FR3107034B1 - Device for closing an aircraft air inlet intended to participate in checking the tightness of at least one tank of the aircraft. - Google Patents
Device for closing an aircraft air inlet intended to participate in checking the tightness of at least one tank of the aircraft. Download PDFInfo
- Publication number
- FR3107034B1 FR3107034B1 FR2001286A FR2001286A FR3107034B1 FR 3107034 B1 FR3107034 B1 FR 3107034B1 FR 2001286 A FR2001286 A FR 2001286A FR 2001286 A FR2001286 A FR 2001286A FR 3107034 B1 FR3107034 B1 FR 3107034B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- air inlet
- tightness
- participate
- checking
- 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
- 238000001514 detection method Methods 0.000 abstract 1
- 238000005259 measurement Methods 0.000 abstract 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M17/00—Testing of vehicles
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
- G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
- G01M3/32—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators
- G01M3/3209—Details, e.g. container closure devices
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M3/00—Investigating fluid-tightness of structures
- G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
- G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
- G01M3/32—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators
- G01M3/3236—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators by monitoring the interior space of the containers
- G01M3/3272—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors for containers, e.g. radiators by monitoring the interior space of the containers for verifying the internal pressure of closed containers
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Pressure Vessels And Lids Thereof (AREA)
Abstract
- Dispositif d’obturation d’une entrée d’air d’aéronef destiné à participer au contrôle de l’étanchéité d’au moins un réservoir de l’aéronef. - Le dispositif (1) comprend au moins une platine (5) configurée pour être fixée à la porte d’une entrée d’air, la platine (5) comportant au moins un raccordement de mesure (8), un raccordement de sécurité (9) et un raccordement de commande de pression (10). Le dispositif (1) permet de simplifier et de faciliter la mise en place de tests de détection de fuite. Figure pour l'abrégé : Fig. 1- Device for closing an aircraft air inlet intended to participate in checking the tightness of at least one tank of the aircraft. - The device (1) comprises at least one plate (5) configured to be fixed to the door of an air inlet, the plate (5) comprising at least one measurement connection (8), a safety connection ( 9) and a pressure control connection (10). The device (1) makes it possible to simplify and facilitate the implementation of leak detection tests. Figure for the abstract: Fig. 1
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2001286A FR3107034B1 (en) | 2020-02-10 | 2020-02-10 | Device for closing an aircraft air inlet intended to participate in checking the tightness of at least one tank of the aircraft. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2001286 | 2020-02-10 | ||
FR2001286A FR3107034B1 (en) | 2020-02-10 | 2020-02-10 | Device for closing an aircraft air inlet intended to participate in checking the tightness of at least one tank of the aircraft. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3107034A1 FR3107034A1 (en) | 2021-08-13 |
FR3107034B1 true FR3107034B1 (en) | 2022-02-25 |
Family
ID=70008976
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2001286A Active FR3107034B1 (en) | 2020-02-10 | 2020-02-10 | Device for closing an aircraft air inlet intended to participate in checking the tightness of at least one tank of the aircraft. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3107034B1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5117876A (en) * | 1991-04-11 | 1992-06-02 | Spokane Industries, Inc. | Defueling fitting and method for removing fuel from an aircraft fuel cell |
FR2841335B1 (en) * | 2002-06-19 | 2004-09-03 | Helitest Ags | METHOD FOR TESTING THE SEALING OF A TANK OF AN AIRCRAFT AND ASSOCIATED DEVICE FOR FITTING THESE TANKS |
FR3066801B1 (en) * | 2017-05-23 | 2019-12-27 | Airbus Helicopters | SHUTTER FOR SEALING A VENT, MAINTENANCE DEVICE FOR TESTING A SEAL AND ASSOCIATED MAINTENANCE METHOD |
US10782203B2 (en) * | 2018-03-30 | 2020-09-22 | The Boeing Company | Methods and systems for leak detection |
-
2020
- 2020-02-10 FR FR2001286A patent/FR3107034B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3107034A1 (en) | 2021-08-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20210813 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
|
PLFP | Fee payment |
Year of fee payment: 4 |
|
PLFP | Fee payment |
Year of fee payment: 5 |