GB407009A - Improvements in or connected with cantilever wings for aircraft - Google Patents
Improvements in or connected with cantilever wings for aircraftInfo
- Publication number
- GB407009A GB407009A GB24942/32A GB2494232A GB407009A GB 407009 A GB407009 A GB 407009A GB 24942/32 A GB24942/32 A GB 24942/32A GB 2494232 A GB2494232 A GB 2494232A GB 407009 A GB407009 A GB 407009A
- Authority
- GB
- United Kingdom
- Prior art keywords
- angle
- spar
- wing
- aileron
- adjusted
- 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
- 230000000994 depressogenic effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Abstract
407,009. Aircraft wings. VICKERS (AVIATION), Ltd., and WALLIS, B. N., Byfleet Road, Weybridge, Surrey. Sept. 7, 1932, No. 24942. [Class 4.] To counteract twist on a cantilever wing when an aileron is depressed the outboard portion carrying the aileron is swept forwardly at an angle to the inboard portion, and this angle may be adjustable. A single spar wing is shown having the inner portion of the spar set at right angles to the fuselage and the outer portion set at 9‹ forward of it. The outer portion may be made relatively longer and set at a smaller angle such as 7¢‹. The inner portion of the spar may alternatively be inclined forwardly or rearwardly. To enable the angle between the inner and outer portions to be adjusted the spars may be connected at a deep joint h<4>, Fig. 3, and adjusted from the cockpit by the screw gear shown. Filling pieces k, k<1> fill the gaps between the adjacent edges of the wing portions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB24942/32A GB407009A (en) | 1932-09-07 | 1932-09-07 | Improvements in or connected with cantilever wings for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB24942/32A GB407009A (en) | 1932-09-07 | 1932-09-07 | Improvements in or connected with cantilever wings for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB407009A true GB407009A (en) | 1934-03-07 |
Family
ID=10219716
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB24942/32A Expired GB407009A (en) | 1932-09-07 | 1932-09-07 | Improvements in or connected with cantilever wings for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB407009A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014074182A1 (en) * | 2012-07-20 | 2014-05-15 | Icon Aircraft, Inc. | Spin resistant aircraft configuration |
-
1932
- 1932-09-07 GB GB24942/32A patent/GB407009A/en not_active Expired
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014074182A1 (en) * | 2012-07-20 | 2014-05-15 | Icon Aircraft, Inc. | Spin resistant aircraft configuration |
| CN104203748A (en) * | 2012-07-20 | 2014-12-10 | 图标飞机制造公司 | Spin resistant aircraft configuration |
| US9327828B2 (en) | 2012-07-20 | 2016-05-03 | Icon Aircraft, Inc. | Spin resistant aircraft configuration |
| CN104203748B (en) * | 2012-07-20 | 2016-08-24 | 图标飞机制造公司 | The aircaft configuration of anti-spin |
| RU2640669C2 (en) * | 2012-07-20 | 2018-01-11 | Айкон Айркрафт, Инк. | Aircraft configuration having spin resistance |
| US9926071B2 (en) | 2012-07-20 | 2018-03-27 | Icon Aircraft, Inc. | Spin resistant aircraft configuration |
| AU2016225939B2 (en) * | 2012-07-20 | 2018-04-05 | SG Investment America, Inc. | Spin Resistant Aircraft Configuration |
| US10723444B2 (en) | 2012-07-20 | 2020-07-28 | Icon Aircraft, Inc. | Spin resistant aircraft configuration |
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