FR2893367A1 - Dispositif de securisation d'un insert dans une structure - Google Patents
Dispositif de securisation d'un insert dans une structure Download PDFInfo
- Publication number
- FR2893367A1 FR2893367A1 FR0553493A FR0553493A FR2893367A1 FR 2893367 A1 FR2893367 A1 FR 2893367A1 FR 0553493 A FR0553493 A FR 0553493A FR 0553493 A FR0553493 A FR 0553493A FR 2893367 A1 FR2893367 A1 FR 2893367A1
- Authority
- FR
- France
- Prior art keywords
- hole
- rod
- head
- piece
- main body
- 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.)
- Granted
Links
- 239000011324 bead Substances 0.000 claims description 10
- 230000000903 blocking effect Effects 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 229910000831 Steel Inorganic materials 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 229910001026 inconel Inorganic materials 0.000 claims description 2
- 229910001220 stainless steel Inorganic materials 0.000 claims description 2
- 239000010935 stainless steel Substances 0.000 claims description 2
- 239000010959 steel Substances 0.000 claims description 2
- 210000005069 ears Anatomy 0.000 description 5
- 239000002184 metal Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
- F16B21/10—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings by separate parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C11/00—Pivots; Pivotal connections
- F16C11/02—Trunnions; Crank-pins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/43—Aeroplanes; Helicopters
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Abstract
Description
Claims (9)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0553493A FR2893367B1 (fr) | 2005-11-17 | 2005-11-17 | Dispositif de securisation d'un insert dans une structure |
US11/561,171 US7681854B2 (en) | 2005-11-17 | 2006-11-17 | Device for securing an insert in a structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0553493A FR2893367B1 (fr) | 2005-11-17 | 2005-11-17 | Dispositif de securisation d'un insert dans une structure |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2893367A1 true FR2893367A1 (fr) | 2007-05-18 |
FR2893367B1 FR2893367B1 (fr) | 2007-12-21 |
Family
ID=36655106
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0553493A Active FR2893367B1 (fr) | 2005-11-17 | 2005-11-17 | Dispositif de securisation d'un insert dans une structure |
Country Status (2)
Country | Link |
---|---|
US (1) | US7681854B2 (fr) |
FR (1) | FR2893367B1 (fr) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2891804B1 (fr) * | 2005-10-12 | 2009-05-01 | Airbus France Sas | Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme |
FR2915176B1 (fr) * | 2007-04-20 | 2009-07-10 | Airbus France Sa | Mat d'accrochage de moteur pour aeronef disposant d'une attache moteur arriere pourvue d'un ecrou a barillet |
WO2008150202A1 (fr) * | 2007-06-08 | 2008-12-11 | Volvo Aero Corporation | Structure de transfert de charges au niveau d'une turbine à gaz, et turbine et aéronef comportant une telle structure |
CN103032434B (zh) * | 2012-11-26 | 2016-05-04 | 中国商用飞机有限责任公司 | 破损安全保险销 |
US9587668B2 (en) * | 2013-03-12 | 2017-03-07 | Harnischfeger Technologies, Inc. | Pin retention system |
CN104613061B (zh) | 2013-11-01 | 2018-09-04 | 空中客车简化股份公司 | 承弯接头和飞行器 |
GB201417202D0 (en) * | 2014-09-30 | 2014-11-12 | Rolls Royce Plc | Gas Turbine Engine Mounting Arrangement |
US11441592B2 (en) * | 2018-05-16 | 2022-09-13 | Raytheon Technologies Corporation | Anti-rotation device for fasteners |
FR3091520A1 (fr) * | 2019-01-09 | 2020-07-10 | Airbus Operations (S.A.S.) | Attache-moteur d’aéronef comprenant au moins un système d’immobilisation en translation d’un pion de cisaillement comportant une plaque d’obturation, procédé de montage de ladite attache-moteur et aéronef comprenant ladite attache-moteur |
FR3094346A1 (fr) * | 2019-03-26 | 2020-10-02 | Airbus Operations | Ensemble pour un aeronef, l’ensemble comportant un mat, une attache moteur et un systeme de fixation entre le mat et l’attache moteur |
CN110937119A (zh) * | 2019-12-24 | 2020-03-31 | 肇庆市海特复合材料技术研究院 | 一种一体式全复合材料连杆结构 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4065077A (en) * | 1976-04-30 | 1977-12-27 | Rolls-Royce Limited | Attachment for attaching jet propulsion engines to fixed structure |
EP0309129A1 (fr) * | 1987-09-18 | 1989-03-29 | British Aerospace Public Limited Company | Unités de construction avec écrou de sécurité |
DE19905299A1 (de) * | 1998-02-11 | 1999-08-12 | Bolt Norge A S | Anordnung bei Lagerzapfen |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1379606A (en) * | 1919-12-26 | 1921-05-31 | Chauncey E Ashley | Locking-socket |
US3923349A (en) * | 1973-06-25 | 1975-12-02 | Lord Corp | Universal bearing support |
US3965954A (en) * | 1975-02-19 | 1976-06-29 | Industrial Innovations, Inc. | Anti-rotational device for bolts and nuts |
US4494710A (en) * | 1983-11-02 | 1985-01-22 | Harris Michael J | Reel brake apparatus |
US6000891A (en) * | 1998-09-25 | 1999-12-14 | Cowell, Jr.; Franklin D. | Combination nut and threaded fastener with locking pin |
-
2005
- 2005-11-17 FR FR0553493A patent/FR2893367B1/fr active Active
-
2006
- 2006-11-17 US US11/561,171 patent/US7681854B2/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4065077A (en) * | 1976-04-30 | 1977-12-27 | Rolls-Royce Limited | Attachment for attaching jet propulsion engines to fixed structure |
EP0309129A1 (fr) * | 1987-09-18 | 1989-03-29 | British Aerospace Public Limited Company | Unités de construction avec écrou de sécurité |
DE19905299A1 (de) * | 1998-02-11 | 1999-08-12 | Bolt Norge A S | Anordnung bei Lagerzapfen |
Also Published As
Publication number | Publication date |
---|---|
FR2893367B1 (fr) | 2007-12-21 |
US20080042007A1 (en) | 2008-02-21 |
US7681854B2 (en) | 2010-03-23 |
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Legal Events
Date | Code | Title | Description |
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CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
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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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PLFP | Fee payment |
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PLFP | Fee payment |
Year of fee payment: 19 |