power-plant nacelles, fairings or cowlings associated with fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1052653A 2010-04-08 2010-04-08 Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence Expired - Fee Related FR2958624B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1052653A FR2958624B1 (fr) 2010-04-08 2010-04-08 Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence
US13/078,460 US8579230B2 (en) 2010-04-08 2011-04-01 Attachment pylon for aircraft turboshaft engine, comprising rear flaps with mobile incidence

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1052653A FR2958624B1 (fr) 2010-04-08 2010-04-08 Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence

Publications (2)

Publication Number Publication Date
FR2958624A1 FR2958624A1 (fr) 2011-10-14
FR2958624B1 true FR2958624B1 (fr) 2012-06-08

Family

ID=43067061

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1052653A Expired - Fee Related FR2958624B1 (fr) 2010-04-08 2010-04-08 Mat d'accrochage pour turbomoteur d'aeronef, comprenant un volet arriere mobile en incidence

Country Status (2)

Country Link
US (1) US8579230B2 (fr)
FR (1) FR2958624B1 (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2935353B1 (fr) * 2008-09-03 2010-09-10 Airbus France Mat pour la suspension d'un turbomoteur sous une aile d'aeronef
FR2968634B1 (fr) * 2010-12-08 2013-08-02 Snecma Pylone de fixation d'un moteur d'aeronef a helices propulsives non carenees
WO2015010315A1 (fr) 2013-07-26 2015-01-29 Mra Systems, Inc. Mât d'accrochage de moteur pour aéronef
US9533754B2 (en) * 2014-04-19 2017-01-03 The Boeing Company Wing aerial refueling system
US9914528B2 (en) * 2015-02-25 2018-03-13 Embraer S.A. Airframe-integrated propeller-driven propulsion systems
FR3037318B1 (fr) * 2015-06-15 2017-06-30 Snecma Ensemble propulsif pour aeronef comprenant un turboreacteur a soufflante non carenee et un pylone d'accrochage
FR3050721B1 (fr) * 2016-04-28 2018-04-13 Airbus Operations Ensemble moteur pour aeronef comprenant un bord d'attaque de mat integre a une rangee annulaire d'aubes directrices de sortie non carenees
FR3052743B1 (fr) * 2016-06-20 2018-07-06 Airbus Operations Ensemble pour aeronef comprenant des moteurs a propulsion par ingestion de la couche limite
US11111029B2 (en) * 2017-07-28 2021-09-07 The Boeing Company System and method for operating a boundary layer ingestion fan
US10906657B2 (en) * 2018-06-19 2021-02-02 Raytheon Technologies Corporation Aircraft system with distributed propulsion
US10759545B2 (en) 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion
US11613345B2 (en) 2019-05-20 2023-03-28 The Boeing Company Aircraft nacelles having adjustable chines
US11745860B2 (en) 2019-05-20 2023-09-05 The Boeing Company Aircraft nacelles having adjustable chines
US11072416B2 (en) 2019-05-20 2021-07-27 The Boeing Company Aircraft nacelles having adjustable chines
US11235857B2 (en) 2019-05-20 2022-02-01 The Boeing Company Aircraft nacelles having adjustable chines
US11535362B2 (en) 2019-05-20 2022-12-27 The Boeing Company Aircraft nacelles having adjustable chines
US11591097B2 (en) 2019-05-20 2023-02-28 The Boeing Company Aircraft nacelles having adjustable chines
US11873078B2 (en) 2019-05-20 2024-01-16 The Boeing Company Aircraft nacelles having adjustable chines
US11174004B2 (en) * 2019-05-20 2021-11-16 The Boeing Company Aircraft nacelles having adjustable chines

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5088661A (en) * 1986-12-31 1992-02-18 The Boeing Company Aircraft
US4966338A (en) 1987-08-05 1990-10-30 General Electric Company Aircraft pylon
US4979699A (en) * 1989-05-26 1990-12-25 Grumman Aerospace Corporation Flight control augmentation inlet device
US5424950A (en) * 1992-06-02 1995-06-13 Honeywell Inc. Vehicle control surface position feedback compensator for reducing vehicle oscillation
US5779191A (en) 1996-11-12 1998-07-14 Brislawn; Mark G. Pylon flap for increasing negative pitching moments
ES2137092B1 (es) * 1996-11-14 2000-08-16 Munoz Saiz Manuel Flap automatico.
GB0127254D0 (en) * 2001-11-13 2002-01-02 Lucas Industries Ltd Aircraft flight surface control system
FR2935353B1 (fr) * 2008-09-03 2010-09-10 Airbus France Mat pour la suspension d'un turbomoteur sous une aile d'aeronef
US8651426B2 (en) * 2010-07-01 2014-02-18 Rolls-Royce Plc Jet engine installation
US8857761B2 (en) * 2010-10-27 2014-10-14 Ata Engineering, Inc. Variable geometry aircraft pylon structure and related operation techniques
EP2673474B1 (fr) * 2011-03-08 2015-09-16 Bell Helicopter Textron Inc. Aube de rotor reconfigurable

Also Published As

Publication number Publication date
US20110248116A1 (en) 2011-10-13
FR2958624A1 (fr) 2011-10-14
US8579230B2 (en) 2013-11-12

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