US2131037A - Bomb nose fuse - Google Patents

Bomb nose fuse Download PDF

Info

Publication number
US2131037A
US2131037A US168490A US16849037A US2131037A US 2131037 A US2131037 A US 2131037A US 168490 A US168490 A US 168490A US 16849037 A US16849037 A US 16849037A US 2131037 A US2131037 A US 2131037A
Authority
US
United States
Prior art keywords
pin
plunger
detonator
fuse
bomb
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
US168490A
Inventor
Harold M Brayton
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US168490A priority Critical patent/US2131037A/en
Application granted granted Critical
Publication of US2131037A publication Critical patent/US2131037A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/28Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
    • F42C15/295Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids operated by a turbine or a propeller; Mounting means therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/18Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved
    • F42C15/184Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a slidable carrier

Definitions

  • the invention relates to an improved nose fuse designed primarily for aerial drop bombs but not necessarily restricted thereto.
  • the improved fuse is of the general type in which a ring pin and a detonator to be fired thereby, are both held normally in safety positions but are armed ready for operation when the bomb travels a safe distance from the craft by means of which it is launched, detonation being effected by impact.
  • Fuses of this general character have heretofore been of rather complicated and expensive nature and have usually required a great many machine operations and special machinery for performing same.
  • the present invention aims to provide a greatly simplified construction which may be easily and inexpensively manufactured without necessarily requiring special shop equipment, the construction, however, being such that no loss in safety, sensitivity, or efficiency, results from the simplification.
  • I utilize a single pin to hold a detonator carrier in safety position when said pin occupies a normal rearward position, and to ilre the detonator upon impact after said pin has been moved, under the influence of a propeller, to a forward armed position, in which latter position, it allows movement of said detonator carrier to armed position. While this general idea has heretofore been proposed, I make unusually simple and inexpensive provision whereby the pin is directly driven by the propeller and is forwardly threaded to its armed position, doing away with parts heretofore used for this purpose and consequently reducing cost and enabling more easy and rapid manufacture.
  • Fig. 1 is a front elevation of a fuse constructed in accordance with the invention.
  • Fig. 2 is a vertical longitudinal sectional view as indicated by line 2-2 of Fig. 1, showing the normal safety positions of parts.
  • Fig. 3 is a fragmentary view similar to Fig. 2 but illustrating the parts in armed position.
  • a forwardly tapered fuse body 5 is shown for connection in any preferred way with the nose of a bomb.
  • 'I'his body is provided with an axial cylindrical bore 8 and with a transverse bore 1 intersecting said bore 8.
  • a carrying bolt 8 for the usual detonator 9 is slidably mounted in the bore 1 and a spring I0 is provided to move said 5 bolt from the safety position of Fig. 2 to the armed position of Fig. 3.
  • 'I'his spring may well thrust against a plug or cap Il which closes one end of the bore 1, the body 5 being preferably crimped at I2 to hold said plug or cap in place.
  • l0 When the bolt 8 is in the armed position of Fig.
  • the detonator 9 is in position to fire the explosive i3 upon firing of saiddetonator.
  • a plunger i4 is slidable in the bore 6 and is itself provided with an axial bore I5, a shear pin l5 I6 being employed to hold said plunger against movement with respect to the fuse body 5, until said plunger is driven rearwardly by impact, causing shearing of said pin I6.
  • the plunger is also held against rotation in the bore 6 by means 20 of a pin or screw I1 driven into an opening in the body 5 and engaging a longitudinal key-way or groove i8 in the periphery of said plunger.
  • This plunger is provided at its front end with an enlarged striking head I9 spaced forwardly 25 from the body 5, and when this head strikes the ground or any stationary object, the plunger is operated to cause the ring pin, hereinafter described, to ilre the detonator 9.
  • the firing pin 20 is threaded at 2l in the bore 30 i 5 of the plunger I4, and the rear end of this firing pin is provided with a reduced portion 22 received normally in a recess 23 in the bolt 8, to hold this bolt in the safety position shown in Fig. 2.
  • a safety pin 2l passes through alined 35 openings in the fuse body 5, the plunger i4 and the firing pin 28 to hold all parts in the positions of Fig. 2 from the time of manufacture until the bomb is placed in the usual rack or the like upon the craft by which it is to be carried, said pin 40 23 being then withdrawn.
  • a propeller 25 is provided for rotating the firing pin 2li in a direction to thread it forwardly as the bomb descends, said propeller being suitably connected with thefront end of said firing pin 20.
  • the propeller 25 is provided with a rearwardly projecting axial stub 26 which is threaded into the front portion of the plunger bore i5, the rear end of said stub being separably connected with the front end of said 50 firing pin, the connection being preferably accomplished by providing said stub with a groove 21 and providing said firing pin with a rib 28 removably received in said groove.
  • the conventional arming wire (not shown) may-be passed through 55 either of the eyes 29 on the'fuse body 5, and engaged with either of the openings 30 in the propeller 25, to hold the latter against accidental rotation after withdrawal of the safety pin 23, said arming wire being of course pulled from engagement with the eye and propeller when the bomb is dropped.
  • the bomb descends.
  • the propeller 25 rotates the ring pin 20 in a direction to forwardly thread said pin in the plunger I4, thereby withdrawing the pin end 22 from the recess 23 of the bolt 8 and allowing the spring I0 to shift this bolt to the armed position of Fig. 3.
  • the propeller preferably continues to drive the firing pin 20 for a few revolutions after arming of the bolt 8 has been effected, the forward movement of the pin being limited by means of a shoulder 3
  • the propeller stub 26 has threaded entirely out of the plunger Ill and the connection 21, 28 allows said propeller to become entirely disconnected from the fuse.
  • the plunger head I9 strikes any object on the continued descent of the bomb, the plunger ld and ring pin 20 are driven rearwardly from the armed position of Fig. 3, causing the pin end 22 to fire the detonator 9, which in turn res the explosive I3 and that within the bomb.
  • a bomb nose fuse having detonator carrying means and means for moving said detonator carrying means to armed position; a firing pin active when in a rearward position to hold said detonator carrying means in safety position and active to fire the detonator when driven rearwardly by impact from a forward armed position, said ring pin having direct threaded engagement with another portion of the fuse, and a propeller connected with the front end of said firing pin for rotating the same in a direction to cause forward threading of said firing pin to said armed position, in which it releases said detonator carrying means.
  • a fuse body detonator carrying means in said body, ring pin carrying means slidable longitudinally of said body and held against movement except under impact, a firing pin having a threaded connection directly with said firing pin carrying means, said firing pin normally engaging said detonator carrying means and holding the same in safety position, a propeller connected with the front end of said firing pin for rotating the same to cause forward movement of said firing pin to armed position, and means for moving said detonator carrying means to armed position when said ring pin releases said detonator carrying means.
  • a bomb nose fuse a fuse body, detonator carrying means in said body, a plunger slidable longitudinally in said body, means holding said plunger against movement with respect to said body except under impact, a firing pin threaded in said plunger and normally engaging said detonator carrying means to hold the same in safety position, a propeller connected with the front end of said firing pin for rotating the same to cause forward movement of said firing pin to armed position, and means for moving said detonator carrying means to armed position when said firing pin releases said carrying means.
  • a fuse body having an axial bore which opens through its front end and a transverse bore which intersects said axial bore, a spring-armed detonator-carrying-bolt slidable in said transverse bore, a plunger slidable in said axial bore and itself having an axial bore, means for holding said plunger against movement with respect to said fuse body except under impact, a firing pin threaded in said axial bore of said plunger and normally engaging said detonatorcarrying-bolt to hold the same in safety position, and a propeller connected with the front end of said firing pin for rotating it in a direction to thread said ring pin forwardly to armed position in which it releases said detonator-carrying-bolt.
  • a bomb nose fuse a fuse body, detonator carrying means in said body and means for moving said detonator carrying means to armed position, a plunger slidable longitudinally in said fuse body and projecting forwardly therefrom, means for holding said plunger against movement with respect to said fuse body except under impact, a firing pin threaded in said plunger and normally engaging said detonator carrying means to hold the same in safety position, and a propeller in front of said plunger and having a rearwardly projecting axial stub, said stub being threaded removably into the front end of said plunger and having a separable driving connection with the front end of said ring pin, said propeller and its stub serving to forwardly thread said ring pin to armed position in which it releases said detonator carrying means, said stub then unthreading completely from said plunger and separating cornpletely from said firing pin.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Automotive Seat Belt Assembly (AREA)

Description

' Sept. 27, 1938.
H. M. BRAYTON BOMB NOSE FUSE Filed oct. 11, i937 Tlf/3.5.
, Haro/J Shag/fo?? Patented` Sept. 27, 1938 UNITED STATES PATENT oFFicE 5 Claims.
The invention relates to an improved nose fuse designed primarily for aerial drop bombs but not necessarily restricted thereto.
The improved fuse is of the general type in which a ring pin and a detonator to be fired thereby, are both held normally in safety positions but are armed ready for operation when the bomb travels a safe distance from the craft by means of which it is launched, detonation being effected by impact. Fuses of this general character have heretofore been of rather complicated and expensive nature and have usually required a great many machine operations and special machinery for performing same. The present invention, however, aims to provide a greatly simplified construction which may be easily and inexpensively manufactured without necessarily requiring special shop equipment, the construction, however, being such that no loss in safety, sensitivity, or efficiency, results from the simplification.
In the improved construction, I utilize a single pin to hold a detonator carrier in safety position when said pin occupies a normal rearward position, and to ilre the detonator upon impact after said pin has been moved, under the influence of a propeller, to a forward armed position, in which latter position, it allows movement of said detonator carrier to armed position. While this general idea has heretofore been proposed, I make unusually simple and inexpensive provision whereby the pin is directly driven by the propeller and is forwardly threaded to its armed position, doing away with parts heretofore used for this purpose and consequently reducing cost and enabling more easy and rapid manufacture.
With the foregoing and minor objects in'view,`
the invention resides in the novel subject matter hereinafter described and claimed, description being accomplished by referenceto the accompanying drawing.
Fig. 1 is a front elevation of a fuse constructed in accordance with the invention.
Fig. 2 is a vertical longitudinal sectional view as indicated by line 2-2 of Fig. 1, showing the normal safety positions of parts.
Fig. 3 is a fragmentary view similar to Fig. 2 but illustrating the parts in armed position.
A preferred construction is shown in the drawing and will be rather specically described, with the understanding, however, that Within the scope of the invention as claimed, variationsmay be made.
A forwardly tapered fuse body 5 is shown for connection in any preferred way with the nose of a bomb. 'I'his body is provided with an axial cylindrical bore 8 and with a transverse bore 1 intersecting said bore 8. A carrying bolt 8 for the usual detonator 9 is slidably mounted in the bore 1 and a spring I0 is provided to move said 5 bolt from the safety position of Fig. 2 to the armed position of Fig. 3. 'I'his spring may well thrust against a plug or cap Il which closes one end of the bore 1, the body 5 being preferably crimped at I2 to hold said plug or cap in place. l0 When the bolt 8 is in the armed position of Fig.
3, the detonator 9 is in position to fire the explosive i3 upon firing of saiddetonator.
A plunger i4 is slidable in the bore 6 and is itself provided with an axial bore I5, a shear pin l5 I6 being employed to hold said plunger against movement with respect to the fuse body 5, until said plunger is driven rearwardly by impact, causing shearing of said pin I6. The plunger is also held against rotation in the bore 6 by means 20 of a pin or screw I1 driven into an opening in the body 5 and engaging a longitudinal key-way or groove i8 in the periphery of said plunger. This plunger is provided at its front end with an enlarged striking head I9 spaced forwardly 25 from the body 5, and when this head strikes the ground or any stationary object, the plunger is operated to cause the ring pin, hereinafter described, to ilre the detonator 9.
The firing pin 20 is threaded at 2l in the bore 30 i 5 of the plunger I4, and the rear end of this firing pin is provided with a reduced portion 22 received normally in a recess 23 in the bolt 8, to hold this bolt in the safety position shown in Fig. 2. A safety pin 2l passes through alined 35 openings in the fuse body 5, the plunger i4 and the firing pin 28 to hold all parts in the positions of Fig. 2 from the time of manufacture until the bomb is placed in the usual rack or the like upon the craft by which it is to be carried, said pin 40 23 being then withdrawn.
A propeller 25 is provided for rotating the firing pin 2li in a direction to thread it forwardly as the bomb descends, said propeller being suitably connected with thefront end of said firing pin 20. 45 In the present showing, the propeller 25 is provided with a rearwardly projecting axial stub 26 which is threaded into the front portion of the plunger bore i5, the rear end of said stub being separably connected with the front end of said 50 firing pin, the connection being preferably accomplished by providing said stub with a groove 21 and providing said firing pin with a rib 28 removably received in said groove. The conventional arming wire (not shown) may-be passed through 55 either of the eyes 29 on the'fuse body 5, and engaged with either of the openings 30 in the propeller 25, to hold the latter against accidental rotation after withdrawal of the safety pin 23, said arming wire being of course pulled from engagement with the eye and propeller when the bomb is dropped.
With the parts positioned as in Fig. 2, with the exception that the safety pin 26 is withdrawn, the bomb descends. During descent, the propeller 25 rotates the ring pin 20 in a direction to forwardly thread said pin in the plunger I4, thereby withdrawing the pin end 22 from the recess 23 of the bolt 8 and allowing the spring I0 to shift this bolt to the armed position of Fig. 3. The propeller preferably continues to drive the firing pin 20 for a few revolutions after arming of the bolt 8 has been effected, the forward movement of the pin being limited by means of a shoulder 3| thereon striking the rear end of the plunger i4. By the time this occurs, the propeller stub 26 has threaded entirely out of the plunger Ill and the connection 21, 28 allows said propeller to become entirely disconnected from the fuse. When the plunger head I9 strikes any object on the continued descent of the bomb, the plunger ld and ring pin 20 are driven rearwardly from the armed position of Fig. 3, causing the pin end 22 to fire the detonator 9, which in turn res the explosive I3 and that within the bomb.
From the foregoing, taken in connection with the accompanying drawing, it will be seen that novel and advantageous provision has been made for carrying out the objects of the invention, and while preferred features have been shown, attention is again invited to the possibility of making variations within the scope of the invention as claimed.
I claim:
1. In a bomb nose fuse having detonator carrying means and means for moving said detonator carrying means to armed position; a firing pin active when in a rearward position to hold said detonator carrying means in safety position and active to fire the detonator when driven rearwardly by impact from a forward armed position, said ring pin having direct threaded engagement with another portion of the fuse, and a propeller connected with the front end of said firing pin for rotating the same in a direction to cause forward threading of said firing pin to said armed position, in which it releases said detonator carrying means.
2. In a bomb nose fuse, a fuse body, detonator carrying means in said body, ring pin carrying means slidable longitudinally of said body and held against movement except under impact, a firing pin having a threaded connection directly with said firing pin carrying means, said firing pin normally engaging said detonator carrying means and holding the same in safety position, a propeller connected with the front end of said firing pin for rotating the same to cause forward movement of said firing pin to armed position, and means for moving said detonator carrying means to armed position when said ring pin releases said detonator carrying means.
3. In a bomb nose fuse, a fuse body, detonator carrying means in said body, a plunger slidable longitudinally in said body, means holding said plunger against movement with respect to said body except under impact, a firing pin threaded in said plunger and normally engaging said detonator carrying means to hold the same in safety position, a propeller connected with the front end of said firing pin for rotating the same to cause forward movement of said firing pin to armed position, and means for moving said detonator carrying means to armed position when said firing pin releases said carrying means.
4. In a bomb nose fuse, a fuse body having an axial bore which opens through its front end and a transverse bore which intersects said axial bore, a spring-armed detonator-carrying-bolt slidable in said transverse bore, a plunger slidable in said axial bore and itself having an axial bore, means for holding said plunger against movement with respect to said fuse body except under impact, a firing pin threaded in said axial bore of said plunger and normally engaging said detonatorcarrying-bolt to hold the same in safety position, and a propeller connected with the front end of said firing pin for rotating it in a direction to thread said ring pin forwardly to armed position in which it releases said detonator-carrying-bolt.
5. In a bomb nose fuse, a fuse body, detonator carrying means in said body and means for moving said detonator carrying means to armed position, a plunger slidable longitudinally in said fuse body and projecting forwardly therefrom, means for holding said plunger against movement with respect to said fuse body except under impact, a firing pin threaded in said plunger and normally engaging said detonator carrying means to hold the same in safety position, and a propeller in front of said plunger and having a rearwardly projecting axial stub, said stub being threaded removably into the front end of said plunger and having a separable driving connection with the front end of said ring pin, said propeller and its stub serving to forwardly thread said ring pin to armed position in which it releases said detonator carrying means, said stub then unthreading completely from said plunger and separating cornpletely from said firing pin.
HAROLD M. BRAYTON.
US168490A 1937-10-11 1937-10-11 Bomb nose fuse Expired - Lifetime US2131037A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US168490A US2131037A (en) 1937-10-11 1937-10-11 Bomb nose fuse

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US168490A US2131037A (en) 1937-10-11 1937-10-11 Bomb nose fuse

Publications (1)

Publication Number Publication Date
US2131037A true US2131037A (en) 1938-09-27

Family

ID=22611704

Family Applications (1)

Application Number Title Priority Date Filing Date
US168490A Expired - Lifetime US2131037A (en) 1937-10-11 1937-10-11 Bomb nose fuse

Country Status (1)

Country Link
US (1) US2131037A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2498043A (en) * 1943-04-02 1950-02-21 Charles C Lauritsen Fuse
US2718192A (en) * 1947-10-17 1955-09-20 Charles F Bowersett Time delay nose fuze for a rocket
US2742859A (en) * 1946-12-20 1956-04-24 Charles F Bowersett Nose fuze for a bomb
US2817295A (en) * 1953-08-14 1957-12-24 Harold B Wylie Firing pin for rocket fuze
US2856854A (en) * 1945-10-17 1958-10-21 Charles F Bowersett Combination fuze
US2963974A (en) * 1958-05-09 1960-12-13 Bendix Corp Impact detonating fuze with arming delay
US4726292A (en) * 1985-06-28 1988-02-23 Fratelli Borletti S.P.A. Fuse for sub-munitions to be expelled from a rocket
US4811664A (en) * 1987-03-31 1989-03-14 The State Of Israel, Ministry Of Defence, Israel Military Industries Fuse for sub-munition warhead
US6631667B1 (en) 2000-10-25 2003-10-14 Lockheed Martin Corporation Explosive-bolt-activated spring-loaded actuation device
WO2003095933A1 (en) * 2002-05-13 2003-11-20 Ruag Munition Percussion fuse

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2498043A (en) * 1943-04-02 1950-02-21 Charles C Lauritsen Fuse
US2856854A (en) * 1945-10-17 1958-10-21 Charles F Bowersett Combination fuze
US2742859A (en) * 1946-12-20 1956-04-24 Charles F Bowersett Nose fuze for a bomb
US2718192A (en) * 1947-10-17 1955-09-20 Charles F Bowersett Time delay nose fuze for a rocket
US2817295A (en) * 1953-08-14 1957-12-24 Harold B Wylie Firing pin for rocket fuze
US2963974A (en) * 1958-05-09 1960-12-13 Bendix Corp Impact detonating fuze with arming delay
US4726292A (en) * 1985-06-28 1988-02-23 Fratelli Borletti S.P.A. Fuse for sub-munitions to be expelled from a rocket
US4811664A (en) * 1987-03-31 1989-03-14 The State Of Israel, Ministry Of Defence, Israel Military Industries Fuse for sub-munition warhead
US6631667B1 (en) 2000-10-25 2003-10-14 Lockheed Martin Corporation Explosive-bolt-activated spring-loaded actuation device
WO2003095933A1 (en) * 2002-05-13 2003-11-20 Ruag Munition Percussion fuse

Similar Documents

Publication Publication Date Title
US2938463A (en) Percussion fuze
US1365870A (en) Explosively-actuated affixing device
US2131037A (en) Bomb nose fuse
US2537855A (en) Point contact fuse
US2014393A (en) Fuse for projectiles
US2030085A (en) Point-detonating fuse for projectiles
US2409205A (en) Bomb fuse
US2007026A (en) High explosive shell
US2413450A (en) Releasing device
US2397781A (en) Fuse
US2750888A (en) Long delay bomb tail fuze
US1975809A (en) Fuse for projectiles
US2911914A (en) Fuze for special shaped charge bomb
US3386334A (en) Firing mechanism for explosively actuated tools
US2817295A (en) Firing pin for rocket fuze
US1992926A (en) Fuse for projectiles
US3677185A (en) Arming device
GB429724A (en) Improvements in percussion fuses for projectiles, bombs and the like
US1382750A (en) Projectile
GB987453A (en) Improvements in or relating to projectile fuzes
US2101082A (en) Fuse
US2498043A (en) Fuse
US2779287A (en) Contact fuze
US1768678A (en) Fuse for trench-mortar projectiles
US2128838A (en) Fuse for projectiles