GB392727A - Improvements relating to aeroplanes - Google Patents
Improvements relating to aeroplanesInfo
- Publication number
- GB392727A GB392727A GB1174632A GB1174632A GB392727A GB 392727 A GB392727 A GB 392727A GB 1174632 A GB1174632 A GB 1174632A GB 1174632 A GB1174632 A GB 1174632A GB 392727 A GB392727 A GB 392727A
- Authority
- GB
- United Kingdom
- Prior art keywords
- roof
- side walls
- cabin
- aeroplane
- rear part
- 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
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1476—Canopies; Windscreens or similar transparent elements
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
392,727. Aeroplane cabin-tops. COMPER AIRCRAFT CO., Ltd., Heston Airport, Hounslow, Middlesex, and COM. PER, N., Hooton Park Aerodrome, Wirral, Cheshire. April 23, 1932, No. 11746. [Class 4.] In an aeroplane a cabin-top comprises two relatively movable parts, each comprising a roof and side walls, of which the front part is provided with a roof movable relatively to the side walls and is adapted in its rearward movement to slide over the roof of the rear part of the cabin-top and to fit closely in contact with the roof, so as to uncover that part of the cockpit adjacent to pilot's and/or passenger's seat. The cabin-top comprises a fixed screen 3, against which abuts a rearwardly slidable part 1, and a fixed rear part 2. Roof portion 9 of part 1 is hinged to its side walls by links 10, 11 at the front and by a pin and slot connection at the rear. Actuating means which may be disposed within the cockpit comprise a pivoted hand-lever 15, rearward movement of which causes part 1 to slide rearwardly, the side walls being engaged in guides formed in the side walls of the fuselage and the underside of roof 9 engaging in guides in top members 14 of the roof of rear part 2. A baffle 6 is fitted to screen 3 at the top and similar baffles may be fitted at its sides.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1174632A GB392727A (en) | 1932-04-23 | 1932-04-23 | Improvements relating to aeroplanes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1174632A GB392727A (en) | 1932-04-23 | 1932-04-23 | Improvements relating to aeroplanes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB392727A true GB392727A (en) | 1933-05-25 |
Family
ID=9991934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1174632A Expired GB392727A (en) | 1932-04-23 | 1932-04-23 | Improvements relating to aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB392727A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2570911A (en) * | 1947-04-01 | 1951-10-09 | Otis T Birdlebough | Boat top |
| US7401493B2 (en) | 2000-12-11 | 2008-07-22 | Honeywell Analytics, Ltd. | Gas sensor calibration method |
-
1932
- 1932-04-23 GB GB1174632A patent/GB392727A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2570911A (en) * | 1947-04-01 | 1951-10-09 | Otis T Birdlebough | Boat top |
| US7401493B2 (en) | 2000-12-11 | 2008-07-22 | Honeywell Analytics, Ltd. | Gas sensor calibration method |
| US7581425B2 (en) | 2000-12-11 | 2009-09-01 | Honeywell Analytics Limited | Gas sensor calibration system |
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