GB577890A - Improvements relating to gun-turrets for aircraft - Google Patents
Improvements relating to gun-turrets for aircraftInfo
- Publication number
- GB577890A GB577890A GB278040A GB278040A GB577890A GB 577890 A GB577890 A GB 577890A GB 278040 A GB278040 A GB 278040A GB 278040 A GB278040 A GB 278040A GB 577890 A GB577890 A GB 577890A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinder
- gun
- turret
- aircraft
- effected
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
- F41A27/30—Stabilisation or compensation systems, e.g. compensating for barrel weight or wind force on the barrel
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Balance (AREA)
- Folding Of Thin Sheet-Like Materials, Special Discharging Devices, And Others (AREA)
- Automatic Tool Replacement In Machine Tools (AREA)
Abstract
577,890. Aircraft gun mountings. BRISTOL AEROPLANE CO., Ltd., FRISE, L. G., and FONSECA, E. C. M. D'ASSIS-. Feb. 13, 1940, No. 2780. [Class 92 (i)] A piston-and-cylinder device 20, 21 for counterbalancing the effect of air pressure in training aircraft guns, utilizes a vacuum or partial vacuum in the cylinder so that the counterbalancing force is produced by atmospheric pressure. In the form shown, the cylinder 21 is carried by the frame 15 supporting the gun turret 10 and the piston 20 is connected to a crankpin 18 on a gear-wheel 17 rotating in phase with the turret by being geared to a fixed wheel 14 of equal size on the axis of the turret. Adjustment for altitude of flight is effected by admitting air to the cylinder by cock 22. Automatic adjustment to suit gun elevation may be effected by sliding the cylinder on the frame 15.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB278040A GB577890A (en) | 1940-02-13 | 1940-02-13 | Improvements relating to gun-turrets for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB278040A GB577890A (en) | 1940-02-13 | 1940-02-13 | Improvements relating to gun-turrets for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB577890A true GB577890A (en) | 1946-06-05 |
Family
ID=9745756
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB278040A Expired GB577890A (en) | 1940-02-13 | 1940-02-13 | Improvements relating to gun-turrets for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB577890A (en) |
-
1940
- 1940-02-13 GB GB278040A patent/GB577890A/en not_active Expired
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