BR112015032739A2 - dispositivo de assistência para operar uma capota de uma nacela de motor turbojato articulada e nacela para um motor turbojato ou semelhante - Google Patents

dispositivo de assistência para operar uma capota de uma nacela de motor turbojato articulada e nacela para um motor turbojato ou semelhante

Info

Publication number
BR112015032739A2
BR112015032739A2 BR112015032739A BR112015032739A BR112015032739A2 BR 112015032739 A2 BR112015032739 A2 BR 112015032739A2 BR 112015032739 A BR112015032739 A BR 112015032739A BR 112015032739 A BR112015032739 A BR 112015032739A BR 112015032739 A2 BR112015032739 A2 BR 112015032739A2
Authority
BR
Brazil
Prior art keywords
turbojet engine
nacelle
bonnet
nipple
articulated
Prior art date
Application number
BR112015032739A
Other languages
English (en)
Inventor
Boileau Patrick
Blondeau Samuel
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 BR112015032739A2 publication Critical patent/BR112015032739A2/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
    • 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
    • E05D—HINGES OR SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS
    • E05D7/00—Hinges or pivots of special construction
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F3/00—Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices
    • E05F3/18—Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices with counteracting springs
    • E—FIXED CONSTRUCTIONS
    • E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
    • E05F3/00—Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices
    • E05F3/20—Closers or openers with braking devices, e.g. checks; Construction of pneumatic or liquid braking devices in hinges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
  • Body Structure For Vehicles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Superstructure Of Vehicle (AREA)
  • Pivots And Pivotal Connections (AREA)

Abstract

a presente invenção diz respeito a um dispositivo para auxiliar a manobra de uma tampa de uma nacela de um motor turbojato ou semelhante. o dispositivo de apoio compreende um conjunto colinear com uma junta existente ou articulação para encaixar a tampa (1, 2), o conjunto do dispositivo sendo rigidamente fixados a uma parte angular (13-15) da qual uma extremidade se apoia no encaixe (35, 38) da tampa (1, 2) e de qual um ponto está articulado a uma mola de compressão (17, 27), a fim de aplicar impulso de assistência para o encaixe da tampa, quando a tampa (1, 2) está levantada. aplicação em nacelas de motores turbojato ou similares.
BR112015032739A 2013-07-01 2014-07-01 dispositivo de assistência para operar uma capota de uma nacela de motor turbojato articulada e nacela para um motor turbojato ou semelhante BR112015032739A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1356383A FR3007739B1 (fr) 2013-07-01 2013-07-01 Dispositif d’assistance pour la manœuvre d’un capot et nacelle de turboreacteur ainsi equipee
PCT/FR2014/051689 WO2015001251A1 (fr) 2013-07-01 2014-07-01 Dispositif d'assistance pour la manœuvre d'un capot et nacelle de turboréacteur ainsi équipée

Publications (1)

Publication Number Publication Date
BR112015032739A2 true BR112015032739A2 (pt) 2017-07-25

Family

ID=49293671

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015032739A BR112015032739A2 (pt) 2013-07-01 2014-07-01 dispositivo de assistência para operar uma capota de uma nacela de motor turbojato articulada e nacela para um motor turbojato ou semelhante

Country Status (8)

Country Link
US (1) US20160101871A1 (pt)
EP (1) EP3016861B1 (pt)
CN (1) CN105452105B (pt)
BR (1) BR112015032739A2 (pt)
CA (1) CA2914333A1 (pt)
FR (1) FR3007739B1 (pt)
RU (1) RU2653980C2 (pt)
WO (1) WO2015001251A1 (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3019526B1 (fr) * 2014-04-07 2017-11-24 Airbus Operations Sas Nacelle d'aeronef comportant un systeme d'ecartement destine a maintenir les deux capots ecartes
US10173783B2 (en) * 2016-08-23 2019-01-08 Airbus Helicopters Rotorcraft with cowling able to rotate and translate relative to the fuselage
FR3101675B1 (fr) * 2019-10-08 2024-04-26 Airbus Operations Sas Ensemble de motorisation pour un aeronef comportant un inverseur de poussee manoeuvrable
FR3108581B1 (fr) 2020-03-26 2022-04-01 Airbus Operations Sas Nacelle d’aéronef comportant un capot et un dispositif de verrouillage à commande automatique limitant la déformation du capot

Family Cites Families (32)

* Cited by examiner, † Cited by third party
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US2122327A (en) * 1937-08-25 1938-06-28 Henry W Schwarz Combination door hinge and control
US2515875A (en) * 1947-02-13 1950-07-18 James J Jones Door check
US2551239A (en) * 1950-06-19 1951-05-01 Clayton W Bond Cover for open top trailers
SU290678A1 (ru) * 1969-08-19 1980-01-15 Предприятие Капот двигател летательного аппарата
US4185415A (en) * 1978-04-14 1980-01-29 The Boeing Company Articulated hinge cooperating with an energy storage device capable of automatically opening and holding open an unlatched compartment door
US4286820A (en) * 1979-07-05 1981-09-01 State Wide Aluminum Of Indiana, Inc. Truck cover and door therefor
RU820141C (ru) * 1979-12-18 1995-06-27 Казанское научно-производственное предприятие "Вертолеты-Ми" Механизм подвески створок капота летательного аппарата
US4399966A (en) * 1980-12-31 1983-08-23 The Boeing Company Power opening system for engine cowl doors
FR2512486A1 (fr) * 1981-09-04 1983-03-11 Renault Dispositif d'equilibrage de hayon de vehicule automobile
US4585189A (en) * 1984-10-22 1986-04-29 Lockheed Corporation Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor
US4627590A (en) * 1984-12-03 1986-12-09 The Boeing Company Stowage receiver for fixed length rod
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
US5110021A (en) * 1989-09-13 1992-05-05 Dawson Jr Fredric O Combination pipe rack and tool locker for a truck bed
US5213286A (en) * 1990-10-10 1993-05-25 General Electric Company Door for aircraft nacelle
FR2673972B1 (fr) * 1991-03-12 1993-07-23 Aerospatiale Porte d'acces, notamment pour nacelle de reacteur d'avion, munie d'un panneau articule a pivotement synchronise.
US5203525A (en) * 1991-10-23 1993-04-20 Rohr, Inc. Hinge with offset pivot line
US5704569A (en) * 1995-05-12 1998-01-06 The Boeing Company Counterbalance mechanism for inwardly and upwardly opening plug-type airplane cargo doors
US5593203A (en) * 1995-06-08 1997-01-14 Abbott; Jay D. Retrofitted door for open luggage rack on passenger busses
FR2756323B1 (fr) * 1996-11-28 1998-12-31 Hispano Suiza Sa Dispositif de liaison d'un inverseur de poussee a un turbomoteur
FR2771710B1 (fr) * 1997-12-03 2000-02-11 Aerospatiale Dispositif d'ouverture commun a deux capots adjacents de nacelle de moteur d'avion
US6041548A (en) * 1998-06-25 2000-03-28 A. L. Hanson Mfg. Co. Support arm
DE10020825B4 (de) * 2000-04-28 2006-08-24 Eurocopter Deutschland Gmbh Verfahren und Vorrichtung zum Schliessen einer Tür eines Flugzeuges
GB0124446D0 (en) * 2001-10-11 2001-12-05 Short Brothers Ltd Aircraft propulsive power unit
GB0320371D0 (en) * 2003-08-29 2003-10-01 Rolls Royce Plc A closure panel arrangement
FR2914700B1 (fr) * 2007-04-04 2009-05-22 Aircelle Sa Inverseur de poussee pour moteur a reaction
FR2920145B1 (fr) * 2007-08-20 2009-09-18 Aircelle Sa Nacelle de turboreacteur a amortisseurs pour demi-coquilles
FR2920134B1 (fr) * 2007-08-20 2010-02-26 Aircelle Sa Nacelle equipee d'au moins une trappe de surpression
US20100037528A1 (en) * 2007-10-18 2010-02-18 Michael Lambright Cargo door/ramp lift assist system
US20100024161A1 (en) * 2008-06-09 2010-02-04 Marathonnorco Aerospace, Inc. Hold Open Rod
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
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US9221545B2 (en) * 2013-04-03 2015-12-29 The Boeing Company Aircraft nacelle assemblies

Also Published As

Publication number Publication date
RU2653980C2 (ru) 2018-05-15
RU2016102800A3 (pt) 2018-03-26
US20160101871A1 (en) 2016-04-14
FR3007739A1 (fr) 2015-01-02
EP3016861B1 (fr) 2017-05-31
CN105452105B (zh) 2018-04-20
WO2015001251A1 (fr) 2015-01-08
RU2016102800A (ru) 2017-08-04
CN105452105A (zh) 2016-03-30
FR3007739B1 (fr) 2016-02-05
EP3016861A1 (fr) 2016-05-11
CA2914333A1 (fr) 2015-01-08

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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]

Free format text: REFERENTE A 5A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO ARQUIVAMENTO PUBLICADO NA RPI 2521 DE 30/04/2019.

B350 Update of information on the portal [chapter 15.35 patent gazette]