DE3721479C2 - - Google Patents
Info
- Publication number
- DE3721479C2 DE3721479C2 DE3721479A DE3721479A DE3721479C2 DE 3721479 C2 DE3721479 C2 DE 3721479C2 DE 3721479 A DE3721479 A DE 3721479A DE 3721479 A DE3721479 A DE 3721479A DE 3721479 C2 DE3721479 C2 DE 3721479C2
- Authority
- DE
- Germany
- Prior art keywords
- slat
- wing
- drive
- guide rails
- articulated
- 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 - Lifetime
Links
- 230000005540 biological transmission Effects 0.000 description 2
- 239000000499 gel Substances 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
-
- 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
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
- B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Blinds (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19873721479 DE3721479A1 (de) | 1987-06-30 | 1987-06-30 | Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels |
EP88108852A EP0297304B1 (de) | 1987-06-30 | 1988-06-03 | Betätigungsanordnung für Vorflügel eines Luftfahrzeug Tragflügels |
US07/213,335 US4915327A (en) | 1987-06-30 | 1988-06-30 | Slat actuation and steering |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19873721479 DE3721479A1 (de) | 1987-06-30 | 1987-06-30 | Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3721479A1 DE3721479A1 (de) | 1989-01-19 |
DE3721479C2 true DE3721479C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1990-02-01 |
Family
ID=6330542
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19873721479 Granted DE3721479A1 (de) | 1987-06-30 | 1987-06-30 | Betaetigungsanordnung fuer vorfluegel eines luftfahrzeug-tragfluegels |
Country Status (3)
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2695905B1 (fr) * | 1992-09-24 | 1994-12-16 | Aerospatiale | Bec kruger rigide, pour bord d'attaque de voilure d'aéronef. |
US5927656A (en) * | 1996-06-26 | 1999-07-27 | The Boeing Company | Wing leading edge flap and method therefor |
US6431498B1 (en) * | 2000-06-30 | 2002-08-13 | Philip Watts | Scalloped wing leading edge |
DE10147772C1 (de) * | 2001-09-27 | 2003-09-11 | Siemens Ag | Verfahren zum Betreiben eines Übertragungssystems und Übertragungssystem in einem Energieversorgungsnetz |
US20060038088A1 (en) * | 2004-08-23 | 2006-02-23 | Dodson Robert T | Aircraft wing |
US7249735B2 (en) * | 2005-06-30 | 2007-07-31 | The Boeing Company | Translating conduit apparatus for an airplane or equipment |
EP1757519B1 (en) * | 2005-08-25 | 2010-03-31 | GKN Aerospace Services Limited | Aircraft wing slat |
DE102006053259A1 (de) * | 2006-11-11 | 2008-05-21 | Airbus Deutschland Gmbh | Hochauftriebssystem am Tragflügel eines Flugzeugs und Verfahren zu seiner Betätigung |
GB0700604D0 (en) * | 2007-01-11 | 2007-02-21 | Airbus Uk Ltd | A leading edge structure for an aerofoil |
EP1972547A1 (en) * | 2007-03-21 | 2008-09-24 | Asco Industries | Wing leading edge device |
DE102007020870A1 (de) * | 2007-05-04 | 2008-11-13 | Airbus Deutschland Gmbh | Hochauftriebssystem am Tragflügel eines Flugzeugs |
GB0721284D0 (en) * | 2007-10-31 | 2007-12-12 | Airbus Uk Ltd | Actuation system for leading edge high-lift device |
DE102008050544A1 (de) * | 2008-10-06 | 2010-04-29 | Airbus Deutschland Gmbh | An der Tragfläche eines Flugzeugs angeordneter Vorflügel |
US8534610B1 (en) * | 2009-07-17 | 2013-09-17 | The Boeing Company | Method and apparatus for a leading edge slat on a wing of an aircraft |
US8534611B1 (en) | 2009-07-17 | 2013-09-17 | The Boeing Company | Moveable leading edge device for a wing |
EP3444182B1 (en) * | 2017-08-18 | 2023-01-18 | Airbus Operations GmbH | Wing for an aircraft |
US12179919B2 (en) * | 2023-04-12 | 2024-12-31 | The Boeing Company | Slat movement system for aircraft |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR797675A (fr) * | 1935-05-14 | 1936-05-01 | Handley Page Ltd | Perfectionnements aux mécanismes de commande pour aéronefs |
US3272458A (en) * | 1964-12-08 | 1966-09-13 | Gen Dynamics Corp | Means for positioning a rotating wing slat device |
GB1572004A (en) * | 1978-03-30 | 1980-07-23 | Hawker Siddeley Aviation Ltd | Aircraft wings |
US4202519A (en) * | 1978-09-08 | 1980-05-13 | The Boeing Company | Airfoil leading edge slat apparatus |
DE2916040C2 (de) * | 1979-04-20 | 1986-01-02 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Tragflügel für ein Luftfahrzeug mit beweglichen Vorflügeln |
US4339970A (en) * | 1980-10-10 | 1982-07-20 | Enstrom Rudolph J | Serviceable releasable socket retaining ratchet |
US4399970A (en) * | 1980-11-13 | 1983-08-23 | The Boeing Company | Wing leading edge slat |
US4650140A (en) * | 1985-12-30 | 1987-03-17 | The Boeing Company | Wind edge movable airfoil having variable camber |
-
1987
- 1987-06-30 DE DE19873721479 patent/DE3721479A1/de active Granted
-
1988
- 1988-06-03 EP EP88108852A patent/EP0297304B1/de not_active Expired - Lifetime
- 1988-06-30 US US07/213,335 patent/US4915327A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE3721479A1 (de) | 1989-01-19 |
EP0297304A3 (en) | 1990-02-28 |
US4915327A (en) | 1990-04-10 |
EP0297304B1 (de) | 1992-12-23 |
EP0297304A2 (de) | 1989-01-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OP8 | Request for examination as to paragraph 44 patent law | ||
D2 | Grant after examination | ||
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: DEUTSCHE AIRBUS GMBH, 2000 HAMBURG, DE |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: DEUTSCHE AEROSPACE AIRBUS GMBH, 2000 HAMBURG, DE |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: DAIMLER-BENZ AEROSPACE AIRBUS GMBH, 21129 HAMBURG, |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: DAIMLERCHRYSLER AEROSPACE AIRBUS GMBH, 21129 HAMBU |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: EADS AIRBUS GMBH, 21129 HAMBURG, DE |
|
8327 | Change in the person/name/address of the patent owner |
Owner name: AIRBUS DEUTSCHLAND GMBH, 21129 HAMBURG, DE |