FR3013682B1 - Structure interne fixe captee - Google Patents

Structure interne fixe captee Download PDF

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Publication number
FR3013682B1
FR3013682B1 FR1461552A FR1461552A FR3013682B1 FR 3013682 B1 FR3013682 B1 FR 3013682B1 FR 1461552 A FR1461552 A FR 1461552A FR 1461552 A FR1461552 A FR 1461552A FR 3013682 B1 FR3013682 B1 FR 3013682B1
Authority
FR
France
Prior art keywords
internal structure
capted
fixed internal
sif
outer sleeve
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
FR1461552A
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English (en)
Other versions
FR3013682A1 (fr
Inventor
Anthony Lacko
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.)
Rohr Inc
Original Assignee
Rohr Inc
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 Rohr Inc filed Critical Rohr Inc
Publication of FR3013682A1 publication Critical patent/FR3013682A1/fr
Application granted granted Critical
Publication of FR3013682B1 publication Critical patent/FR3013682B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • 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
    • F02K1/64—Reversing fan flow
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • 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

Abstract

Un système de propulsion d'un avion comprend une structure interne fixe (SIF) (132, 137) et un manchon externe (465, 460) qui peuvent être couplés séparément à un pylône (110). Par exemple, la structure fixe interne (465, 460) et le manchon extérieur (432, 437) peuvent être amovibles indépendamment l'un par rapport à l'autre. Un verrou unique du système de fermeture (200) divulgué ici peut être configuré pour verrouiller les 4 panneaux (par exemple, les deux moitiés de la SIF (432, 437) et les deux portes du manchon extérieur (465, 460)), ensemble et/ou en une position rapprochée et retenue.
FR1461552A 2013-11-27 2014-11-27 Structure interne fixe captee Active FR3013682B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/092,372 US9366202B2 (en) 2013-11-27 2013-11-27 System and method for captured inner fixed structure

Publications (2)

Publication Number Publication Date
FR3013682A1 FR3013682A1 (fr) 2015-05-29
FR3013682B1 true FR3013682B1 (fr) 2020-10-02

Family

ID=53052562

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1461552A Active FR3013682B1 (fr) 2013-11-27 2014-11-27 Structure interne fixe captee

Country Status (2)

Country Link
US (1) US9366202B2 (fr)
FR (1) FR3013682B1 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014164238A1 (fr) * 2013-03-13 2014-10-09 United Technologies Corporation Verrou de nacelle à commande hydraulique pour moteur à turbine à gaz
US10167741B2 (en) 2015-11-03 2019-01-01 Rohr, Inc. Nacelle fluid drain
FR3054827B1 (fr) * 2016-08-08 2019-08-23 Aircelle Element de fixation pour nacelle de turboreacteur d’aeronef et ensemble propulsif comportant un tel element
US10239628B2 (en) 2016-09-15 2019-03-26 Rohr, Inc. Set of latches with identical components for nacelle doors
US10759541B2 (en) 2016-10-14 2020-09-01 Rohr, Inc. Nacelle bifurcation with leading edge structure
FR3076323B1 (fr) * 2017-12-28 2020-01-10 Safran Nacelles Inverseur de poussee a grilles pour turboreacteur
FR3079878A1 (fr) * 2018-04-05 2019-10-11 Airbus Operations Turboreacteur comportant une nacelle equipee d'un systeme inverseur comportant un capot articule
GB201806564D0 (en) 2018-04-23 2018-06-06 Rolls Royce Plc Gas turbine engine inner barrel
GB201806563D0 (en) 2018-04-23 2018-06-06 Rolls Royce Plc Gas turbine engine keel beam
US11492925B2 (en) * 2018-10-03 2022-11-08 Rohr, Inc. Magnetic fire seal for aircraft nacelle
US11008089B2 (en) * 2018-10-24 2021-05-18 Gulfstream Aerospace Corporation Fireproof pressure relief assembly
US11548653B2 (en) 2019-10-08 2023-01-10 Rohr, Inc. Support structure for inner cowls of an aircraft propulsion system
FR3124815A1 (fr) * 2021-07-02 2023-01-06 Safran Nacelles Systeme de verrouillage pour nacelle d’aeronef

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
GB9120658D0 (en) * 1991-09-27 1991-11-06 Short Brothers Plc Ducted fan turbine engine
FR2772342B1 (fr) * 1997-12-16 2000-02-18 Aerospatiale Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef
US20090173823A1 (en) * 2008-01-07 2009-07-09 Rohr, Inc. Method and component for determining load on a latch assembly
EP2619093B1 (fr) * 2010-09-24 2018-12-05 Short Brothers Plc Nacelle dotée de portes de capot articulées permettant d'accéder au moteur

Also Published As

Publication number Publication date
FR3013682A1 (fr) 2015-05-29
US9366202B2 (en) 2016-06-14
US20150143796A1 (en) 2015-05-28

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