FR3098195B1 - Aircraft comprising at least one cowl associated with a spacer system - Google Patents
Aircraft comprising at least one cowl associated with a spacer system Download PDFInfo
- Publication number
- FR3098195B1 FR3098195B1 FR1907337A FR1907337A FR3098195B1 FR 3098195 B1 FR3098195 B1 FR 3098195B1 FR 1907337 A FR1907337 A FR 1907337A FR 1907337 A FR1907337 A FR 1907337A FR 3098195 B1 FR3098195 B1 FR 3098195B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- cowl
- spacer system
- spacer
- cover
- 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
- 125000006850 spacer group Chemical group 0.000 title abstract 3
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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Wind Motors (AREA)
Abstract
Aéronef comportant au moins un capot associé à un système d’écartement L'invention a pour objet un aéronef comprenant : au moins un capot (22) relié à une structure fixe par un axe de pivotement, mobile par rapport à la structure fixe entre une position ouverte et une position fermée, au moins un mécanisme de verrouillage configuré pour occuper un état verrouillé dans lequel il maintient le capot (22) en position fermée et un état déverrouillé dans lequel il autorise le capot (22) à pivoter au moins un système d’écartement (30) configuré pour pousser le capot (22) dans une position entrouverte lorsque le mécanisme de verrouillage n’est pas correctement verrouillé. Figure 5Aircraft comprising at least one cowl associated with a spacer system The subject of the invention is an aircraft comprising: at least one cowl (22) connected to a fixed structure by a pivot axis, movable with respect to the fixed structure between a open position and a closed position, at least one locking mechanism configured to occupy a locked state in which it maintains the cover (22) in the closed position and an unlocked state in which it allows the cover (22) to pivot at least one system spacer (30) configured to push the hood (22) into a half-open position when the locking mechanism is not properly locked. Figure 5
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1907337A FR3098195B1 (en) | 2019-07-02 | 2019-07-02 | Aircraft comprising at least one cowl associated with a spacer system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1907337 | 2019-07-02 | ||
FR1907337A FR3098195B1 (en) | 2019-07-02 | 2019-07-02 | Aircraft comprising at least one cowl associated with a spacer system |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3098195A1 FR3098195A1 (en) | 2021-01-08 |
FR3098195B1 true FR3098195B1 (en) | 2022-01-21 |
Family
ID=68581917
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1907337A Active FR3098195B1 (en) | 2019-07-02 | 2019-07-02 | Aircraft comprising at least one cowl associated with a spacer system |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3098195B1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2907759B1 (en) * | 2006-10-31 | 2008-12-12 | Aircelle Sa | NACELLE FOR TURBOREACTOR WITH SIDE OPENING |
FR3007390B1 (en) | 2013-06-19 | 2015-07-17 | Airbus Operations Sas | LOCKING MECHANISM OF AN AIRCRAFT HOOD INTEGRATING A SENSOR FOR DETECTING THE UNLOCKED HOOD CONDITION |
FR3008072B1 (en) * | 2013-07-03 | 2017-08-18 | Airbus Operations Sas | NACELLE OF A PROPULSIVE AIRCRAFT ASSEMBLY COMPRISING A HOOD AND A SHUT-OFF MECHANISM OF HOOD SHUTTERS |
FR3012114B1 (en) * | 2013-10-18 | 2017-02-24 | Airbus Operations Sas | PROPELLANT AIRCRAFT ASSEMBLY COMPRISING A BOAT COMPRISING A LOCKING AND CLOSING MECHANISM |
-
2019
- 2019-07-02 FR FR1907337A patent/FR3098195B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3098195A1 (en) | 2021-01-08 |
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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: 20210108 |
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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 |