FR2443380B1 - Dispositif a charniere pour gouvernes, notamment d'avions et d'hydroglisseurs - Google Patents
Dispositif a charniere pour gouvernes, notamment d'avions et d'hydroglisseursInfo
- Publication number
- FR2443380B1 FR2443380B1 FR7926565A FR7926565A FR2443380B1 FR 2443380 B1 FR2443380 B1 FR 2443380B1 FR 7926565 A FR7926565 A FR 7926565A FR 7926565 A FR7926565 A FR 7926565A FR 2443380 B1 FR2443380 B1 FR 2443380B1
- Authority
- FR
- France
- Prior art keywords
- hydroglisters
- governors
- hinged device
- especially aircraft
- aircraft
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
- B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection
-
- 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
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/69—Redundant disconnection blocking means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
- Hinges (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/966,529 US4213587A (en) | 1978-12-04 | 1978-12-04 | Hinge arrangement for control surfaces |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2443380A1 FR2443380A1 (fr) | 1980-07-04 |
| FR2443380B1 true FR2443380B1 (fr) | 1985-07-12 |
Family
ID=25511552
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7926565A Expired FR2443380B1 (fr) | 1978-12-04 | 1979-10-25 | Dispositif a charniere pour gouvernes, notamment d'avions et d'hydroglisseurs |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US4213587A (enExample) |
| JP (1) | JPS5579799A (enExample) |
| BE (1) | BE879654A (enExample) |
| DE (1) | DE2944114A1 (enExample) |
| FR (1) | FR2443380B1 (enExample) |
| GB (1) | GB2039593B (enExample) |
| IT (1) | IT1164026B (enExample) |
Families Citing this family (39)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4305177A (en) * | 1979-11-28 | 1981-12-15 | The Boeing Company | Hinge assembly for controllable surfaces |
| US4335671A (en) * | 1980-07-17 | 1982-06-22 | The Boeing Company | Flap leading edge for hydrofoil vessels and the like |
| US4345538A (en) * | 1980-07-31 | 1982-08-24 | The Boeing Company | Flap flexure retainer/seal for hydrofoil vessels and the like |
| NL8200197A (nl) * | 1982-01-20 | 1983-08-16 | Fokker Bv | Vleugelklepconstructie en vliegtuig, voorzien van zulk een constructie. |
| US4483498A (en) * | 1982-07-14 | 1984-11-20 | Mcdonnell Douglas Corporation | Flight control surface coupling system |
| US4962904A (en) * | 1984-06-07 | 1990-10-16 | The Boeing Company | Transition fitting for high strength composite |
| FR2591557B1 (fr) * | 1985-12-13 | 1988-03-25 | Aerospatiale | Systeme de couplage de deux volets d'une aile d'aeronef, et aile d'aeronef equipee d'un tel systeme |
| US5344103A (en) * | 1992-01-24 | 1994-09-06 | Alliedsignal, Inc. | Actuating system for aircraft wing slat and flap panels |
| FR2718707B1 (fr) * | 1994-04-18 | 1996-07-12 | Aerospatiale | Dispositif de protection d'une charnière de gouverne, notamment pour aéronef. |
| EP0888201B1 (en) * | 1996-03-22 | 2006-05-31 | The Boeing Company | Determinant spar assembly |
| US7509740B2 (en) * | 2001-11-13 | 2009-03-31 | The Boeing Company | Method of manufacturing a wing |
| US6224646B1 (en) * | 1997-10-17 | 2001-05-01 | Manitoba Ltd. | Waste treatment system |
| US7051982B1 (en) * | 1998-03-27 | 2006-05-30 | Bae Systems Plc | Fairing arrangements for aircraft |
| US6227139B1 (en) | 2000-03-16 | 2001-05-08 | The United States Of America As Represented By The Secretary Of The Navy | Control tab assisted lift reducing system for underwater hydrofoil surface |
| RU2187445C1 (ru) * | 2000-12-15 | 2002-08-20 | Открытое акционерное общество "Туполев" | Устройство для соединения закрылков |
| ATE284346T1 (de) | 2001-01-26 | 2004-12-15 | Fischer Adv Components Gmbh | Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl. |
| AT409482B (de) | 2001-01-26 | 2002-08-26 | Fischer Adv Components Gmbh | Einrichtung zum verbinden beweglicher teile mit strukturbauteilen von flugzeugen od. dgl. |
| US6984109B2 (en) * | 2003-12-04 | 2006-01-10 | Sikorsky Aircraft Corporation | Rotor blade pitch control assembly |
| DE102004035921B4 (de) * | 2004-07-23 | 2006-08-03 | Airbus Deutschland Gmbh | Klappen-Kopplungssystem für Luftfahrzeuge |
| ES2277716B1 (es) * | 2004-12-31 | 2008-05-16 | Airbus España, S.L. | Tapa reforzada para ranuras en un contorno aerodinamico. |
| ES2277715B1 (es) * | 2004-12-31 | 2008-05-16 | Airbus España, S.L. | Tapa reforzada para escotaduras en un contorno aerodinamico. |
| US7316539B2 (en) * | 2005-04-07 | 2008-01-08 | Siemens Power Generation, Inc. | Vane assembly with metal trailing edge segment |
| US20080019832A1 (en) * | 2006-07-10 | 2008-01-24 | Thomas Anderson | Turbine/rotorcraft/oar blade |
| ES2345584B1 (es) * | 2007-12-21 | 2011-07-18 | Airbus Operations, S.L. | Superficie de control de aeronave. |
| RU2375251C2 (ru) * | 2007-12-27 | 2009-12-10 | Закрытое акционерное общество "Гражданские самолеты Сухого" | Устройство герметизации зазора между закрылками |
| GB0807395D0 (en) * | 2008-04-23 | 2008-05-28 | Airbus Uk Ltd | Flight surface seal |
| GB2472759A (en) | 2009-03-17 | 2011-02-23 | Vestas Wind Sys As | Retractable hinge apparatus for wind turbine control surface |
| GB0905818D0 (en) * | 2009-04-06 | 2009-05-20 | Airbus Uk Ltd | Coupling assembly |
| GB0913913D0 (en) * | 2009-08-10 | 2009-09-16 | Airbus Operations Ltd | Pinned lug joint |
| DE102009051983A1 (de) * | 2009-11-05 | 2011-05-12 | Airbus Operations Gmbh | Tragflügel eines Flugzeugs |
| DE102010006447A1 (de) | 2010-02-01 | 2011-08-04 | Airbus Operations GmbH, 21129 | Verbindungsvorrichtung |
| KR101234218B1 (ko) * | 2010-06-25 | 2013-02-18 | 국방과학연구소 | 비행체의 날개장치 및 이를 구비하는 비행체 |
| US9090326B2 (en) * | 2010-10-13 | 2015-07-28 | The Boeing Company | Active flow control on a vertical stabilizer and rudder |
| JP5956803B2 (ja) * | 2012-03-29 | 2016-07-27 | 一般社団法人日本航空宇宙工業会 | 飛行体の高揚力装置 |
| GB201315341D0 (en) * | 2013-08-29 | 2013-10-09 | Airbus Operations Ltd | An aircraft structure and method of manufacture |
| US10562619B2 (en) * | 2015-01-07 | 2020-02-18 | Sikorsky Aircraft Corporation | Main rotor trim tab retention system, an aircraft employing same and a method of replacing a trim tab assembly from blade housing |
| US10532805B2 (en) * | 2016-09-20 | 2020-01-14 | Gulfstream Aerospace Corporation | Airfoil for an aircraft having reduced noise generation |
| JP2020500761A (ja) | 2016-11-11 | 2020-01-16 | エアロバイロメント, インコーポレイテッドAerovironment, Inc. | 押出成形された翼の保護システム及び装置 |
| US20220266998A1 (en) * | 2021-02-19 | 2022-08-25 | Lilium Eaircraft Gmbh | Aircraft |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE469690C (de) * | 1928-12-19 | Daimler Benz Akt Ges | Langgestrecktes Querruder aus mehreren Teilflaechen | |
| US619356A (en) * | 1899-02-14 | Charles ii | ||
| FR519911A (fr) * | 1915-01-08 | 1921-06-17 | Ago Flugzeugwerke G M B H | Système de montage à billes pour plans directeurs des appareils d'aviation |
| FR509630A (fr) * | 1919-04-04 | 1920-11-16 | Jean Jules Marie Antoine Eugen | Dispositif pour l'articulation entre les ailes ou plans d'empennage et les ailerons d'aéronefs |
| US1911121A (en) * | 1930-11-10 | 1933-05-23 | Henry Weis Mfg Company Inc | Hinge |
| US2295306A (en) * | 1938-08-03 | 1942-09-08 | Tampier Rene | Aircraft |
| US2329133A (en) * | 1941-04-09 | 1943-09-07 | Douglas Aircraft Co Inc | Aircraft construction |
| US2445399A (en) * | 1945-06-14 | 1948-07-20 | Cons Vultee Aircraft Corp | Airplane hinge connection |
| US2850340A (en) * | 1954-04-07 | 1958-09-02 | Gen Motors Corp | Piston pin retainer and method of inserting same |
| US3140066A (en) * | 1962-12-04 | 1964-07-07 | North American Aviation Inc | Multiple pivot mounting means |
-
1978
- 1978-12-04 US US05/966,529 patent/US4213587A/en not_active Expired - Lifetime
-
1979
- 1979-10-22 GB GB7936570A patent/GB2039593B/en not_active Expired
- 1979-10-25 FR FR7926565A patent/FR2443380B1/fr not_active Expired
- 1979-10-26 BE BE1/9589A patent/BE879654A/fr not_active IP Right Cessation
- 1979-10-30 DE DE19792944114 patent/DE2944114A1/de not_active Ceased
- 1979-10-30 IT IT50700/79A patent/IT1164026B/it active
- 1979-10-31 JP JP14115379A patent/JPS5579799A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| FR2443380A1 (fr) | 1980-07-04 |
| IT7950700A0 (it) | 1979-10-30 |
| BE879654A (fr) | 1980-04-28 |
| IT1164026B (it) | 1987-04-08 |
| US4213587A (en) | 1980-07-22 |
| GB2039593A (en) | 1980-08-13 |
| JPS635319B2 (enExample) | 1988-02-03 |
| GB2039593B (en) | 1983-03-02 |
| JPS5579799A (en) | 1980-06-16 |
| DE2944114A1 (de) | 1980-06-26 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| FR2443380B1 (fr) | Dispositif a charniere pour gouvernes, notamment d'avions et d'hydroglisseurs | |
| FR2428763B1 (fr) | Dispositif d'accouplement | |
| BE876552A (fr) | Dispositif d'abrasion | |
| BE878602A (fr) | Dispositif d'inhalation | |
| BE873976A (fr) | Dispositif a ajutage | |
| FR2445892B1 (fr) | Dispositif de retenue d'aubes de turbo-machine | |
| FR2447077B1 (fr) | Unite d'antememoire a dispositif a file d'attente de commandes | |
| BE873601A (fr) | Dispositif d'accouplement | |
| BE876086A (fr) | Dispositif piezo-electrique | |
| FR2339415A1 (fr) | Dispositif d'arret pour ski | |
| FR2341471A1 (fr) | Dispositif d'auto-ajustement pour bogies | |
| BE861445A (fr) | Dispositif d'atterrissage pour aeronefs | |
| FR2427532B1 (fr) | Dispositif anti-reflux | |
| BE879195A (fr) | Dispositif de verification d'identite | |
| FR2340681A1 (fr) | Dispositif d'entrainement pour recolteuse-hacheuse | |
| BE878929A (fr) | Dispositif d'homogeneisation | |
| BE856111A (fr) | Dispositif d'etancheite | |
| FR2342879A1 (fr) | Dispositif d'accouplement pour convoyeur aerien | |
| BE873539R (fr) | Dispositif d'etancheite | |
| FR2417833B1 (fr) | Dispositif d'aimantation supraconducteur perfectionne | |
| BE873811A (fr) | Dispositif inhalateur | |
| FR2337669A1 (fr) | Dispositif d'envoloppes | |
| BE877854A (fr) | Dispositif d'etancheite de sas de haut fourneau | |
| FR2347298A1 (fr) | Dispositif d'envidage | |
| BE858584A (fr) | Dispositif d'enregistrement electroradiographique |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |