GB474043A - Improvements in or relating to anti-aircraft guns - Google Patents
Improvements in or relating to anti-aircraft gunsInfo
- Publication number
- GB474043A GB474043A GB1147336A GB1147336A GB474043A GB 474043 A GB474043 A GB 474043A GB 1147336 A GB1147336 A GB 1147336A GB 1147336 A GB1147336 A GB 1147336A GB 474043 A GB474043 A GB 474043A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sight
- gun
- angle
- pointer
- adjustable
- 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
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
474,043. Gun-sights. CARNAN, J. C. April 22, 1936, No. 11473. [Class 92 (ii)] Relates to anti-aircraft gun-sights which are adjustable relatively to the gun barrel to bring the sight on to the burst of a previously fired shell in order to adjust the angle between gun and sight previously set up to correct for speed of target. According to the invention, a telescopic sight 1, connected to the gun so as to move synchronously therewith in elevation and training, is mounted for independent universal adjustment to set the sight for the predicted angle of advance, a pointer 18, Fig. 2, in the eyepiece 3 being also set in relation to a mark 2 in the object glass to the same predicted angle. Further, to correct the angle of advance, the line of sight 18, 2 is adjusted on to the burst and the sight then clamped in relation to the gun barrel so that the sight and gun thereafter move in conformity. In the form shown, the sight is connected with the gun by parallelmotion links adjustable by a turnbuckle 22 which alters the length of the link 12. The sight is also universally mounted in a clampable bearing 23. The pointer 18 and a complementary pointer 18<1>, used when the target reverses its direction of flight, are adjustable by means of right- and left-handed screws rotated by knobs 21.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1147336A GB474043A (en) | 1936-04-22 | 1936-04-22 | Improvements in or relating to anti-aircraft guns |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1147336A GB474043A (en) | 1936-04-22 | 1936-04-22 | Improvements in or relating to anti-aircraft guns |
Publications (1)
Publication Number | Publication Date |
---|---|
GB474043A true GB474043A (en) | 1937-10-22 |
Family
ID=9986904
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1147336A Expired GB474043A (en) | 1936-04-22 | 1936-04-22 | Improvements in or relating to anti-aircraft guns |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB474043A (en) |
-
1936
- 1936-04-22 GB GB1147336A patent/GB474043A/en not_active Expired
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