US2293817A - Aerial bomb - Google Patents

Aerial bomb Download PDF

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Publication number
US2293817A
US2293817A US243019A US24301938A US2293817A US 2293817 A US2293817 A US 2293817A US 243019 A US243019 A US 243019A US 24301938 A US24301938 A US 24301938A US 2293817 A US2293817 A US 2293817A
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United States
Prior art keywords
plummet
bomb
cap
contacts
explosive
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 - Lifetime
Application number
US243019A
Inventor
George E Graver
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.)
WILLARD M GILLIES
Original Assignee
WILLARD M GILLIES
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Publication date
Application filed by WILLARD M GILLIES filed Critical WILLARD M GILLIES
Priority to US243019A priority Critical patent/US2293817A/en
Application granted granted Critical
Publication of US2293817A publication Critical patent/US2293817A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/20Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/201Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
    • F42B12/204Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/14Impact fuzes, i.e. fuzes actuated only by ammunition impact operating at a predetermined distance from ground or target by means of a protruding member

Definitions

  • Another object is to provide a detonsting mcsns I for aerial bombs adopted to incr the eiTectiveness thereof by detonoting thebombs Just prior to striking the ground.
  • Fig. l is e side view partly in section embodying my invention.
  • Fig. 2 is a. partial view in section of the forward end oi the same and showing the detonating mechanism in extended position.
  • a cross of a. bomb well 9 loans the front end of chamber-6, end the nose l is provided with an open end iii.
  • a pair of longitudinal partitions l l extend from the well e to the open end iii and form e. chemis provided with a ceive a threaded the ground, the
  • the stud 2c is formed its outer end which will in flight and unscrew the stud 24 and release the cap 2! from the nose I.
  • a look screw 28 is positioned plummet l3 and engages the rod IS with sufficient pressure to keep the rod l9 separated from the contacts It. -The pressure of the screw 26, however, is such that when the plummet l3 strikes impact of the cap 2
  • the explosive charge is adapted to be detonated by an electric current from one or more electric batteries lb suitably secured to the well 9 or otherwise. Wires id connect the batteries 55 to the explosive charge, and
  • wires ll connect the batteries id to a pair of contacts l8 suitably secured in the plummet I8.
  • an explosive carrying aerial w o. having an elongated body, means forming a restricted chamber in the forward end thereof, a, plummet stored in said chamber, a chain in said chamber and connected to the body and the plummet for limiting the distance the plummet may leave the body, means for detonating the explosive including batteries in the body on the outside of the restricted chamber, contacts intho plummet and wires connecting the contacts in a circuit including the batteries, a cap closing the end of ssidchamber, a sliding rod in the plummet connected to said cap for closing the said contacts, and an air propeller operated screw securing said cap to the body, whereby the cap and plummet are released after a predetermined time of travel of the bomb.
  • an air propeller having a screw threaded shaft met, and cables stored in the restricted chamber connected in circuit with the batteries, contacts and explosive charge for detonating the same, a

Description

ge. 5,,canuvzn I 2,293,817
AERIAL BOMB Filed NOV. 29, 1938 INVENTOR. GEORGE E. GEUVE/i.
K /034 v. amt/+6 ATTORNEYJ Aug, es, recs entree stern mm norm George Grover,
oil one-half to Willard Pd (Delhi.
don Francisco, Chili, designer I Gillies, lLos Angela,
Application November 29, oss, Serial No. 243,019
2 @1312 This invention relates to serial bombs, and
, more particularly to means for detoneting the Another object is to provide a detonsting mcsns I for aerial bombs adopted to incr the eiTectiveness thereof by detonoting thebombs Just prior to striking the ground.
Other objects end edventoges will appear. and be brought out more fully in the following specifipotion, reference being hsd to the eccom drewing, wherein,
Fig. l is e side view partly in section embodying my invention. v
Fig. 2 is a. partial view in section of the forward end oi the same and showing the detonating mechanism in extended position.
Heretofore eeriel bombs of e type dropped by airplanes have been detonated upon striking the ground and n large percentage of power, often as much as seventy percent, is ineffective, this energy resulting only inmching a hole in the ground. Therefore, it follows that if the bomb could be exploded a second or two previous to the impact of the be with the und, the explosive force thereof would have greater effectiveness then. otherwise. Such. as result is achieved by this invention as will beept from the following description.
Referring more particularly to the dre, I show u bomb 5 oi the type usually carried by sir-= plumes end the like, having at chamber 8 for the explosive charge, end having a tapered nose or end portion l and a plurality oi tsil fins d. A cross of a. bomb well 9 loans the front end of chamber-6, end the nose l is provided with an open end iii.
A pair of longitudinal partitions l l extend from the well e to the open end iii and form e. chemis provided with a ceive a threaded the ground, the
tapped bore 23 adapted to restud 24 which passes through the hole 2% by which means the cap 2| is accured to the nose I.
The stud 2c is formed its outer end which will in flight and unscrew the stud 24 and release the cap 2! from the nose I.
A look screw 28 is positioned plummet l3 and engages the rod IS with sufficient pressure to keep the rod l9 separated from the contacts It. -The pressure of the screw 26, however, is such that when the plummet l3 strikes impact of the cap 2| will cause the plummet E3 to be advanced along the rod I! causing the latter to complete the electric circuit between the contacts with an air screw at charge.
the explosive her i2 adopted for the accommodation of a plummet lil secured by a. chain id to the wall 9. These partitions also form two compartments in'which ere-arranged the batteries, ds later described.
The explosive charge is adapted to be detonated by an electric current from one or more electric batteries lb suitably secured to the well 9 or otherwise. Wires id connect the batteries 55 to the explosive charge, and
wires ll connect the batteries id to a pair of contacts l8 suitably secured in the plummet I8.
which may be supplied v A metallic rod lQ-is positioned in a bore Ed in the plummet i3 and is provided closes the open end Id of the is provided with a bore hole bomb. The cup 29 2 and the nose l with a. cap 2i which Fins 8 are each provided with a curved terminal portion 2i, the function of which is toretard the bomb 5 suiliciently to permit the plummet I; to fall out in advance of thebomb after the cap 2| has been released by the air screw 25, the plummet however being held by the chain ll the length of which may vary from a few to several feet as may It will thus be apparent that by the foregoing construction, the bomb will be detonated a few feet before striking the ground and the full explosive power will be eflective otherwise than by it"! v. .1 I 5 a large hole in the ground ving described my invention what I claim is. t 1. In combination, an explosive carrying aerial w o. having an elongated body, means forming a restricted chamber in the forward end thereof, a, plummet stored in said chamber, a chain in said chamber and connected to the body and the plummet for limiting the distance the plummet may leave the body, means for detonating the explosive including batteries in the body on the outside of the restricted chamber, contacts intho plummet and wires connecting the contacts in a circuit including the batteries, a cap closing the end of ssidchamber, a sliding rod in the plummet connected to said cap for closing the said contacts, and an air propeller operated screw securing said cap to the body, whereby the cap and plummet are released after a predetermined time of travel of the bomb.
2. In combination, an explosive carrying aerialturn when the bomb is,
laterally in the l8 thus detonating the be determined upon by actual conditions.
an air propeller having a screw threaded shaft met, and cables stored in the restricted chamber connected in circuit with the batteries, contacts and explosive charge for detonating the same, a
rod passing through the plumrfiet and normally held out of contact with the contacts, and an enlarged head carried by the outer end of the rod.
and closing the end of the restricted chamber and extending beyond the periphery thereof, and
passing through the edge 01 the enlarged head and into the body or the bomb for securing the same to the body, whereby the cap and the plummet are released after a. predetermined time 0! travel of the bomb.
GEO. E. GRQYIER.
US243019A 1938-11-29 1938-11-29 Aerial bomb Expired - Lifetime US2293817A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US243019A US2293817A (en) 1938-11-29 1938-11-29 Aerial bomb

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
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US2293817A true US2293817A (en) 1942-08-25

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417980A (en) * 1942-10-19 1947-03-25 Worth C Goss Demolition bomb
US3385214A (en) * 1965-09-01 1968-05-28 Sperry Rand Corp Two body fuzing system
US3416448A (en) * 1966-07-05 1968-12-17 Army Usa Control system for stand-off functioning of a projectile in flight over a target area
US3515067A (en) * 1968-07-19 1970-06-02 Us Navy Impact responsive proximity initiator
US3677179A (en) * 1966-09-29 1972-07-18 Lester A Potteiger Telescoping ordnance device
US4567829A (en) * 1984-07-30 1986-02-04 General Electric Company Shaped charge projectile system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417980A (en) * 1942-10-19 1947-03-25 Worth C Goss Demolition bomb
US3385214A (en) * 1965-09-01 1968-05-28 Sperry Rand Corp Two body fuzing system
US3416448A (en) * 1966-07-05 1968-12-17 Army Usa Control system for stand-off functioning of a projectile in flight over a target area
US3677179A (en) * 1966-09-29 1972-07-18 Lester A Potteiger Telescoping ordnance device
US3515067A (en) * 1968-07-19 1970-06-02 Us Navy Impact responsive proximity initiator
US4567829A (en) * 1984-07-30 1986-02-04 General Electric Company Shaped charge projectile system
WO1986000979A1 (en) * 1984-07-30 1986-02-13 General Electric Company Shaped charge projectile system

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