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BRPI0814916A2 - "dispositivo de acoplamento e nacela de aeronave" - Google Patents

"dispositivo de acoplamento e nacela de aeronave"

Info

Publication number
BRPI0814916A2
BRPI0814916A2 BRPI0814916A BRPI0814916A2 BR PI0814916 A2 BRPI0814916 A2 BR PI0814916A2 BR PI0814916 A BRPI0814916 A BR PI0814916A BR PI0814916 A2 BRPI0814916 A2 BR PI0814916A2
Authority
BR
Brazil
Prior art keywords
coupling
aircraft
coupling device
aircraft coupling
Prior art date
Application number
Other languages
English (en)
Inventor
Pascal Soulier
Aurelie De Sorbay
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BRPI0814916A2 publication Critical patent/BRPI0814916A2/pt

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
    • B64D29/08—Inspection panels for power plants
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B51/00—Operating or controlling locks or other fastening devices by other non-mechanical means
    • E05B51/02—Operating or controlling locks or other fastening devices by other non-mechanical means by pneumatic or hydraulic means
    • E05B51/023—Operating or controlling locks or other fastening devices by other non-mechanical means by pneumatic or hydraulic means actuated in response to external pressure, blast or explosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/69—Redundant disconnection blocking means
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Body Structure For Vehicles (AREA)
BRPI0814916 2007-08-20 2008-06-20 "dispositivo de acoplamento e nacela de aeronave" BRPI0814916A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0705902A FR2920174A1 (fr) 2007-08-20 2007-08-20 Dispositif de liaison entre les deux demi-coquilles d'une nacelle de moteur d'aeronef, et nacelle equipee d'un tel dispositif
PCT/FR2008/000863 WO2009024661A2 (fr) 2007-08-20 2008-06-20 Dispositif de liaison entre les deux demi-coquilles d'une nacelle de moteur d'aeronef, et nacelle equipee d'un tel dispositif

Publications (1)

Publication Number Publication Date
BRPI0814916A2 true BRPI0814916A2 (pt) 2015-02-03

Family

ID=39233065

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0814916 BRPI0814916A2 (pt) 2007-08-20 2008-06-20 "dispositivo de acoplamento e nacela de aeronave"

Country Status (9)

Country Link
US (1) US20120018005A1 (pt)
EP (1) EP2178756B1 (pt)
CN (1) CN101821164B (pt)
BR (1) BRPI0814916A2 (pt)
CA (1) CA2696461C (pt)
ES (1) ES2400408T3 (pt)
FR (1) FR2920174A1 (pt)
RU (1) RU2460673C2 (pt)
WO (1) WO2009024661A2 (pt)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2973421B1 (fr) * 2011-03-29 2013-04-05 Aircelle Sa Dispositif de verrouillage a detection mecanique de fermeture et ouverture
FR3037039B1 (fr) * 2015-06-03 2017-06-02 Aircelle Sa Dispositif de verrouillage de capots pivotants d’un inverseur de poussee
US11453507B2 (en) * 2018-10-03 2022-09-27 Rohr, Inc. Thrust reverser compression rod engagement apparatus
US11149564B2 (en) 2019-06-24 2021-10-19 Rohr, Inc. Nacelle thrust reverser compression rod supporting system
FR3119648B1 (fr) * 2021-02-05 2023-01-27 Safran Nacelles Inverseur de poussée comprenant des grilles et des capots mobiles assemblés par embrèvement

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2291091A1 (fr) * 1974-11-13 1976-06-11 Snecma Dispositif de montage sur avion d'un turboreacteur
US4549708A (en) * 1982-08-31 1985-10-29 United Technologies Corporation Cowling latch system
US4555078A (en) * 1983-12-27 1985-11-26 Societe Belge D'exploitation De La Navigation Aerienne (Sabena) Apparatus for the suspension of an aircraft engine cowling
US4679750A (en) * 1984-06-20 1987-07-14 The Boeing Company Latch system
US5076514A (en) * 1990-08-03 1991-12-31 The Boeing Company Apparatus for latching two parts together
FR2756323B1 (fr) * 1996-11-28 1998-12-31 Hispano Suiza Sa Dispositif de liaison d'un inverseur de poussee a un turbomoteur
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
FR2771710B1 (fr) * 1997-12-03 2000-02-11 Aerospatiale Dispositif d'ouverture commun a deux capots adjacents de nacelle de moteur d'avion
US6189832B1 (en) * 1998-04-03 2001-02-20 Hartwell Corporation Permanently connected remote latch mechanism
FR2795793B1 (fr) * 1999-07-01 2001-08-03 Snecma Biellette fusible a absorption d'energie
GB0016135D0 (en) * 2000-06-30 2000-08-23 Aerospace Design Facilities Li Safety enhancement method & apparatus
US6629712B2 (en) * 2001-03-30 2003-10-07 Hartwell Corporation Extendable latch
GB0124446D0 (en) * 2001-10-11 2001-12-05 Short Brothers Ltd Aircraft propulsive power unit
US6517027B1 (en) * 2001-12-03 2003-02-11 Pratt & Whitney Canada Corp. Flexible/fixed support for engine cowl
FR2857048B1 (fr) * 2003-07-04 2005-08-26 Snecma Moteurs Verrouillage des capots de nacelle d'un turboreacteur
US8353639B2 (en) * 2005-11-18 2013-01-15 Deere & Company Turnbuckle lock
US8925979B2 (en) * 2006-11-30 2015-01-06 Hartwell Corporation Command latch and pin latch system
FR2920177B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Dispositif de liaison, destine a relier un premier et second elements mobiles l'un par rapport a l'autre
FR2920178B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Dispositif de liaison, destine a relier un premier et un second elements articules l'un par rapport a l'autre

Also Published As

Publication number Publication date
WO2009024661A3 (fr) 2009-04-16
EP2178756A2 (fr) 2010-04-28
FR2920174A1 (fr) 2009-02-27
WO2009024661A2 (fr) 2009-02-26
CN101821164B (zh) 2014-09-03
EP2178756B1 (fr) 2012-11-28
RU2010109776A (ru) 2011-09-27
RU2460673C2 (ru) 2012-09-10
CA2696461C (fr) 2015-06-09
ES2400408T3 (es) 2013-04-09
US20120018005A1 (en) 2012-01-26
CN101821164A (zh) 2010-09-01
CA2696461A1 (fr) 2009-02-26

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]