FR2914363B1 - Systeme de guidage verrouillable pour partie mobile d'une nacelle - Google Patents
Systeme de guidage verrouillable pour partie mobile d'une nacelleInfo
- Publication number
- FR2914363B1 FR2914363B1 FR0702167A FR0702167A FR2914363B1 FR 2914363 B1 FR2914363 B1 FR 2914363B1 FR 0702167 A FR0702167 A FR 0702167A FR 0702167 A FR0702167 A FR 0702167A FR 2914363 B1 FR2914363 B1 FR 2914363B1
- Authority
- FR
- France
- Prior art keywords
- nacelle
- guide system
- mobile part
- lockable guide
- lockable
- 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
Links
- VJYFKVYYMZPMAB-UHFFFAOYSA-N ethoprophos Chemical group CCCSP(=O)(OCC)SCCC VJYFKVYYMZPMAB-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- 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
-
- 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
- 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
- E05F5/00—Braking devices, e.g. checks; Stops; Buffers
- E05F5/003—Braking devices, e.g. checks; Stops; Buffers for sliding wings
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
- E05Y2900/502—Application of doors, windows, wings or fittings thereof for vehicles for aircraft or spacecraft
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/14—Casings or housings protecting or supporting assemblies within
-
- 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
- F05D2260/00—Function
- F05D2260/50—Kinematic linkage, i.e. transmission of position
- F05D2260/52—Kinematic linkage, i.e. transmission of position involving springs
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)
- Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
- Emergency Lowering Means (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0702167A FR2914363B1 (fr) | 2007-03-26 | 2007-03-26 | Systeme de guidage verrouillable pour partie mobile d'une nacelle |
EP08787771A EP2129580A1 (fr) | 2007-03-26 | 2008-03-07 | Système de guidage verrouillable pour partie mobile d'une nacelle |
US12/531,526 US8919693B2 (en) | 2007-03-26 | 2008-03-07 | Lockable guiding system for a mobile part of a nacelle |
PCT/FR2008/000302 WO2008132321A1 (fr) | 2007-03-26 | 2008-03-07 | Système de guidage verrouillable pour partie mobile d'une nacelle |
CA2677567A CA2677567C (fr) | 2007-03-26 | 2008-03-07 | Systeme de guidage verrouillable pour partie mobile d'une nacelle |
BRPI0809417-9A BRPI0809417A2 (pt) | 2007-03-26 | 2008-03-07 | Dispositivo de guia para porção translacionalmente móvel de nacela de motor turbojato e nacela para motor turbojato |
CN200880009913.2A CN101646601B (zh) | 2007-03-26 | 2008-03-07 | 用于发动机机舱活动部件的可锁定引导*** |
RU2009138833/11A RU2460674C2 (ru) | 2007-03-26 | 2008-03-07 | Направляющая система с возможностью блокировки для подвижной части гондолы |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0702167A FR2914363B1 (fr) | 2007-03-26 | 2007-03-26 | Systeme de guidage verrouillable pour partie mobile d'une nacelle |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2914363A1 FR2914363A1 (fr) | 2008-10-03 |
FR2914363B1 true FR2914363B1 (fr) | 2012-07-27 |
Family
ID=38724168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0702167A Active FR2914363B1 (fr) | 2007-03-26 | 2007-03-26 | Systeme de guidage verrouillable pour partie mobile d'une nacelle |
Country Status (8)
Country | Link |
---|---|
US (1) | US8919693B2 (fr) |
EP (1) | EP2129580A1 (fr) |
CN (1) | CN101646601B (fr) |
BR (1) | BRPI0809417A2 (fr) |
CA (1) | CA2677567C (fr) |
FR (1) | FR2914363B1 (fr) |
RU (1) | RU2460674C2 (fr) |
WO (1) | WO2008132321A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2500588C2 (ru) * | 2008-11-13 | 2013-12-10 | Эрсель | Гондола турбореактивного двигателя |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2938237B1 (fr) * | 2008-11-13 | 2011-05-20 | Aircelle Sa | Nacelle pour turboreacteur a capot amont translatable |
US8181905B2 (en) * | 2008-12-17 | 2012-05-22 | Rohr, Inc. | Aircraft engine nacelle with translating inlet cowl |
DE102012213973B4 (de) * | 2012-08-07 | 2022-03-03 | Schaeffler Technologies AG & Co. KG | Montageschiene für einen Führungswagen einer Profilschienen-Wälzführung |
FR3004700B1 (fr) * | 2013-04-19 | 2015-04-03 | Aircelle Sa | Nacelle pour turboreacteur d’aeronef a levre avant etendue |
US20170283081A1 (en) * | 2016-04-05 | 2017-10-05 | Rohr, Inc. | Securing a translating fanlet for an aircraft propulsion system nacelle |
US10738737B2 (en) | 2016-11-18 | 2020-08-11 | Rohr, Inc. | Self-locking alignment at a nacelle interface |
US10543927B2 (en) | 2016-11-18 | 2020-01-28 | Rohr, Inc. | Lockable track system for a translating nacelle structure |
US10436112B2 (en) * | 2017-06-26 | 2019-10-08 | The Boeing Company | Translating turning vanes for a nacelle inlet |
CN107289000B (zh) * | 2017-07-01 | 2023-06-16 | 北方联创通信有限公司 | 角度滑轨连杆装置 |
FR3075761A1 (fr) * | 2017-12-21 | 2019-06-28 | Airbus Operations | Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline |
US11441514B2 (en) * | 2018-10-02 | 2022-09-13 | Woodward, Inc. | Tertiary lock |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2579534A (en) * | 1948-05-12 | 1951-12-25 | United Aircraft Corp | Flap mechanism |
US3480239A (en) * | 1967-02-23 | 1969-11-25 | Tridair Industries | Quick change system |
SU801441A1 (ru) * | 1979-10-02 | 2004-12-10 | И.В. Козлов | Створка гондолы двигателя летательного аппарата |
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 |
US6340135B1 (en) * | 2000-05-30 | 2002-01-22 | Rohr, Inc. | Translating independently mounted air inlet system for aircraft turbofan jet engine |
TW489618U (en) * | 2001-01-05 | 2002-06-01 | King Slide Works Co Ltd | Front-pulling type latch mechanism for rail |
CN2498913Y (zh) * | 2001-01-22 | 2002-07-10 | 川湖工厂股份有限公司 | 滑轨的前拉式栓锁机构 |
US6851774B2 (en) * | 2003-03-06 | 2005-02-08 | King Slide Works Co., Ltd. | Retaining structure for a track device for drawers |
US20060033408A1 (en) * | 2004-08-11 | 2006-02-16 | Nan Juen International Co., Ltd. | Extended rod of slide mechanism for drawer slide track |
FR2890378B1 (fr) * | 2005-09-08 | 2009-01-16 | Airbus France Sas | Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot. |
US7762057B2 (en) * | 2007-06-05 | 2010-07-27 | The Boeing Company | Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
FR2925877B1 (fr) * | 2007-12-26 | 2009-12-04 | Aircelle Sa | Installation de systeme de guidage sur une nacelle d'aeronef. |
-
2007
- 2007-03-26 FR FR0702167A patent/FR2914363B1/fr active Active
-
2008
- 2008-03-07 RU RU2009138833/11A patent/RU2460674C2/ru not_active IP Right Cessation
- 2008-03-07 CA CA2677567A patent/CA2677567C/fr not_active Expired - Fee Related
- 2008-03-07 EP EP08787771A patent/EP2129580A1/fr not_active Withdrawn
- 2008-03-07 BR BRPI0809417-9A patent/BRPI0809417A2/pt not_active IP Right Cessation
- 2008-03-07 WO PCT/FR2008/000302 patent/WO2008132321A1/fr active Application Filing
- 2008-03-07 US US12/531,526 patent/US8919693B2/en not_active Expired - Fee Related
- 2008-03-07 CN CN200880009913.2A patent/CN101646601B/zh not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2500588C2 (ru) * | 2008-11-13 | 2013-12-10 | Эрсель | Гондола турбореактивного двигателя |
Also Published As
Publication number | Publication date |
---|---|
EP2129580A1 (fr) | 2009-12-09 |
US8919693B2 (en) | 2014-12-30 |
CA2677567C (fr) | 2015-06-02 |
CA2677567A1 (fr) | 2008-11-06 |
CN101646601B (zh) | 2013-11-06 |
RU2009138833A (ru) | 2011-05-10 |
CN101646601A (zh) | 2010-02-10 |
WO2008132321A1 (fr) | 2008-11-06 |
US20100031629A1 (en) | 2010-02-11 |
BRPI0809417A2 (pt) | 2014-09-16 |
FR2914363A1 (fr) | 2008-10-03 |
RU2460674C2 (ru) | 2012-09-10 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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CD | Change of name or company name |
Owner name: SAFRAN NACELLES, FR Effective date: 20180125 |
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PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 15 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |