GB416841A - Improvements in gun mountings for aircraft - Google Patents
Improvements in gun mountings for aircraftInfo
- Publication number
- GB416841A GB416841A GB28849/32A GB2884932A GB416841A GB 416841 A GB416841 A GB 416841A GB 28849/32 A GB28849/32 A GB 28849/32A GB 2884932 A GB2884932 A GB 2884932A GB 416841 A GB416841 A GB 416841A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rollers
- brakes
- standards
- tracks
- gun
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWERÂ PLANTSÂ OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/02—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
416,841. Gun mountings; brakes. VICKERS (AVIATION), Ltd., and WALLIS, B. N., Byfleet Road, Weybridge, Surrey. March 24, 1933, No. 28849/32. [Class 92 (i).] An aircraft gun mounting, having upper and lower parallel tracks a, b of similar shape around which run rollers c, d on standards e for an arm g carrying the gun, has the rollers slidable in the standards and controlled by brakes applied by means which force the brakes against the rollers and the rollers against the tracks. The mechanism for withdrawing the brakes therefore acts to relieve the pressure on the rollers to facilitate easy training of the mounting. The upper and lower spring- pressed brake blocks f are simultaneously operated by a two-part link f<7>, f<17> one end of which is connected to a Bowden wire f<14> the spaced points of the other end being connected to the brake blocks by rods f<5>, f". The arrangement is such that the lever operates one brake block by rocking about the point of attachment to the other brake block. Each member c<3> carrying a ,brake block is free to slide and turn in a carrier member c<6>, adjustable by a screw in the end of a standard to permit of retraction of the rollers when fitting them between the tracks. An adjustable seat i is connected by parallel-motion links to the standards as described in Specification 406,753.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB28849/32A GB416841A (en) | 1933-03-24 | 1933-03-24 | Improvements in gun mountings for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB28849/32A GB416841A (en) | 1933-03-24 | 1933-03-24 | Improvements in gun mountings for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB416841A true GB416841A (en) | 1934-09-24 |
Family
ID=10282139
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB28849/32A Expired GB416841A (en) | 1933-03-24 | 1933-03-24 | Improvements in gun mountings for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB416841A (en) |
-
1933
- 1933-03-24 GB GB28849/32A patent/GB416841A/en not_active Expired
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