GB441074A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB441074A GB441074A GB2045034A GB2045034A GB441074A GB 441074 A GB441074 A GB 441074A GB 2045034 A GB2045034 A GB 2045034A GB 2045034 A GB2045034 A GB 2045034A GB 441074 A GB441074 A GB 441074A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- air
- gaps
- aircraft
- stalling
- 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
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
441,074. Aircraft. BISHOP, W. H., 48, Moor Street, Birmingham. July 12, 1934, No. 20450. [Class 4] [See also Group X] Means for reducing the danger of stalling comprise the provision at the top front edge of an enclosed body or the outer portions of the wings, or of both of an upturned portion 2 flared out from the normal contour and preferably downwardly concave and which leaves a rearwardly facing gap 11 in communication with the interior of the aircraft and situated at the point where pressure of the boundary layer of air falls below a safe minimum to produce stalling. Back flow of air is prevented by a strip 5 and means may be provided for closing or partly closing at will the gaps 11 or air passages leading thereto. Flow of air past the gaps 11 induces ventilation in the wings and body and air inlets 10 may be provided on the pressure side of the body or wings. The gaps may extend over the whole length of the wings. Specifications 379,135 and 404,942, [both in Group X], are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2045034A GB441074A (en) | 1934-07-12 | 1934-07-12 | Improvements in or relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2045034A GB441074A (en) | 1934-07-12 | 1934-07-12 | Improvements in or relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB441074A true GB441074A (en) | 1936-01-13 |
Family
ID=10146147
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2045034A Expired GB441074A (en) | 1934-07-12 | 1934-07-12 | Improvements in or relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB441074A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2934289A (en) * | 1955-09-27 | 1960-04-26 | Leo Geib | Jettisonable attachment for airfoil lift modification |
-
1934
- 1934-07-12 GB GB2045034A patent/GB441074A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2934289A (en) * | 1955-09-27 | 1960-04-26 | Leo Geib | Jettisonable attachment for airfoil lift modification |
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