US1791716A - Bomb - Google Patents
Bomb Download PDFInfo
- Publication number
- US1791716A US1791716A US251721A US25172128A US1791716A US 1791716 A US1791716 A US 1791716A US 251721 A US251721 A US 251721A US 25172128 A US25172128 A US 25172128A US 1791716 A US1791716 A US 1791716A
- Authority
- US
- United States
- Prior art keywords
- bomb
- tube
- charge
- tail portion
- nose portion
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
- F42C1/02—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
- F42C1/08—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze with delayed action after ignition of fuze or after impact
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
- F42C1/02—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
- F42C1/09—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze the fuze activating a propulsive charge for propelling the ammunition or the warhead into the air, e.g. in rebounding projectiles
Definitions
- the subjectof this invention is a bomb.
- Fig. 1 is a longitudinal sectional view of the bomb constructed in accordance with ⁇ the invention.
- Fig. 2 is an enlarged sectional v1ew o f the forward end of the axial tube.
- the tail portion is provided 'with a firing pm carrier 10, a delay element 11, a detonator .12 and a booster 13, the explosive elements bemg encased as a unit for insertion in an axial tube 14 and for retention therein by the carrier l0 when threaded to the tube.
- This tube is threaded as at 15 in the forward Wall of the tail portion and is fitted with a thimble 16 which enters a socket 17 in the rear end of the tail portion.
- the firing pin carrier 10 slidably mounts a firing pm 18 which is held in the safe position agalnst rearward movement by means of a pin 19 which is sheared when the expelling charge 9 1s set off.
- the firing pin is also held against forward displacement on impact by means of a heavy bolt 20.
- the bomb Upon impact with the ground, the bomb will penetrate until retarded after which the fuse 8 ignites the expelling charge 9 which breaks the connection 7, drives the firing pin 1 8 home,.and propels the tail portion into the air.
- the period of the delay in the delay element 11 will be controlled by the nature of the contents o f the bomb. For the most effective burst or under special circumstances an air burst of different height may be required depending upon the particular kind of gas in the bomb or whether the contents are incendiary or smoke producing material.
- a bomb comprising a tail portion, a nose portion frangibly connected thereto, an expeiling charge in the nose portion, a delay fuse in the nose portion, a tube secured to the forward end of the tail portion, and having a socket engagement with the rear end'thereof, explosive elements encased as a unit inserted in the tube, a ring'pin carrier secured to the tube and retaining the explosive elements, a firing pin slidably mounted in the carrier and available to the expelling charge and means for holding the firing pin against movement towards the expelling charge.
- a bomb comprising a tail ortion, a nose portion frangibly connected tliereto, an expelling charge in the nose portion, a delay fuse inthe nose portion, an axial tube in the tail portion, explosive elements encased as a unit inserted in the tube, a ring pin carrier secured to the tube and retaining the explosive elements, a firing pin slidably mounted in the carrier and available to the expelling charge and means for holding the rng in against movement towards the expelhng charge.
- a bomb comprising a tail portion, a nose portion frangibly connected thereto, an ex'- pelling charge in the nose portion, a delay fuse in the nose portion, a tube secured to the forward end of the tail portion, and having a, socket engagement with the rear end thereof and a firing mechanism, including an expelling-charge-actuated iring pin carried by the tube.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Geophysics And Detection Of Objects (AREA)
Description
Feb. l0, 193i. M. H. DAVIS ET AL BOMB Filed Feb. 5. 1928 nvnom Merle 'H Davs David L Wnndherrg Patented Feb. 10, 1931 UNITED 4STATES PATEN'I OFFICE MERLE H. DAVIS, OF THE UNITED STATES ARMY, AND DAVID L. WOODBERBY, BOTH 0F EDGEWOOD ARSENAL, MARYLAND BOMB Application led February 3, 1928. Serial No. 251,721.
(GRANTEDUNDER THE ACT 0F MARCH 3, 1883, AS AMENDED APRIL 30, 1928; 870 0. G. 757) The invention described herein may be manufactured and used by or for the Government for governmental purposes wlthout the lpayment to us of any royalty thereon.
The subjectof this invention is a bomb.
In bombing operations against personnel or unprotected positions it isv necessary that the explosions of the bomb occur in the alr to secure an eflicient dispersion ofthe shell fragments or the chemical, incendiary, or smoke contents of the bomb. To meet this requirement it has been customary to provide a rapid detonating device protruding from the nose of the bomb. While an air burst may thus be secured the bomb is practically on the ground and under the inuence of inertia.
According to this invention it is proposed to provide a bomb which is -permitted to first strike and penetrate the ground and then be driven rearwardly to a predetermined height above the ground before the burstingv charge is set oil'.
With the foregoing and other objects in view, our invention resides in the novel arrangement and combination of parts and 1n the details of construction hereinafter described and claimed, it being understood that changes in the precise embodiment of the invention herein disclosed may be made within the scope of what is claimed without departing from the spirit of the invention.
A practical embodiment of the inventlon 1s illustrated in the drawings, wherein:
Fig. 1 is a longitudinal sectional view of the bomb constructed in accordance with` the invention.
Fig. 2 is an enlarged sectional v1ew o f the forward end of the axial tube.
is of sutlicient capacity to insure propulsion lof the tail portion into the air.
.The tail portion is provided 'with a firing pm carrier 10, a delay element 11, a detonator .12 and a booster 13, the explosive elements bemg encased as a unit for insertion in an axial tube 14 and for retention therein by the carrier l0 when threaded to the tube. This tube is threaded as at 15 in the forward Wall of the tail portion and is fitted with a thimble 16 which enters a socket 17 in the rear end of the tail portion.
"The firing pin carrier 10 slidably mounts a firing pm 18 which is held in the safe position agalnst rearward movement by means of a pin 19 which is sheared when the expelling charge 9 1s set off. The firing pin is also held against forward displacement on impact by means of a heavy bolt 20.
.Upon impact with the ground, the bomb will penetrate until retarded after which the fuse 8 ignites the expelling charge 9 which breaks the connection 7, drives the firing pin 1 8 home,.and propels the tail portion into the air. The period of the delay in the delay element 11 will be controlled by the nature of the contents o f the bomb. For the most effective burst or under special circumstances an air burst of different height may be required depending upon the particular kind of gas in the bomb or whether the contents are incendiary or smoke producing material.
We claim:
1. A bomb comprising a tail portion, a nose portion frangibly connected thereto, an expeiling charge in the nose portion, a delay fuse in the nose portion, a tube secured to the forward end of the tail portion, and having a socket engagement with the rear end'thereof, explosive elements encased as a unit inserted in the tube, a ring'pin carrier secured to the tube and retaining the explosive elements, a firing pin slidably mounted in the carrier and available to the expelling charge and means for holding the firing pin against movement towards the expelling charge.
2. A bomb comprising a tail ortion, a nose portion frangibly connected tliereto, an expelling charge in the nose portion, a delay fuse inthe nose portion, an axial tube in the tail portion, explosive elements encased as a unit inserted in the tube, a ring pin carrier secured to the tube and retaining the explosive elements, a firing pin slidably mounted in the carrier and available to the expelling charge and means for holding the rng in against movement towards the expelhng charge.
3. A bomb comprising a tail portion, a nose portion frangibly connected thereto, an ex'- pelling charge in the nose portion, a delay fuse in the nose portion, a tube secured to the forward end of the tail portion, and having a, socket engagement with the rear end thereof and a firing mechanism, including an expelling-charge-actuated iring pin carried by the tube.
MERLE H. DAVIS, LT. OBD. DAVID L. WOODBERRY.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US251721A US1791716A (en) | 1928-02-03 | 1928-02-03 | Bomb |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US251721A US1791716A (en) | 1928-02-03 | 1928-02-03 | Bomb |
Publications (1)
Publication Number | Publication Date |
---|---|
US1791716A true US1791716A (en) | 1931-02-10 |
Family
ID=22953121
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US251721A Expired - Lifetime US1791716A (en) | 1928-02-03 | 1928-02-03 | Bomb |
Country Status (1)
Country | Link |
---|---|
US (1) | US1791716A (en) |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2433875A (en) * | 1944-11-16 | 1948-01-06 | Walker Brooks | Method of clearing mine fields |
US2457817A (en) * | 1944-03-31 | 1949-01-04 | Garland L Harrell | Bomb |
US2742856A (en) * | 1944-11-06 | 1956-04-24 | Louis F Fieser | Burster |
US2926607A (en) * | 1957-05-28 | 1960-03-01 | Jr Hollis L Muller | Hermetically sealed explosive cartridge |
US3216354A (en) * | 1952-07-10 | 1965-11-09 | Marshall P Bearce | Land mine |
US3344742A (en) * | 1965-05-10 | 1967-10-03 | Cornell Aeronautical Labor Inc | Explosive projector |
US3408935A (en) * | 1964-08-18 | 1968-11-05 | Navy Usa | Flexible line delivery method and device for chemical and incapacitating agents |
US3505960A (en) * | 1967-03-31 | 1970-04-14 | Armes De Guerre Fab Nat | Projectile fuse and projectiles equipped with said fuse |
US3552326A (en) * | 1968-12-19 | 1971-01-05 | William J Howe | Low aerial burst detonating device |
US3589294A (en) * | 1957-06-21 | 1971-06-29 | Us Navy | System for multiple point simultaneous initiation of explosive charges |
US3736874A (en) * | 1970-05-28 | 1973-06-05 | Us Navy | Chemiluminescent expulsion device |
US3811381A (en) * | 1972-03-16 | 1974-05-21 | Fmc Corp | Smoke spotting cartridge |
FR2229947A1 (en) * | 1973-05-18 | 1974-12-13 | Raufoss Ammunisjonsfabrikker | |
US3921528A (en) * | 1971-06-15 | 1975-11-25 | Us Navy | Land mine expulsion system |
US3968748A (en) * | 1973-01-15 | 1976-07-13 | The United States Of America As Represented By The Secretary Of The Navy | Target discriminating bomblet |
US3992995A (en) * | 1975-09-04 | 1976-11-23 | The United States Of America As Represented By The Secretary Of The Air Force | Speed controlled second event launcher |
US3996857A (en) * | 1972-05-10 | 1976-12-14 | The United States Of America As Represented By The Secretary Of The Army | Jungle penetration munition |
US3999482A (en) * | 1975-07-09 | 1976-12-28 | The United States Of America As Represented By The Secretary Of The Air Force | High explosive launcher system |
US4132169A (en) * | 1970-11-06 | 1979-01-02 | Beech Aircraft Corporation | Fuel-air type bomb |
US4227460A (en) * | 1977-07-26 | 1980-10-14 | Buck Chemisch-Technische Werke Gmbh & Co. | Practice war head device |
US4318343A (en) * | 1971-08-19 | 1982-03-09 | The United States Of America As Represented By The Secretary Of The Navy | Dual mode incendiary bomblet |
US4458596A (en) * | 1982-07-06 | 1984-07-10 | The United States Of America As Represented By The Secretary Of The Navy | Multi-purpose bomblet |
-
1928
- 1928-02-03 US US251721A patent/US1791716A/en not_active Expired - Lifetime
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2457817A (en) * | 1944-03-31 | 1949-01-04 | Garland L Harrell | Bomb |
US2742856A (en) * | 1944-11-06 | 1956-04-24 | Louis F Fieser | Burster |
US2433875A (en) * | 1944-11-16 | 1948-01-06 | Walker Brooks | Method of clearing mine fields |
US3216354A (en) * | 1952-07-10 | 1965-11-09 | Marshall P Bearce | Land mine |
US2926607A (en) * | 1957-05-28 | 1960-03-01 | Jr Hollis L Muller | Hermetically sealed explosive cartridge |
US3589294A (en) * | 1957-06-21 | 1971-06-29 | Us Navy | System for multiple point simultaneous initiation of explosive charges |
US3408935A (en) * | 1964-08-18 | 1968-11-05 | Navy Usa | Flexible line delivery method and device for chemical and incapacitating agents |
US3344742A (en) * | 1965-05-10 | 1967-10-03 | Cornell Aeronautical Labor Inc | Explosive projector |
US3505960A (en) * | 1967-03-31 | 1970-04-14 | Armes De Guerre Fab Nat | Projectile fuse and projectiles equipped with said fuse |
US3552326A (en) * | 1968-12-19 | 1971-01-05 | William J Howe | Low aerial burst detonating device |
US3736874A (en) * | 1970-05-28 | 1973-06-05 | Us Navy | Chemiluminescent expulsion device |
US4132169A (en) * | 1970-11-06 | 1979-01-02 | Beech Aircraft Corporation | Fuel-air type bomb |
US3921528A (en) * | 1971-06-15 | 1975-11-25 | Us Navy | Land mine expulsion system |
US4318343A (en) * | 1971-08-19 | 1982-03-09 | The United States Of America As Represented By The Secretary Of The Navy | Dual mode incendiary bomblet |
US3811381A (en) * | 1972-03-16 | 1974-05-21 | Fmc Corp | Smoke spotting cartridge |
US3996857A (en) * | 1972-05-10 | 1976-12-14 | The United States Of America As Represented By The Secretary Of The Army | Jungle penetration munition |
US3968748A (en) * | 1973-01-15 | 1976-07-13 | The United States Of America As Represented By The Secretary Of The Navy | Target discriminating bomblet |
FR2229947A1 (en) * | 1973-05-18 | 1974-12-13 | Raufoss Ammunisjonsfabrikker | |
US3999482A (en) * | 1975-07-09 | 1976-12-28 | The United States Of America As Represented By The Secretary Of The Air Force | High explosive launcher system |
US3992995A (en) * | 1975-09-04 | 1976-11-23 | The United States Of America As Represented By The Secretary Of The Air Force | Speed controlled second event launcher |
US4227460A (en) * | 1977-07-26 | 1980-10-14 | Buck Chemisch-Technische Werke Gmbh & Co. | Practice war head device |
US4458596A (en) * | 1982-07-06 | 1984-07-10 | The United States Of America As Represented By The Secretary Of The Navy | Multi-purpose bomblet |
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