GB545459A - Improvements in or relating to gun-turrets for aircraft - Google Patents

Improvements in or relating to gun-turrets for aircraft

Info

Publication number
GB545459A
GB545459A GB361037A GB361037A GB545459A GB 545459 A GB545459 A GB 545459A GB 361037 A GB361037 A GB 361037A GB 361037 A GB361037 A GB 361037A GB 545459 A GB545459 A GB 545459A
Authority
GB
United Kingdom
Prior art keywords
gun
elevation
guns
training
turret
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
Application number
GB361037A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB361037A priority Critical patent/GB545459A/en
Publication of GB545459A publication Critical patent/GB545459A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A27/00Gun mountings permitting traversing or elevating movement, e.g. gun carriages
    • F41A27/06Mechanical systems
    • F41A27/18Mechanical systems for gun turrets

Abstract

545,459. Aircraft gun mountings. BRISTOL AEROPLANE CO., Ltd., and FRISE, L. G. Feb. 6, 1937, No. 3610. [Classes 92 (i) and 92 (ii)] [Also in Group XXXIII] A gun turret for aircraft comprises a hollow disc-like structure 16 tapered at its periphery and disposed edgewise to the direction of flight, the structure and the gun or guns carried thereby being rotatable about a transverse axis. In the form shown, the structure is rotated for training by a hydraulic jack 44 connected to one end of a cable 40 passing round a pulley 41 and anchored at its other end to a rubber loop spring 46. Two guns 11, 12 are mounted for elevation on a trunnion 15 and two further guns 10, 13 linked at 75 to the first pair move synchronously therewith about a trunion 14. Elevation of the guns in slots in the structure is effected by a hydraulic jack 31 through cable 32, pulley 35, and rubber loop spring 38. The gunner, accommodated in a fixed cabin 57 on a seat 25 automatically adjusted by the jack 31 to suit gun elevation, uses a sight 50 moved synchronously with the gun in elevation and training by cable gears, and controls the elevation and training by a handle 53 connected to valves 60, 61. The turret shown forms a rearward continuation of the tail plane 54 and is supported in bearings, trussed by a U-shaped member 23 in the gunner's cabin which is mounted above the tail plane and comprises opaque portions 55, 56 and a transparent portion 57. The guns are loaded through an opening 85 in the floor of the cabin which registers with an opening 87 in the turret.
GB361037A 1937-02-06 1937-02-06 Improvements in or relating to gun-turrets for aircraft Expired GB545459A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB361037A GB545459A (en) 1937-02-06 1937-02-06 Improvements in or relating to gun-turrets for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB361037A GB545459A (en) 1937-02-06 1937-02-06 Improvements in or relating to gun-turrets for aircraft

Publications (1)

Publication Number Publication Date
GB545459A true GB545459A (en) 1938-08-08

Family

ID=9761572

Family Applications (1)

Application Number Title Priority Date Filing Date
GB361037A Expired GB545459A (en) 1937-02-06 1937-02-06 Improvements in or relating to gun-turrets for aircraft

Country Status (1)

Country Link
GB (1) GB545459A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430747A (en) * 1943-01-30 1947-11-11 Bell Aircraft Corp Power-operated gun mount
US2442164A (en) * 1942-09-18 1948-05-25 Oilgear Co Power-operated means and control mechanism therefor
US2457242A (en) * 1944-11-30 1948-12-28 United Shoe Machinery Corp Gun turret
US2484869A (en) * 1944-01-01 1949-10-18 Borg Warner Reversible plural clutch drive
US2487237A (en) * 1945-02-14 1949-11-08 United Shoe Machinery Corp Power-operated flexible machine gun mount
US2569010A (en) * 1951-09-25 Gun sight
US2685233A (en) * 1943-04-19 1954-08-03 Rose Brothers Ltd Gun turret
US2700920A (en) * 1944-11-10 1955-02-01 United Shoe Machinery Corp Instrument control mount
CN102145751A (en) * 2011-03-14 2011-08-10 沈阳飞机工业(集团)有限公司 Device for simulating airplane throttle steel cable winding process

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2569010A (en) * 1951-09-25 Gun sight
US2442164A (en) * 1942-09-18 1948-05-25 Oilgear Co Power-operated means and control mechanism therefor
US2430747A (en) * 1943-01-30 1947-11-11 Bell Aircraft Corp Power-operated gun mount
US2685233A (en) * 1943-04-19 1954-08-03 Rose Brothers Ltd Gun turret
US2484869A (en) * 1944-01-01 1949-10-18 Borg Warner Reversible plural clutch drive
US2700920A (en) * 1944-11-10 1955-02-01 United Shoe Machinery Corp Instrument control mount
US2457242A (en) * 1944-11-30 1948-12-28 United Shoe Machinery Corp Gun turret
US2487237A (en) * 1945-02-14 1949-11-08 United Shoe Machinery Corp Power-operated flexible machine gun mount
CN102145751A (en) * 2011-03-14 2011-08-10 沈阳飞机工业(集团)有限公司 Device for simulating airplane throttle steel cable winding process
CN102145751B (en) * 2011-03-14 2013-07-17 沈阳飞机工业(集团)有限公司 Device for simulating airplane throttle steel cable winding process

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