GB1055428A - Improvements in or relating to wings for flying bodies - Google Patents
Improvements in or relating to wings for flying bodiesInfo
- Publication number
- GB1055428A GB1055428A GB4788563A GB4788563A GB1055428A GB 1055428 A GB1055428 A GB 1055428A GB 4788563 A GB4788563 A GB 4788563A GB 4788563 A GB4788563 A GB 4788563A GB 1055428 A GB1055428 A GB 1055428A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spars
- wing
- spar
- displacing
- apex
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/40—Varying angle of sweep
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Connection Of Plates (AREA)
Abstract
1,055,428. Aircraft. HIRTENBERGER PATRONEN - ZUNDHUTCHEN - UND METALLWARENFABRIK A.G. Dec. 4, 1963 [Dec. 14, 1962], No. 47885/63. Heading B7W. A wing for a flying body is defined by three arcuate spars 1, 2 and 3 (Fig. 2, not shown) which are provided with a covering (not shown), spars 1 and 2 are of similar shape and are joined together at 4, spar 3 spans spars 1 and 2 and is joined to them at 5 and 6, a rib 7 supports the wing at 4 and at the apex 8 of spar 3, the covering is applied under stress to the unloaded wing and follows without wrinkling the changes of shape of the wing under load. As shown, the points of support 4 and 8 are fixed but in a modification (Fig. 3, not shown) the spar junction 4 is slidably mounted and will move towards the rear under load. The rib 7 may be telescopic for displacing the junction 4 and an hydraulic or electromagnetic drive may be provided for said displacing. The spars are made of plastics material as is the cover, the plastics for the spars being reinforced with glass fibres. The spars may taper towards the outer edge of the wing. In a further embodiment, spar 3 is bipartite and the two parts of the spars are connected by a hinge at their apex (Figs. 4 to 6, not shown).
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT978362A AT232871B (en) | 1962-12-14 | 1962-12-14 | Airfoil for an extremely high-speed missile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1055428A true GB1055428A (en) | 1967-01-18 |
Family
ID=3617245
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4788563A Expired GB1055428A (en) | 1962-12-14 | 1963-12-04 | Improvements in or relating to wings for flying bodies |
Country Status (2)
| Country | Link |
|---|---|
| AT (1) | AT232871B (en) |
| GB (1) | GB1055428A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4159087A (en) * | 1977-10-31 | 1979-06-26 | The Quaker Oats Company | Glider kite |
| CN110589020A (en) * | 2019-09-24 | 2019-12-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Structure and method for determining influence of surface quality defects of airplane |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3835213A1 (en) * | 1988-10-15 | 1990-05-10 | Schiffer Dietrich F W | Wing construction for energy transmission in the media of water and gas, and for a vehicle for movement on land or water and in the air |
-
1962
- 1962-12-14 AT AT978362A patent/AT232871B/en active
-
1963
- 1963-12-04 GB GB4788563A patent/GB1055428A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4159087A (en) * | 1977-10-31 | 1979-06-26 | The Quaker Oats Company | Glider kite |
| CN110589020A (en) * | 2019-09-24 | 2019-12-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Structure and method for determining influence of surface quality defects of airplane |
Also Published As
| Publication number | Publication date |
|---|---|
| AT232871B (en) | 1964-04-10 |
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