DE2211248A1 - Klappensystem für Flugzeugtragflügel zur Auftriebserhöhung - Google Patents
Klappensystem für Flugzeugtragflügel zur AuftriebserhöhungInfo
- Publication number
- DE2211248A1 DE2211248A1 DE19722211248 DE2211248A DE2211248A1 DE 2211248 A1 DE2211248 A1 DE 2211248A1 DE 19722211248 DE19722211248 DE 19722211248 DE 2211248 A DE2211248 A DE 2211248A DE 2211248 A1 DE2211248 A1 DE 2211248A1
- Authority
- DE
- Germany
- Prior art keywords
- guide
- flap
- wing
- guide device
- flap system
- 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.)
- Pending
Links
- 230000008878 coupling Effects 0.000 claims description 6
- 238000010168 coupling process Methods 0.000 claims description 6
- 238000005859 coupling reaction Methods 0.000 claims description 6
- 210000002435 tendon Anatomy 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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
- B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Body Structure For Vehicles (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB823671 | 1971-03-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE2211248A1 true DE2211248A1 (de) | 1972-09-14 |
Family
ID=9848591
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19722211248 Pending DE2211248A1 (de) | 1971-03-12 | 1972-03-08 | Klappensystem für Flugzeugtragflügel zur Auftriebserhöhung |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3785594A (enExample) |
| DE (1) | DE2211248A1 (enExample) |
| FR (1) | FR2128856B1 (enExample) |
| GB (1) | GB1339331A (enExample) |
| IT (1) | IT952197B (enExample) |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2804254C2 (de) * | 1978-02-01 | 1985-02-07 | Grob, Burkhart, Dipl.-Ing. ETH, 8023 Großhesselohe | Tragflügel mit Klappe |
| EP0045987A1 (en) * | 1980-08-13 | 1982-02-17 | The Boeing Company | Extendible airfoil cable drum track assembly |
| US4434959A (en) | 1981-09-28 | 1984-03-06 | The Boeing Company | Airfoil flap assembly with flap track member |
| USRE32907E (en) * | 1981-09-28 | 1989-04-18 | The Boeing Company | Airfoil flap assembly with flap track member |
| US5722621A (en) * | 1995-12-05 | 1998-03-03 | The Boeing Company | Bipod load support |
| CN101221433B (zh) * | 2007-12-28 | 2010-10-13 | 中交第二公路工程局有限公司 | 悬索桥主缆缠丝机集成控制系统 |
| GB0810460D0 (en) * | 2008-06-09 | 2008-07-09 | Airbus Uk Ltd | Support assembly |
| GB0810584D0 (en) * | 2008-06-11 | 2008-07-16 | Airbus Uk Ltd | Aircraft wing assembly |
| GB0913473D0 (en) * | 2009-08-04 | 2009-09-16 | Airbus Operations Ltd | Support assembly |
| GB201008773D0 (en) * | 2010-05-26 | 2010-07-14 | Airbus Uk Ltd | Aircraft slat assembly |
| DE102011082888B4 (de) * | 2011-09-16 | 2016-01-07 | Airbus Defence and Space GmbH | Auftriebsklappenanordnung, Tragflügel sowie Flugzeug |
| US8622350B1 (en) * | 2011-11-14 | 2014-01-07 | The Boeing Company | Compound leading edge device for aircraft |
| WO2014209714A1 (en) * | 2013-06-26 | 2014-12-31 | Learjet Inc. | Mechanism for trailing edge control surface |
| FR3011226B1 (fr) * | 2013-09-30 | 2017-05-19 | Airbus Operations Sas | Systeme de volet de bord de fuite hypersustentateur pour voilure d'aeronef. |
| EP2942272A1 (en) * | 2014-05-09 | 2015-11-11 | Airbus Operations GmbH | An aircraft wing and an aircraft comprising such aircraft wing |
| US9868517B2 (en) | 2014-08-13 | 2018-01-16 | The Boeing Company | Rotatable wing tip joint and method of making same |
| GB2533311A (en) * | 2014-12-15 | 2016-06-22 | Airbus Operations Ltd | A track container |
| GB2535488A (en) * | 2015-02-17 | 2016-08-24 | Airbus Operations Ltd | An arrangement for effecting movement of a wing tip device between a flight configuration and a ground configuration |
| GB2535489A (en) | 2015-02-17 | 2016-08-24 | Airbus Operations Ltd | An arrangement for moving a wing tip device between a flight configuration and a ground configuration |
| GB2535580A (en) | 2015-02-17 | 2016-08-24 | Airbus Operations Ltd | Actuation assembly for moving a wing tip device on an aircraft wing |
| US11192627B2 (en) * | 2018-06-18 | 2021-12-07 | Bombardier Inc. | Aircraft wing with deployable flap |
| EP4424592A1 (en) * | 2023-02-28 | 2024-09-04 | Airbus Operations GmbH | Wing for an aircraft |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR802742A (fr) * | 1935-02-26 | 1936-09-14 | Surface portante d'avion | |
| US2405726A (en) * | 1940-08-14 | 1946-08-13 | Edward F Zap | Airplane wing construction |
| US2938680A (en) * | 1957-07-02 | 1960-05-31 | North American Aviation Inc | Multiple position airfoil slat |
| GB1227316A (enExample) * | 1967-05-16 | 1971-04-07 |
-
1971
- 1971-03-12 GB GB823671A patent/GB1339331A/en not_active Expired
-
1972
- 1972-03-08 DE DE19722211248 patent/DE2211248A1/de active Pending
- 1972-03-10 US US00233505A patent/US3785594A/en not_active Expired - Lifetime
- 1972-03-10 FR FR7208513A patent/FR2128856B1/fr not_active Expired
- 1972-03-10 IT IT48903/72A patent/IT952197B/it active
Also Published As
| Publication number | Publication date |
|---|---|
| FR2128856B1 (enExample) | 1977-01-14 |
| FR2128856A1 (enExample) | 1972-10-20 |
| GB1339331A (en) | 1973-12-05 |
| IT952197B (it) | 1973-07-20 |
| US3785594A (en) | 1974-01-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OHJ | Non-payment of the annual fee |