BR9305531A - Conjunto estrutural, e, nacela de aeromotor - Google Patents

Conjunto estrutural, e, nacela de aeromotor

Info

Publication number
BR9305531A
BR9305531A BR9305531A BR9305531A BR9305531A BR 9305531 A BR9305531 A BR 9305531A BR 9305531 A BR9305531 A BR 9305531A BR 9305531 A BR9305531 A BR 9305531A BR 9305531 A BR9305531 A BR 9305531A
Authority
BR
Brazil
Prior art keywords
nacelle
engine
structural assembly
structural
assembly
Prior art date
Application number
BR9305531A
Other languages
English (en)
Inventor
Michael John Arnold
Kenneth Henry Johnson
Brian Joseph Hall
Original Assignee
Short Brothers Plc
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
Priority claimed from GB929210997A external-priority patent/GB9210997D0/en
Priority claimed from GB929212666A external-priority patent/GB9212666D0/en
Application filed by Short Brothers Plc filed Critical Short Brothers Plc
Publication of BR9305531A publication Critical patent/BR9305531A/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
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B41/00—Locks with visible indication as to whether the lock is locked or unlocked
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S292/00—Closure fasteners
    • Y10S292/49—Toggle catches
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S292/00—Closure fasteners
    • Y10S292/65—Emergency or safety
    • 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
    • Y10T292/00—Closure fasteners
    • Y10T292/20—Clamps
    • Y10T292/205—Ring
    • Y10T292/212—With expanding or contracting means
    • Y10T292/216—Toggle lever

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Alarm Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Lock And Its Accessories (AREA)
  • Emergency Lowering Means (AREA)
  • Fluid-Damping Devices (AREA)
  • Circuit For Audible Band Transducer (AREA)
  • Telephone Function (AREA)
BR9305531A 1992-05-22 1993-05-20 Conjunto estrutural, e, nacela de aeromotor BR9305531A (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB929210997A GB9210997D0 (en) 1992-05-22 1992-05-22 Closure default indicator
GB929212666A GB9212666D0 (en) 1992-06-15 1992-06-15 Closure default indicator
PCT/GB1993/001032 WO1993024368A1 (en) 1992-05-22 1993-05-20 Closure default indicator

Publications (1)

Publication Number Publication Date
BR9305531A true BR9305531A (pt) 1994-11-22

Family

ID=26300923

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9305531A BR9305531A (pt) 1992-05-22 1993-05-20 Conjunto estrutural, e, nacela de aeromotor

Country Status (9)

Country Link
US (1) US5518206A (pt)
EP (1) EP0596070B1 (pt)
JP (1) JPH06509305A (pt)
AU (1) AU665424B2 (pt)
BR (1) BR9305531A (pt)
CA (1) CA2113619A1 (pt)
DE (1) DE69303253D1 (pt)
IL (1) IL105775A0 (pt)
WO (1) WO1993024368A1 (pt)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
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FR2765917B1 (fr) * 1997-07-10 1999-08-20 Hispano Suiza Sa Inverseur de poussee a visualisation de verrouillage
US5915765A (en) * 1998-03-17 1999-06-29 The Boeing Company Opposing hook latch
US6279971B1 (en) * 1999-10-05 2001-08-28 Hartwell Corporation Latch with sensor
FR2800707B1 (fr) 1999-11-10 2002-01-18 Aerospatiale Matra Airbus Indicateur de defaut de fermeture, notamment pour des capots de nacelle d'un moteur d'avion
US6325428B1 (en) * 1999-11-10 2001-12-04 Hartwell Corporation Latch assembly including sensor
US6625972B1 (en) * 2001-08-30 2003-09-30 The Boeing Company Thrust reverser sleeve lock
FR2832752B1 (fr) 2001-11-27 2004-08-06 Airbus France Dispositif indicateur de defaut de fermeture d'au moins un mecanisme de verrouillage interpose entre deux elements
US6517027B1 (en) 2001-12-03 2003-02-11 Pratt & Whitney Canada Corp. Flexible/fixed support for engine cowl
FR2835870B1 (fr) 2002-02-14 2005-03-11 Airbus France Systeme de fermeture interpose entre deux elements
FR2907759B1 (fr) * 2006-10-31 2008-12-12 Aircelle Sa Nacelle pour turboreacteur a ouverture laterale
FR2916426B1 (fr) * 2007-05-22 2010-04-02 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.
US7843363B2 (en) * 2007-07-12 2010-11-30 Rosemount Aerospace Inc. Mechanical latch locking detection sensors
FR2920171B1 (fr) * 2007-08-20 2017-01-13 Aircelle Sa Dispositif de verrouillage concu pour etre dispose dans une zone de jonction d'une nacelle
FR2920144B1 (fr) * 2007-08-20 2010-01-08 Aircelle Sa Nacelle equipee d'un dispositif de detection de l'etat de verrouillage d'un dispositif de verrouillage
US7661321B2 (en) 2007-09-25 2010-02-16 Rosemount Aerospace Inc. Force sensing clevis insert
US8419088B2 (en) * 2007-12-17 2013-04-16 Avibank Manufacturing, Inc. Latches and latching systems having a positive status indicator
US20090173823A1 (en) * 2008-01-07 2009-07-09 Rohr, Inc. Method and component for determining load on a latch assembly
ES2359305B1 (es) * 2008-07-09 2012-03-23 Eads Construcciones Aeronauticas, S.A. Dispositivo para una unidad de propulsión de una aeronave.
US8607640B2 (en) 2010-07-19 2013-12-17 Odd Harald Steen Eriksen Sensor for measuring large mechanical strains in shear or lateral translation
US8627727B2 (en) 2010-07-19 2014-01-14 United Technologies Corporation Sensor for measuring large mechanical strains with fine adjustment device
US8359932B2 (en) 2010-07-19 2013-01-29 Goodrich Corporation Systems and methods for mounting landing gear strain sensors
US8933713B2 (en) 2010-07-19 2015-01-13 Goodrich Corporation Capacitive sensors for monitoring loads
US8659307B2 (en) 2010-08-17 2014-02-25 Rosemount Aerospace Inc. Capacitive sensors for monitoring load bearing on pins
US8286508B2 (en) 2010-07-19 2012-10-16 Goodrich Corporation Systems and methods for measuring angular motion
US10131419B2 (en) 2010-10-15 2018-11-20 Goodrich Corporation Systems and methods for detecting landing gear ground loads
FR2966433B1 (fr) * 2010-10-26 2012-12-07 Airbus Operations Sas Capot d'aeronef incorporant des moyens pour limiter les phenomenes d'ecope de type pneumatique
FR2973421B1 (fr) * 2011-03-29 2013-04-05 Aircelle Sa Dispositif de verrouillage a detection mecanique de fermeture et ouverture
US9567097B2 (en) 2012-02-03 2017-02-14 Rosemount Aerospace Inc. System and method for real-time aircraft performance monitoring
US9783315B2 (en) * 2012-02-24 2017-10-10 Rohr, Inc. Nacelle with longitudinal translating cowling and rotatable sleeves
ES2716992T3 (es) 2013-07-22 2019-06-18 Airbus Defence And Space Sa Sistema de seguimiento para el seguimiento de una unidad de bloqueo de un capó de dos partes
FR3015953B1 (fr) 2014-01-02 2016-02-12 Airbus Operations Sas Systeme de verrouillage de capots
FR3016157B1 (fr) 2014-01-07 2018-03-02 Airbus Operations (S.A.S) Nacelle d'aeronef comprenant un dispositif visuel d'alerte de defaut de verrouillage des capots.
WO2016040501A1 (en) 2014-09-09 2016-03-17 Hartwell Corporation Clevis sensing lock
US10081434B2 (en) * 2015-03-12 2018-09-25 Rohr, Inc. Track mounted hold open rod
US10399688B2 (en) * 2016-11-09 2019-09-03 Rohr, Inc. Nacelle latch alignment
US10577115B2 (en) * 2016-12-16 2020-03-03 Rohr, Inc. Nacelle alignment assembly with a multi-piece locator
US10267060B2 (en) * 2016-12-21 2019-04-23 The Boeing Company Apparatuses and methods for cowl latch indication
FR3064601B1 (fr) * 2017-03-30 2021-01-01 Safran Nacelles Nacelle pour turboreacteur reliee au fuselage d'un aeronef, et ensemble propulsif
US10822102B2 (en) * 2017-06-16 2020-11-03 Rohr, Inc. Adjustable length beam between cowl hinges
US11142326B2 (en) * 2018-07-27 2021-10-12 The Boeing Company Mechanism for indicating position of a latch mechanism for an aircraft nacelle
US10906661B2 (en) 2018-11-05 2021-02-02 Rohr, Inc. Nacelle cowl hinge
ES2943140T3 (es) * 2019-02-05 2023-06-09 Airbus Defence & Space Sau Sistema de aviso de estado abierto de una cubierta de ventilador de dos partes
FR3108097B1 (fr) * 2020-03-10 2022-07-29 Safran Aircraft Engines Dispositif de positionnement pour un capot de nacelle d’un ensemble propulsif d’aeronef
CN112173063B (zh) * 2020-09-25 2022-07-15 中国直升机设计研究所 一种与直升机舱门密封的应急窗

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4150802A (en) * 1977-05-31 1979-04-24 The Boeing Company Aircraft engine installation
US4265474A (en) * 1977-12-01 1981-05-05 Hartwell Corporation Flush type rotary drive for latches
US4127215A (en) * 1978-02-06 1978-11-28 Kaiser Aerospace & Electronics Corporation Access port covering device
US4613099A (en) * 1982-02-05 1986-09-23 The Boeing Company Latch signal and cowling structure
US4498823A (en) * 1982-09-29 1985-02-12 The Boeing Company Retractable vertical restraint mechanism for an aircraft cargo system
US4679750A (en) * 1984-06-20 1987-07-14 The Boeing Company Latch system
US4905892A (en) * 1985-08-16 1990-03-06 Fischer Glenn N Damage-resistant mailbox
DE3807067A1 (de) * 1988-03-04 1989-09-14 Messerschmitt Boelkow Blohm Verriegelung fuer eine flugzeugtuer
US5011200A (en) * 1989-11-21 1991-04-30 The Boeing Company Latch with preload indication
FR2667925B1 (fr) * 1990-10-10 1992-12-04 Hispano Suiza Sa Systeme de securite mecanique.
DE9017146U1 (de) * 1990-12-19 1991-03-14 BSH Bosch und Siemens Hausgeräte GmbH, 81669 München Verschlußvorrichtung für eine an einem kastenartigen Behälter angeordnete Tür

Also Published As

Publication number Publication date
JPH06509305A (ja) 1994-10-20
DE69303253D1 (de) 1996-07-25
AU665424B2 (en) 1996-01-04
EP0596070B1 (en) 1996-06-19
WO1993024368A1 (en) 1993-12-09
EP0596070A1 (en) 1994-05-11
US5518206A (en) 1996-05-21
AU4082493A (en) 1993-12-30
CA2113619A1 (en) 1993-12-09
IL105775A0 (en) 1993-09-22

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Legal Events

Date Code Title Description
EE Request for examination
FD5 Application fees: dismissal - article 86 of industrial property law