GB1296994A - - Google Patents
Info
- Publication number
- GB1296994A GB1296994A GB2778769A GB1296994DA GB1296994A GB 1296994 A GB1296994 A GB 1296994A GB 2778769 A GB2778769 A GB 2778769A GB 1296994D A GB1296994D A GB 1296994DA GB 1296994 A GB1296994 A GB 1296994A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jack
- skin
- frame
- leading edge
- supported
- 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
- 239000012530 fluid Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/42—Adjusting about chordwise axes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/48—Varying camber by relatively-movable parts of wing structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/52—Warping
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Bridges Or Land Bridges (AREA)
- Body Structure For Vehicles (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2778769 | 1969-06-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1296994A true GB1296994A (enrdf_load_stackoverflow) | 1972-11-22 |
Family
ID=10265314
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2778769A Expired GB1296994A (enrdf_load_stackoverflow) | 1969-06-02 | 1969-06-02 |
Country Status (6)
| Country | Link |
|---|---|
| JP (1) | JPS5431279B1 (enrdf_load_stackoverflow) |
| DE (1) | DE2026054C3 (enrdf_load_stackoverflow) |
| FR (1) | FR2045801B1 (enrdf_load_stackoverflow) |
| GB (1) | GB1296994A (enrdf_load_stackoverflow) |
| NL (1) | NL169849C (enrdf_load_stackoverflow) |
| SE (1) | SE365474B (enrdf_load_stackoverflow) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2000017046A1 (en) * | 1998-09-24 | 2000-03-30 | Raimo Hirvinen | Profile and process for changing the maximum angle of attack of aprofile |
| US6070834A (en) * | 1996-12-21 | 2000-06-06 | Daimlerchrysler Ag | Aerodynamic body with internal actuating drives |
| GB2450236A (en) * | 2007-06-11 | 2008-12-17 | Boeing Co | Aircraft tail having leading edge slat |
| WO2011011161A1 (en) * | 2009-07-21 | 2011-01-27 | The Boeing Company | Shape-changing control surface |
| DE102010024121B4 (de) * | 2010-06-17 | 2017-04-06 | Airbus Defence and Space GmbH | Stellantriebseinheit |
| US10654557B2 (en) | 2014-09-25 | 2020-05-19 | Bombardier Inc. | Morphing skin for an aircraft |
| CN113874284A (zh) * | 2019-02-01 | 2021-12-31 | G·科隆比耶斯 | 具有被动适应性轮廓的承载结构 |
| US11459083B2 (en) | 2019-07-03 | 2022-10-04 | National Research Council Of Canada | Deforming foil structure for bridging curved fluid-dynamic surface |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3816431A1 (de) * | 1988-05-13 | 1989-11-16 | Otilio Nemec | Zwischenstufige kruemmungsvorrichtung fuer aerodynamische steuerflaechen |
| DE19643222C2 (de) * | 1996-10-19 | 1998-12-10 | Daimler Benz Ag | Auftriebskörper mit veränderbarer Wölbung |
| DE19852944C1 (de) * | 1998-11-17 | 2000-02-10 | Daimler Chrysler Ag | Adaptiver Strömungskörper |
| DE19858872C2 (de) | 1998-12-19 | 2001-02-08 | Daimler Chrysler Ag | Adaptiver Flugzeugtragflügel |
| AT408216B (de) | 1999-05-04 | 2001-09-25 | Ofner Anton Gerald Dr | Flugzeugtragflügel |
| EP2883787B1 (de) * | 2013-12-12 | 2019-06-12 | Airbus Defence and Space GmbH | Antriebsmechanismus für eine verformbare Tragflächenvorderkante |
| WO2021037976A1 (en) | 2019-08-30 | 2021-03-04 | Airbus Operations Gmbh | Flow body for an aircraft having an integrated de-icing system |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE445182C (de) * | 1927-06-04 | Hanns Freiherr Schertel Von Bu | Tragflaeche, deren Prolfil waehrend des Flugs veraenderbar ist | |
| GB110031A (en) * | 1916-10-10 | 1917-10-10 | Patent Corp Ltd | Improvements in Flying Machines. |
| FR574803A (fr) * | 1922-12-30 | 1924-07-19 | Perfectionnements apportés à des ailes fluido-dynamiques, variables, telles que les ailes pour aéroplanes | |
| FR922899A (fr) * | 1946-01-14 | 1947-06-20 | Dispositif pour la variation de courbure des surfaces portantes, empennages et surfaces auxiliaires des appareils de locomotion aérienne | |
| US2650047A (en) * | 1949-01-22 | 1953-08-25 | Douglas Aircraft Co Inc | Variable camber wing |
| US3076623A (en) * | 1960-10-19 | 1963-02-05 | Donald G Lyon | Variable shaped airfoil |
| US3179357A (en) * | 1962-02-27 | 1965-04-20 | Donald G Lyon | Variable shaped airfoil |
-
1969
- 1969-06-02 GB GB2778769A patent/GB1296994A/en not_active Expired
-
1970
- 1970-05-27 DE DE2026054A patent/DE2026054C3/de not_active Expired
- 1970-06-01 SE SE07546/70A patent/SE365474B/xx unknown
- 1970-06-01 JP JP4642570A patent/JPS5431279B1/ja active Pending
- 1970-06-02 NL NLAANVRAGE7007986,A patent/NL169849C/xx not_active IP Right Cessation
- 1970-06-02 FR FR707020232A patent/FR2045801B1/fr not_active Expired
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6070834A (en) * | 1996-12-21 | 2000-06-06 | Daimlerchrysler Ag | Aerodynamic body with internal actuating drives |
| WO2000017046A1 (en) * | 1998-09-24 | 2000-03-30 | Raimo Hirvinen | Profile and process for changing the maximum angle of attack of aprofile |
| GB2450236A (en) * | 2007-06-11 | 2008-12-17 | Boeing Co | Aircraft tail having leading edge slat |
| GB2450236B (en) * | 2007-06-11 | 2009-05-20 | Boeing Co | Symmetric leading edge device and method to delay flow separation |
| US7913949B2 (en) | 2007-06-11 | 2011-03-29 | The Boeing Company | Symmetric leading edge device and method to delay flow separation |
| WO2011011161A1 (en) * | 2009-07-21 | 2011-01-27 | The Boeing Company | Shape-changing control surface |
| US8382045B2 (en) | 2009-07-21 | 2013-02-26 | The Boeing Company | Shape-changing control surface |
| DE102010024121B4 (de) * | 2010-06-17 | 2017-04-06 | Airbus Defence and Space GmbH | Stellantriebseinheit |
| US10654557B2 (en) | 2014-09-25 | 2020-05-19 | Bombardier Inc. | Morphing skin for an aircraft |
| CN113874284A (zh) * | 2019-02-01 | 2021-12-31 | G·科隆比耶斯 | 具有被动适应性轮廓的承载结构 |
| US11459083B2 (en) | 2019-07-03 | 2022-10-04 | National Research Council Of Canada | Deforming foil structure for bridging curved fluid-dynamic surface |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5431279B1 (enrdf_load_stackoverflow) | 1979-10-05 |
| NL7007986A (enrdf_load_stackoverflow) | 1970-12-04 |
| NL169849B (nl) | 1982-04-01 |
| DE2026054B2 (de) | 1980-11-06 |
| DE2026054A1 (enrdf_load_stackoverflow) | 1970-12-10 |
| SE365474B (enrdf_load_stackoverflow) | 1974-03-25 |
| FR2045801A1 (enrdf_load_stackoverflow) | 1971-03-05 |
| DE2026054C3 (de) | 1981-08-13 |
| NL169849C (nl) | 1982-09-01 |
| FR2045801B1 (enrdf_load_stackoverflow) | 1974-07-12 |
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| GB1296994A (enrdf_load_stackoverflow) | ||
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| LADSON | Description and calibration of the Langley 6- by 19-inch transonic tunnel(Design and calibration of Langley 6 by 19 inch transonic tunnel for testing two dimensional airfoil sections) | |
| REGAN et al. | Aeroballistic evaluation and computer stability analysis of the US Navy 20-millimeter general purpose projectile(Aeroballistic evaluation and computer stability analysis of general purpose 20-millimeter projectile from ballistics range and wind tunnel measurements) | |
| LORSON | The effects of external stores on the longitudinal static stability of aircraft(Effects of various external stores characteristics, spanwise positions, and Mach number on static longitudinal stability of several military aircraft)[Progress Report, 1 Sep. 1971- 15 Jun. 1972] | |
| Dhawan | Effect of a Griffith crack on the distribution of stress in a semi-infinite two-dimensional medium |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |