GB715078A - Improvements in and relating to canopies of aircraft cockpits - Google Patents
Improvements in and relating to canopies of aircraft cockpitsInfo
- Publication number
- GB715078A GB715078A GB210952A GB210952A GB715078A GB 715078 A GB715078 A GB 715078A GB 210952 A GB210952 A GB 210952A GB 210952 A GB210952 A GB 210952A GB 715078 A GB715078 A GB 715078A
- Authority
- GB
- United Kingdom
- Prior art keywords
- canopy
- pivoted
- fuselage
- releasable
- aircraft
- 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)
- Hinges (AREA)
Abstract
715,078. Releasable cockpit canopies for aircraft. ENGLISH ELECTRIC CO., Ltd. Jan. 23, 1953 [Jan. 25, 1952], No. 2109/52. Class 4 A canopy for an aircraft cockpit is hinged at its back to the aircraft structure and held in its normal position by catches which are releasable to enable the canopy to be thrown open by a spring-loaded lever mechanism. The canopy 1 is pivoted at 3 to the fuselage 4 by hinges which may be releasable as described in Specification 711,987. It is provided along its lower edges with hooks 16 engaged in the closed position by pins 17 formed on levers 18 pivoted to the fuselage,and connected by tie rods 19 mounted inside the cockpit for operation by the pilot to release the canopy in an emergency. The canopy is urged into the open position by rods 15 each pivoted at one end to the canopy and at the other to one extremity of a lever 12, which levers are pivoted to the fuselage at 14 and urged into the canopy-releasing direction by torsion springs 13. In an alternative embodiment Figs. 1 and 2, (not shown), the mechanism to urge the canopy into the open position comprises a pair of interconnected toggle links loaded by a coiled tension spring.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB210952A GB715078A (en) | 1952-01-25 | 1952-01-25 | Improvements in and relating to canopies of aircraft cockpits |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB210952A GB715078A (en) | 1952-01-25 | 1952-01-25 | Improvements in and relating to canopies of aircraft cockpits |
Publications (1)
Publication Number | Publication Date |
---|---|
GB715078A true GB715078A (en) | 1954-09-08 |
Family
ID=9733774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB210952A Expired GB715078A (en) | 1952-01-25 | 1952-01-25 | Improvements in and relating to canopies of aircraft cockpits |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB715078A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5137232A (en) * | 1990-01-16 | 1992-08-11 | British Aerospace Public Limited Company | Canopy or panel locking assembly |
CN113562155A (en) * | 2021-08-25 | 2021-10-29 | 成都飞机工业(集团)有限责任公司 | Clamping type airplane cabin cover opening and closing mechanism, airplane cabin mechanism and opening and closing method thereof |
-
1952
- 1952-01-25 GB GB210952A patent/GB715078A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5137232A (en) * | 1990-01-16 | 1992-08-11 | British Aerospace Public Limited Company | Canopy or panel locking assembly |
CN113562155A (en) * | 2021-08-25 | 2021-10-29 | 成都飞机工业(集团)有限责任公司 | Clamping type airplane cabin cover opening and closing mechanism, airplane cabin mechanism and opening and closing method thereof |
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