FR1207944A - Aircraft warping device - Google Patents
Aircraft warping deviceInfo
- Publication number
- FR1207944A FR1207944A FR1207944DA FR1207944A FR 1207944 A FR1207944 A FR 1207944A FR 1207944D A FR1207944D A FR 1207944DA FR 1207944 A FR1207944 A FR 1207944A
- Authority
- FR
- France
- Prior art keywords
- aircraft
- warping device
- warping
- aircraft warping
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
- B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
- B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
- B64C23/072—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices being moveable in their entirety
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/08—Stabilising surfaces mounted on, or supported by, wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C2009/005—Ailerons
-
- 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
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1207944T | 1958-07-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1207944A true FR1207944A (en) | 1960-02-19 |
Family
ID=9674166
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1207944D Expired FR1207944A (en) | 1958-07-29 | 1958-07-29 | Aircraft warping device |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1207944A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3063659A (en) * | 1960-12-23 | 1962-11-13 | Szerda Frank | Safety aircraft |
FR2425379A1 (en) * | 1978-05-08 | 1979-12-07 | Dornier Gmbh | Aircraft control surface actuating gear - has quadrilateral linkage with idler replaced by three link unit with T-link coupled to bell-crank |
US4455004A (en) * | 1982-09-07 | 1984-06-19 | Lockheed Corporation | Flight control device for airplanes |
US5918832A (en) * | 1997-03-14 | 1999-07-06 | General Atomics Aeronautical Systems, Inc. | Wing design using a high-lift center section, augmented by all-moving wing tips and tails |
DE10313290A1 (en) * | 2003-03-25 | 2004-10-21 | Eads Deutschland Gmbh | Wing structure for aircraft, has outer wing that swivels relative to inner wing when it hits certain counter force to reduce high fluid mechanical loads affecting aircraft wing |
WO2019141361A1 (en) | 2018-01-18 | 2019-07-25 | Fleck Future Concepts Gmbh | Space-efficiently stowable, automatably deployable, condensable airplane wing |
-
1958
- 1958-07-29 FR FR1207944D patent/FR1207944A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3063659A (en) * | 1960-12-23 | 1962-11-13 | Szerda Frank | Safety aircraft |
FR2425379A1 (en) * | 1978-05-08 | 1979-12-07 | Dornier Gmbh | Aircraft control surface actuating gear - has quadrilateral linkage with idler replaced by three link unit with T-link coupled to bell-crank |
US4455004A (en) * | 1982-09-07 | 1984-06-19 | Lockheed Corporation | Flight control device for airplanes |
US5918832A (en) * | 1997-03-14 | 1999-07-06 | General Atomics Aeronautical Systems, Inc. | Wing design using a high-lift center section, augmented by all-moving wing tips and tails |
DE10313290A1 (en) * | 2003-03-25 | 2004-10-21 | Eads Deutschland Gmbh | Wing structure for aircraft, has outer wing that swivels relative to inner wing when it hits certain counter force to reduce high fluid mechanical loads affecting aircraft wing |
DE10313290B4 (en) * | 2003-03-25 | 2005-12-29 | Johannes Schweiger | Fluid-mechanically effective surface of a moving in a fluid device, in particular an aircraft, in particular wing or rudder surface of an aircraft |
WO2019141361A1 (en) | 2018-01-18 | 2019-07-25 | Fleck Future Concepts Gmbh | Space-efficiently stowable, automatably deployable, condensable airplane wing |
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