FR3088360B1 - LOCKING / RELEASING DEVICE AND AN AIRCRAFT PROPULSIVE NACELLE INCLUDING SUCH A DEVICE - Google Patents
LOCKING / RELEASING DEVICE AND AN AIRCRAFT PROPULSIVE NACELLE INCLUDING SUCH A DEVICE Download PDFInfo
- Publication number
- FR3088360B1 FR3088360B1 FR1860290A FR1860290A FR3088360B1 FR 3088360 B1 FR3088360 B1 FR 3088360B1 FR 1860290 A FR1860290 A FR 1860290A FR 1860290 A FR1860290 A FR 1860290A FR 3088360 B1 FR3088360 B1 FR 3088360B1
- Authority
- FR
- France
- Prior art keywords
- locking
- finger
- unlocking
- support element
- configuration
- 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
- 230000001141 propulsive effect Effects 0.000 title 1
- 238000012423 maintenance Methods 0.000 abstract 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
- E05C3/00—Fastening devices with bolts moving pivotally or rotatively
- E05C3/02—Fastening devices with bolts moving pivotally or rotatively without latching action
- E05C3/04—Fastening devices with bolts moving pivotally or rotatively without latching action with operating handle or equivalent member rigid with the bolt
- E05C3/047—Fastening devices with bolts moving pivotally or rotatively without latching action with operating handle or equivalent member rigid with the bolt rotating about an axis parallel to the surface on which the fastener is mounted
- E05C3/048—Fastening devices with bolts moving pivotally or rotatively without latching action with operating handle or equivalent member rigid with the bolt rotating about an axis parallel to the surface on which the fastener is mounted parallel to the wing edge
-
- 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
- E05B15/00—Other details of locks; Parts for engagement by bolts of fastening devices
- E05B15/02—Striking-plates; Keepers; Bolt staples; Escutcheons
- E05B15/0205—Striking-plates, keepers, staples
- E05B15/022—Striking-plates, keepers, staples movable, resilient or yieldable
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Lock And Its Accessories (AREA)
Abstract
L'invention se rapporte à un dispositif de verrouillage/déverrouillage 1 d'une pièce mobile 2 relativement à une pièce fixe 3. Ce dispositif 1 comprend un verrou 11 et un élément d'appui 12. Le verrou 11 comporte un doigt de verrouillage 111 et un élément de déclenchement 112. Dans une configuration de verrouillage, le doigt 111 coopère avec l'élément d'appui 12 de manière à maintenir la pièce mobile 2 dans une position de fermeture. Dans une configuration de déverrouillage, le doigt 111 et l'élément de déclenchement 112 sont désenclenchés, permettant un déplacement de la pièce mobile 2 relativement à la pièce fixe 3. La structure du verrou 11 est telle que le déverrouillage du dispositif 1 fait passer le doigt 111 par une position angulaire dans laquelle celui-ci écrase l'élément d'appui 12 jusqu'à désenclenchement du doigt 111 et de l'élément de déclenchement 112. Pour permettre un tel déverrouillage tout en assurant un maintien satisfaisant en configuration de verrouillage, l'élément d'appui possède des propriétés élastiques.The invention relates to a locking / unlocking device 1 of a moving part 2 relative to a fixed part 3. This device 1 comprises a latch 11 and a support element 12. The latch 11 comprises a locking finger 111 and a trigger element 112. In a locking configuration, the finger 111 cooperates with the support element 12 so as to maintain the movable part 2 in a closed position. In an unlocking configuration, the finger 111 and the trigger element 112 are disengaged, allowing movement of the movable part 2 relative to the fixed part 3. The structure of the lock 11 is such that the unlocking of the device 1 passes the finger 111 by an angular position in which the latter crushes the support element 12 until the finger 111 and the trigger element 112 release. To allow such unlocking while ensuring satisfactory maintenance in the locking configuration , the support element has elastic properties.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1860290A FR3088360B1 (en) | 2018-11-08 | 2018-11-08 | LOCKING / RELEASING DEVICE AND AN AIRCRAFT PROPULSIVE NACELLE INCLUDING SUCH A DEVICE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1860290A FR3088360B1 (en) | 2018-11-08 | 2018-11-08 | LOCKING / RELEASING DEVICE AND AN AIRCRAFT PROPULSIVE NACELLE INCLUDING SUCH A DEVICE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3088360A1 FR3088360A1 (en) | 2020-05-15 |
FR3088360B1 true FR3088360B1 (en) | 2020-12-25 |
Family
ID=65685693
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1860290A Active FR3088360B1 (en) | 2018-11-08 | 2018-11-08 | LOCKING / RELEASING DEVICE AND AN AIRCRAFT PROPULSIVE NACELLE INCLUDING SUCH A DEVICE |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3088360B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3126001A1 (en) * | 2021-08-03 | 2023-02-10 | Airbus Operations | ASSEMBLY FOR A NACELLE OF AN AIRCRAFT ENGINE, THE SUCH ASSEMBLY COMPRISING A FIXED HOOD AND A HOOD MOBILE MOUNTED ON THE FIXED HOOD |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5638709A (en) * | 1994-04-25 | 1997-06-17 | Clavin; Timothy J. | Trigger latch |
DE202004003707U1 (en) * | 2004-03-10 | 2005-07-28 | Ramsauer, Dieter | Tolerance compensation device for hinged and folding latch |
US8646819B2 (en) * | 2011-10-31 | 2014-02-11 | Alcoa Inc. | Rotary-handle latch |
US9273488B1 (en) * | 2013-07-15 | 2016-03-01 | Avibank Manufacturing, Inc. | Positive locking keeper |
-
2018
- 2018-11-08 FR FR1860290A patent/FR3088360B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3088360A1 (en) | 2020-05-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20200515 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |