GB280737A - Improvements in or relating to recoil and run-out apparatus for ordnance - Google Patents
Improvements in or relating to recoil and run-out apparatus for ordnanceInfo
- Publication number
- GB280737A GB280737A GB1079/27A GB107927A GB280737A GB 280737 A GB280737 A GB 280737A GB 1079/27 A GB1079/27 A GB 1079/27A GB 107927 A GB107927 A GB 107927A GB 280737 A GB280737 A GB 280737A
- Authority
- GB
- United Kingdom
- Prior art keywords
- recoil
- cylinder
- recuperator
- ram
- cradle
- 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
- F41A25/00—Gun mountings permitting recoil or return to battery, e.g. gun cradles; Barrel buffers or brakes
- F41A25/16—Hybrid systems
- F41A25/20—Hydropneumatic systems
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Orthopedics, Nursing, And Contraception (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
Abstract
280,737. Vickers, Ltd., Dawson, Sir A. T., Buckham, Sir G. T., and White, J. F. Jan. 13, 1927. Recoil apparatus.-Relates to recoil and runout apparatus of the kind in which the pneumatic recuperator does not communicate with the interior of the hydraulic recoil cylinder. According to the invention, the recuperator cylinder C and the recoil cylinder D are arranged in line one behind the other and the recoil cylinder or its piston rod, whichever moves relatively to the recuperator cylinder, is provided with a ram D<3> to compress air in the recuperator during recoil and return the gun after recoil. In the form shown in Fig. 1, the recoil cylinder D and the air-compressing ram D<2> are attached at the front end to a crosshead D<4> connected by rods D' to lugs A<1> on the breech ring of the gun and adapted to slide on guides B<1> on the cradle B. The recuperator cylinder, retained in a housing on the cradle by a nut b<3>, has glands C<2> through which the ram passes; the ram having a wall D<6> separating the liquid and air spaces. The recoil piston D<1> is connected by its rod D<2> to a lug B<2> on the cradle, and has a rearward extension F engaging a cylinder extending from the wall D<6> to control the run-out. A valve F<3> serves to regulate the run-out to suit the angle of elevation of the gun. The liquid in the recoil brake is replenished from a reservoir E on the crosshead D<4> through a passage d. In a modification, in which the recoil apparatus is arranged below the gun, the recoil cylinder is connected to the cradle, its piston rod is connected to the ram, and the run-out control rod is attached to the cradle and disposed in a bore formed in the recoil piston rod. In a further modification, Fig. 6, the recoil cylinder is detachably connected to the front end of the recuperator cylinder by bolts C<1x> and the ram D<3> is formed by a hollow extension of the recoil piston rod D<2> which is attached to the gun lug A' by a rod D<3x>. The arrangement permits of ready access to the glands C<2>, one of which may be carried by the recoil cylinder and the other by the recuperator.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1079/27A GB280737A (en) | 1927-01-13 | 1927-01-13 | Improvements in or relating to recoil and run-out apparatus for ordnance |
US211736A US1690281A (en) | 1927-01-13 | 1927-08-09 | Recoil and run-out apparatus for ordnance |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1079/27A GB280737A (en) | 1927-01-13 | 1927-01-13 | Improvements in or relating to recoil and run-out apparatus for ordnance |
Publications (1)
Publication Number | Publication Date |
---|---|
GB280737A true GB280737A (en) | 1927-11-24 |
Family
ID=9715792
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1079/27A Expired GB280737A (en) | 1927-01-13 | 1927-01-13 | Improvements in or relating to recoil and run-out apparatus for ordnance |
Country Status (2)
Country | Link |
---|---|
US (1) | US1690281A (en) |
GB (1) | GB280737A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL7110752A (en) * | 1970-10-29 | 1972-05-03 |
-
1927
- 1927-01-13 GB GB1079/27A patent/GB280737A/en not_active Expired
- 1927-08-09 US US211736A patent/US1690281A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US1690281A (en) | 1928-11-06 |
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