GB539699A - Improvements in and relating to aerial bombs - Google Patents

Improvements in and relating to aerial bombs

Info

Publication number
GB539699A
GB539699A GB3179239A GB3179239A GB539699A GB 539699 A GB539699 A GB 539699A GB 3179239 A GB3179239 A GB 3179239A GB 3179239 A GB3179239 A GB 3179239A GB 539699 A GB539699 A GB 539699A
Authority
GB
United Kingdom
Prior art keywords
bomb
pin
water
rod
impact
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
GB3179239A
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.)
CHRISTOPHER WILLIAM KENT
Original Assignee
CHRISTOPHER WILLIAM KENT
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 CHRISTOPHER WILLIAM KENT filed Critical CHRISTOPHER WILLIAM KENT
Priority to GB3179239A priority Critical patent/GB539699A/en
Publication of GB539699A publication Critical patent/GB539699A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B25/00Fall bombs

Abstract

539,699. Aerial bombs. KENT, C. W. Dec. 8, 1939, No. 31792. [Class 9 (i)] An aerial bomb having direct-acting detonating-means operated by impact is fitted with a nose-portion 13 adapted to be sheared from the main body 9 on impact with water, leaving one or more oblique surfaces 14 which cause the bomb to be diverted towards, or out of the surface of the water, delay-action detonating-means being provided to operate after a pre-determined lessening of the water resistance. Figs. 1 and 6 show the bomb in its composite form, and Figs. 5 and 7 after removal of the detachable nose-portion. The latter is normally secured to the body portion by means of interengaging tongues and grooves with or without catch-means such as a removable locking-pin, or a spring detent. A firing-pin 21 on a rod 20 is normally held at safety by a pin 23 engaging a sleeve 18, the pin being sheared on impact of the sleeve on the ground or other hard object such as a ship 34, Fig. 8. The delay-action means, which become operable when the noseportion 13 is removed, comprise a flap 26 pivoted on a guide-bearing 22 for the rod 20, and formed with detents 29 normally engaging lugs 32 on a rod 30 swung from a collar 24 slidable on the rod 20. In this position (Fig. 6), a spring 25 is compressed between the collar 24 and the sleeve 22. As the bomb enters the water, and is diverted along paths such as 37, 44, 40, Fig. 8, the reaction of the water against the flap 26 at first overcomes the pressure of the spring 25 which ultimately reacts to disengage the detents 29 from the lugs 32. The collar 24 is then forcibly urged against the flange 33 of the firing- pin to explode the bomb as indicated at 38 or 42, Fig. 8. The same Figure indicates impact explosion at 36. 45. To enhance the diversion of the submerged bomb, one or more tail fins 11 may be pivoted in an unbalanced arrangement so as to produce a hydroplane effect as indicated at 41, Fig. 8. In modifications (not shown), the main portion may comprise a series of bomb elements having differentlydirected diversion-surfaces so as to increase the effective area of operation.
GB3179239A 1939-12-08 1939-12-08 Improvements in and relating to aerial bombs Expired GB539699A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3179239A GB539699A (en) 1939-12-08 1939-12-08 Improvements in and relating to aerial bombs

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3179239A GB539699A (en) 1939-12-08 1939-12-08 Improvements in and relating to aerial bombs

Publications (1)

Publication Number Publication Date
GB539699A true GB539699A (en) 1941-09-22

Family

ID=10328467

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3179239A Expired GB539699A (en) 1939-12-08 1939-12-08 Improvements in and relating to aerial bombs

Country Status (1)

Country Link
GB (1) GB539699A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472866A (en) * 1944-02-19 1949-06-14 John I Thompson Marine mine
US2758542A (en) * 1950-09-07 1956-08-14 Burg Solomon Ahead-thrown weapon for submarine warfare
US3017831A (en) * 1948-08-24 1962-01-23 Barry Adelbert Aerially launched marine mine
US3282214A (en) * 1964-12-14 1966-11-01 Madison H Briscoe Projectile
WO1997007379A2 (en) 1995-08-17 1997-02-27 State Of Israel, Ministry Of Defense Rafael, Armament Development Authority Asymmetric penetration warhead
AU700862B2 (en) * 1995-08-17 1999-01-14 Rafael-Armament Development Authority Ltd. Asymmetric penetration warhead
US6012393A (en) * 1995-08-17 2000-01-11 State Of Israel-Ministry Of Defense, Rafael-Armamient Dieve Asymmetric penetration warhead

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472866A (en) * 1944-02-19 1949-06-14 John I Thompson Marine mine
US3017831A (en) * 1948-08-24 1962-01-23 Barry Adelbert Aerially launched marine mine
US2758542A (en) * 1950-09-07 1956-08-14 Burg Solomon Ahead-thrown weapon for submarine warfare
US3282214A (en) * 1964-12-14 1966-11-01 Madison H Briscoe Projectile
WO1997007379A2 (en) 1995-08-17 1997-02-27 State Of Israel, Ministry Of Defense Rafael, Armament Development Authority Asymmetric penetration warhead
WO1997007379A3 (en) * 1995-08-17 1997-05-22 Israel State Asymmetric penetration warhead
AU700862B2 (en) * 1995-08-17 1999-01-14 Rafael-Armament Development Authority Ltd. Asymmetric penetration warhead
US6012393A (en) * 1995-08-17 2000-01-11 State Of Israel-Ministry Of Defense, Rafael-Armamient Dieve Asymmetric penetration warhead

Similar Documents

Publication Publication Date Title
GB539699A (en) Improvements in and relating to aerial bombs
GB928734A (en) Improvements in turbines
GB545904A (en) Improvements in or relating to firing devices for the fuzes of bombs, flares, and the like
GB417314A (en) Improvements in projectiles
USD180341S (en) Pblotless propeller driven airplane
USD137292S (en) Airplane propeller
Usher Jr The civil administration of the British Navy during the American Revolution
USD140117S (en) Design foe an airplane
ES8353Y (en) Current limiter, the purpose of which is to prevent the cost of electrical fluid from exceeding a certain limit set in advance, and for which the limiter is properly conditioned.
GB145829A (en) Improvements in or relating to shell fuzes
Hornstein Some Words of War and Peace from 1945
GB578727A (en) Improvements in projectiles, bombs and torpedoes
GB560860A (en) Improvements in or relating to aerial bombs
CA411213A (en) Fuel priming valve assembly
FETTY et al. A test pilot's view of the sub-sonic jet upset problem(Alleviation of inadvertent dives of aircraft when overspeed region between normal cruise and design dive speed is entered)
CA411534A (en) Aircraft fuel pump by-pass valve
Nevins Rivalry in Armaments
GB986669A (en) Improvements in and relating to projectiles with instantaneous and delayed detonation
DK65234C (en) Hydraulic Steering Mechanism for Valves or Sliders, In particular for Explosion Engines.
CA410600A (en) Sump selector valve for fuel tanks
GB530715A (en) A safety device for bomb fuzes
CA412340A (en) Skid fender for life boats
GB533503A (en) Improvements in or relating to fuzes for shells or bombs
AU118284B2 (en) Improvements in or relating to vent valve assemblies, particularly for aircraft fuel tanks
AU113337B2 (en) Protective means for ships against mines, and torpedo attack