FR2480228A1 - Dispositif de manoeuvre d'un volet d'aile - Google Patents
Dispositif de manoeuvre d'un volet d'aile Download PDFInfo
- Publication number
- FR2480228A1 FR2480228A1 FR8024911A FR8024911A FR2480228A1 FR 2480228 A1 FR2480228 A1 FR 2480228A1 FR 8024911 A FR8024911 A FR 8024911A FR 8024911 A FR8024911 A FR 8024911A FR 2480228 A1 FR2480228 A1 FR 2480228A1
- Authority
- FR
- France
- Prior art keywords
- flap
- wing
- articulated
- rods
- pairs
- 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
- 238000006073 displacement reaction Methods 0.000 claims abstract description 8
- 238000012423 maintenance Methods 0.000 claims abstract description 3
- 230000007246 mechanism Effects 0.000 claims description 25
- 230000005540 biological transmission Effects 0.000 claims description 7
- 238000011144 upstream manufacturing Methods 0.000 claims description 7
- 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
- 238000012544 monitoring process Methods 0.000 claims description 4
- 150000001768 cations Chemical class 0.000 claims 1
- 238000000034 method Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000005339 levitation Methods 0.000 description 2
- WYUYEJNGHIOFOC-VVTVMFAVSA-N 2-[(z)-1-(4-methylphenyl)-3-pyrrolidin-1-ylprop-1-enyl]pyridine;hydrochloride Chemical compound Cl.C1=CC(C)=CC=C1C(\C=1N=CC=CC=1)=C\CN1CCCC1 WYUYEJNGHIOFOC-VVTVMFAVSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000002427 irreversible effect Effects 0.000 description 1
- 230000009467 reduction Effects 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
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/30—Wing lift efficiency
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/20—Control lever and linkage systems
- Y10T74/20576—Elements
- Y10T74/20582—Levers
- Y10T74/20588—Levers toggle
- Y10T74/20594—Lazy tongs
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Steering Controls (AREA)
- Steering Devices For Bicycles And Motorcycles (AREA)
- Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19803013774 DE3013774A1 (de) | 1980-04-10 | 1980-04-10 | Betaetigungsanordnung fuer fluegelklappen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2480228A1 true FR2480228A1 (fr) | 1981-10-16 |
| FR2480228B1 FR2480228B1 (en, 2012) | 1984-06-15 |
Family
ID=6099660
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8024911A Granted FR2480228A1 (fr) | 1980-04-10 | 1980-11-24 | Dispositif de manoeuvre d'un volet d'aile |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US4405105A (en, 2012) |
| DE (1) | DE3013774A1 (en, 2012) |
| FR (1) | FR2480228A1 (en, 2012) |
| GB (1) | GB2073681B (en, 2012) |
Families Citing this family (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4470569A (en) * | 1981-12-28 | 1984-09-11 | Mcdonnell Douglas Corporation | Locking, redundant slat drive mechanism |
| US4784355A (en) * | 1986-11-10 | 1988-11-15 | The United States Of America As Represented By The Secretary Of The Air Force | Flap system for short takeoff and landing aircraft |
| US4872993A (en) * | 1988-02-24 | 1989-10-10 | Harrison George C | Waste treatment |
| US4995575A (en) * | 1988-09-26 | 1991-02-26 | The Boeing Company | Wing trailing edge flap mechanism |
| AU3621695A (en) * | 1994-09-29 | 1996-04-19 | Michael Craig Broadbent | Linkage to deploy a surface relative to a wing |
| US5651513A (en) * | 1995-03-01 | 1997-07-29 | Northrop Grumman Corporation | Linear flap drive system |
| US6010097A (en) * | 1997-10-16 | 2000-01-04 | Northrop Grumman Corporation | Scissor linkage type slotted flap mechanism |
| US6139090A (en) * | 1999-01-25 | 2000-10-31 | Stidd; Robert S. | Adjustable spoiler support for racing car |
| US6974112B2 (en) * | 2003-06-17 | 2005-12-13 | Michael Craig Broadbent | Deployment system for a moveable wing surface |
| DE10328717B3 (de) * | 2003-06-25 | 2004-12-02 | Eads Deutschland Gmbh | Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe |
| DE102005044549B4 (de) * | 2005-09-17 | 2008-04-17 | Eads Deutschland Gmbh | Flugzeugflügel mit ausfahrbarer Nasenklappe |
| GB0805599D0 (en) | 2008-03-28 | 2008-04-30 | Airbus Uk Ltd | Slat deployment mechanism |
| DE102008020654B4 (de) * | 2008-04-24 | 2018-10-04 | Airbus Operations Gmbh | Tragflügel und Flugzeug mit einer Lateral-Kopplungsvorrichtung |
| DE102009037707B4 (de) * | 2009-08-17 | 2013-12-24 | Airbus Operations Gmbh | Verstellmechanismus einer Verstellvorrichtung zur Ankopplung einer Verstellklappe an einen Hauptflügel und eine solche Verstellvorrichtung |
| AU2010314745B2 (en) * | 2009-11-04 | 2016-08-11 | John Mcmurray Clark | A compound motion structure |
| GB0921007D0 (en) | 2009-11-30 | 2010-01-13 | Airbus Operations Ltd | Trailing edge flap |
| GB201011378D0 (en) * | 2010-07-06 | 2010-08-18 | Ultra Electronics Ltd | Linkage for guiding a flexible cable |
| US8449311B2 (en) * | 2010-10-19 | 2013-05-28 | Ppc Broadband, Inc. | Locking audio plug |
| US10059431B2 (en) * | 2011-06-09 | 2018-08-28 | United Technologies Corporation | Method and apparatus for attaching components having dissimilar rates of thermal expansion |
| GB201209686D0 (en) * | 2012-05-31 | 2012-07-18 | Airbus Operations Ltd | A slat support assembly |
| GB201214143D0 (en) * | 2012-08-08 | 2012-09-19 | Airbus Operations Ltd | Slat support and deployment coupling |
| EP2695810B1 (en) | 2012-08-09 | 2016-10-19 | Airbus Operations GmbH | Drive system for control surfaces of an aircraft |
| EP2886451A1 (en) * | 2013-12-18 | 2015-06-24 | Airbus Operations GmbH | Trailing-edge flap system for a wing of an aircraft and aircraft comprising a wing and at least one such trailing-edge flap system |
| US10974816B2 (en) | 2017-09-28 | 2021-04-13 | The Boeing Company | High-fowler flap actuation apparatus and related methods |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2114670A1 (de) * | 1971-03-26 | 1972-10-05 | Vereinigte Flugtechnische Werke-Fokker GmbH, 2800 Bremen | Vorrichtung zum Ausfahren eines Vorflügels aus Tragflächen von Luftfahrzeugen |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1845644A (en) * | 1929-06-20 | 1932-02-16 | Martin W Bardwell | Portable electric saw |
| US2246116A (en) * | 1937-10-28 | 1941-06-17 | Messerschmitt Boelkow Blohm | Airplane wing structure |
| FR858073A (fr) * | 1939-04-18 | 1940-11-16 | Perfectionnements apportés aux surfaces sustentatrices pour aérodynes | |
| US2348150A (en) * | 1941-06-02 | 1944-05-02 | Lockheed Aircraft Corp | Extendible wing flap |
| US2492245A (en) * | 1945-07-25 | 1949-12-27 | Cons Vultee Aircraft Corp | Aircraft control means |
| US2779555A (en) * | 1952-07-05 | 1957-01-29 | Lockheed Aircraft Corp | Wing flap actuating mechanism |
| US2973925A (en) * | 1958-03-24 | 1961-03-07 | Lockheed Aircraft Corp | Aerodynamically automatic airfoil slat mechanism |
| DE2047221C3 (de) * | 1970-09-25 | 1975-07-17 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Tragflügel für Luftfahrzeuge mit einer Doppelspaltlandeklappe |
| GB1400449A (en) * | 1971-09-23 | 1975-07-16 | Lucas Industries Ltd | Actuating arrangements for aircraft control surfaces |
| DE2354420C3 (de) * | 1973-10-31 | 1978-04-06 | Dornier Gmbh, 7990 Friedrichshafen | Klappenbetätigungsanordnung aneinem Tragflügel für Luftfahrzeuge |
| US3986689A (en) * | 1973-12-11 | 1976-10-19 | Lucas Industries Limited | Drive arrangements for aircraft control surfaces |
| US3985319A (en) * | 1975-02-03 | 1976-10-12 | The Boeing Company | Variable pivot trailing edge flap |
| US4305177A (en) * | 1979-11-28 | 1981-12-15 | The Boeing Company | Hinge assembly for controllable surfaces |
-
1980
- 1980-04-10 DE DE19803013774 patent/DE3013774A1/de active Granted
- 1980-11-24 FR FR8024911A patent/FR2480228A1/fr active Granted
-
1981
- 1981-04-06 US US06/250,931 patent/US4405105A/en not_active Expired - Fee Related
- 1981-04-09 GB GB8111244A patent/GB2073681B/en not_active Expired
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2114670A1 (de) * | 1971-03-26 | 1972-10-05 | Vereinigte Flugtechnische Werke-Fokker GmbH, 2800 Bremen | Vorrichtung zum Ausfahren eines Vorflügels aus Tragflächen von Luftfahrzeugen |
Also Published As
| Publication number | Publication date |
|---|---|
| DE3013774A1 (de) | 1981-10-15 |
| GB2073681B (en) | 1984-03-14 |
| FR2480228B1 (en, 2012) | 1984-06-15 |
| GB2073681A (en) | 1981-10-21 |
| DE3013774C2 (en, 2012) | 1991-09-19 |
| US4405105A (en) | 1983-09-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TP | Transmission of property | ||
| ST | Notification of lapse |