BRPI0821699A2 - Nacela de motor turbojato compreendendo sistema de travamento para estrutura de entrada de ar. - Google Patents

Nacela de motor turbojato compreendendo sistema de travamento para estrutura de entrada de ar.

Info

Publication number
BRPI0821699A2
BRPI0821699A2 BRPI0821699-1A BRPI0821699A BRPI0821699A2 BR PI0821699 A2 BRPI0821699 A2 BR PI0821699A2 BR PI0821699 A BRPI0821699 A BR PI0821699A BR PI0821699 A2 BRPI0821699 A2 BR PI0821699A2
Authority
BR
Brazil
Prior art keywords
air inlet
locking system
turbojet engine
inlet structure
engine nacelle
Prior art date
Application number
BRPI0821699-1A
Other languages
English (en)
Inventor
Guy Bernard Vauchel
Stéphane Beilliard
Jean-Philippe Dauguet
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 BRPI0821699A2 publication Critical patent/BRPI0821699A2/pt

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05CBOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
    • E05C19/00Other devices specially designed for securing wings, e.g. with suction cups
    • E05C19/10Hook fastenings; Fastenings in which a link engages a fixed hook-like member
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/06Attaching of nacelles, fairings or cowlings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings, or cowlings
    • B64D29/08Inspection panels for power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B47/00Operating or controlling locks or other fastening devices by electric or magnetic means
    • E05B47/0001Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
    • E05B2047/0014Constructional features of actuators or power transmissions therefor
    • E05B2047/0018Details of actuator transmissions
    • E05B2047/0023Nuts or nut-like elements moving along a driven threaded axle
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B47/00Operating or controlling locks or other fastening devices by electric or magnetic means
    • E05B2047/0084Key or electric means; Emergency release
    • E05B2047/0086Emergency release, e.g. key or electromagnet
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B47/00Operating or controlling locks or other fastening devices by electric or magnetic means
    • E05B47/0001Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
    • E05B47/0012Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof with rotary electromotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/70Disassembly methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI0821699-1A 2008-01-18 2008-11-28 Nacela de motor turbojato compreendendo sistema de travamento para estrutura de entrada de ar. BRPI0821699A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0800265A FR2926537B1 (fr) 2008-01-18 2008-01-18 Systeme de verrouillage pour structure d'entree d'air d'une nacelle de turboreacteur
PCT/FR2008/001659 WO2009098402A2 (fr) 2008-01-18 2008-11-28 Système de verrouillage pour structure d'entrée d'air d'une nacelle de turboréacteur

Publications (1)

Publication Number Publication Date
BRPI0821699A2 true BRPI0821699A2 (pt) 2015-06-16

Family

ID=39735405

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0821699-1A BRPI0821699A2 (pt) 2008-01-18 2008-11-28 Nacela de motor turbojato compreendendo sistema de travamento para estrutura de entrada de ar.

Country Status (8)

Country Link
US (1) US8876041B2 (pt)
EP (1) EP2229323A2 (pt)
CN (1) CN101909999B (pt)
BR (1) BRPI0821699A2 (pt)
CA (1) CA2705887C (pt)
FR (1) FR2926537B1 (pt)
RU (1) RU2010133741A (pt)
WO (1) WO2009098402A2 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
US8181905B2 (en) * 2008-12-17 2012-05-22 Rohr, Inc. Aircraft engine nacelle with translating inlet cowl
FR2942457B1 (fr) * 2009-02-24 2011-04-22 Snecma Nacelle de turboreacteur a structure d'entree d'air amovible
FR2961484B1 (fr) * 2010-06-18 2013-01-04 Snecma Manche d?entree d?air pour nacelle de turboreacteur
FR3005100B1 (fr) * 2013-04-26 2015-05-01 Snecma Carter de turbomachine
FR3010051B1 (fr) 2013-08-29 2015-09-11 Aircelle Sa Capot avant pour une nacelle de turboreacteur comportant un systeme de manœuvre
FR3020040B1 (fr) * 2014-04-17 2018-06-29 Societe Lorraine De Construction Aeronautique Ensemble propulsif pour aeronef
US20170283081A1 (en) * 2016-04-05 2017-10-05 Rohr, Inc. Securing a translating fanlet for an aircraft propulsion system nacelle
US10543927B2 (en) * 2016-11-18 2020-01-28 Rohr, Inc. Lockable track system for a translating nacelle structure
FR3075761A1 (fr) * 2017-12-21 2019-06-28 Airbus Operations Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
WO2022203995A1 (en) * 2021-03-24 2022-09-29 Raytheon Company Launch rail transport system
FR3124815A1 (fr) 2021-07-02 2023-01-06 Safran Nacelles Systeme de verrouillage pour nacelle d’aeronef

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2800346A (en) * 1955-12-29 1957-07-23 Avro Aircraft Ltd Hand actuated toggle
US4365775A (en) * 1980-12-08 1982-12-28 The Boeing Company Cowl structure alignment and shear device
US4613099A (en) * 1982-02-05 1986-09-23 The Boeing Company Latch signal and cowling structure
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
FR2765916B1 (fr) * 1997-07-10 1999-08-20 Hispano Suiza Sa Inverseur de poussee a resistance amelioree aux impacts
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
US7252311B2 (en) * 2003-09-17 2007-08-07 Hartwell Corporation Motor driven latch
FR2906568B1 (fr) 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
FR2913062A1 (fr) 2007-02-22 2008-08-29 Aircelle Sa Nacelle de turboreacteur a ecoulement ameliore
FR2916425B1 (fr) 2007-05-25 2009-07-03 Aircelle Sa Dispositif de verrouillage d'une partie ouvrante de nacelle de turboreacteur par rapport a une partie fixe,et nacelle equipee d'un tel dispositif

Also Published As

Publication number Publication date
US20100314501A1 (en) 2010-12-16
EP2229323A2 (fr) 2010-09-22
RU2010133741A (ru) 2012-02-27
CA2705887A1 (fr) 2009-08-13
FR2926537B1 (fr) 2010-02-12
CA2705887C (fr) 2016-01-19
WO2009098402A2 (fr) 2009-08-13
CN101909999B (zh) 2014-09-24
FR2926537A1 (fr) 2009-07-24
US8876041B2 (en) 2014-11-04
WO2009098402A3 (fr) 2009-10-08
CN101909999A (zh) 2010-12-08

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