GB472366A - Improvements in removable roof for the cockpit of aircraft - Google Patents
Improvements in removable roof for the cockpit of aircraftInfo
- Publication number
- GB472366A GB472366A GB35147/36A GB3514736A GB472366A GB 472366 A GB472366 A GB 472366A GB 35147/36 A GB35147/36 A GB 35147/36A GB 3514736 A GB3514736 A GB 3514736A GB 472366 A GB472366 A GB 472366A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lugs
- aircraft
- lever
- roof
- cockpit
- 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
Abstract
472,366. Aircraft cockpit hoods. SAULNIER, R. Dec. 22, 1936, No. 35147. Convention date, Dec. 27, 1935. [Class 4] An aircraft cockpit is provided with a slidable cover operated and detachable by means of mechanism disposed inside the aircraft. As shown, the cover 1 is provided with two hinged side panels 9, 10, provided with, e.g. lugs 26, 27 which, when the panels are closed, are situated on either sides of lugs 31, 30, 29 respectively. The lugs 31, 30, 29 are provided on a carriage 28 which is translated along guides . through rack-andpinion gear 38, 35 on operation of a handle 36. The ends of the roof are provided with further lugs 14. Hooks, e.g. 21 on rods 12, are passed through holes in adjacent lugs, e.g. 27, 14 and 31. The roof is released, by a pull exerted on a member 25 which through a bell-crank lever 22 moves the rod 12 axially against the action of a spring 20 connected to a lever 16. After operation, the tension of the spring is maintained by co operation between the lever 16 and a bracket 41.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR472366X | 1935-12-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB472366A true GB472366A (en) | 1937-09-22 |
Family
ID=8902681
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB35147/36A Expired GB472366A (en) | 1935-12-27 | 1936-12-22 | Improvements in removable roof for the cockpit of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB472366A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2424834A (en) * | 1944-04-25 | 1947-07-29 | Messrs R Malcolm Ltd | Slidable and releasable hood for aircraft |
US2444114A (en) * | 1944-03-04 | 1948-06-29 | Republic Aviat Corp | Coordinated lock, equalizing valve, and closure seal |
US2445438A (en) * | 1944-09-14 | 1948-07-20 | Republic Aviat Corp | Canopy mounting and releasing mechanism |
-
1936
- 1936-12-22 GB GB35147/36A patent/GB472366A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2444114A (en) * | 1944-03-04 | 1948-06-29 | Republic Aviat Corp | Coordinated lock, equalizing valve, and closure seal |
US2424834A (en) * | 1944-04-25 | 1947-07-29 | Messrs R Malcolm Ltd | Slidable and releasable hood for aircraft |
US2445438A (en) * | 1944-09-14 | 1948-07-20 | Republic Aviat Corp | Canopy mounting and releasing mechanism |
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