US1793567A - Supersensitive fuse for projectiles - Google Patents

Supersensitive fuse for projectiles Download PDF

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Publication number
US1793567A
US1793567A US306985A US30698528A US1793567A US 1793567 A US1793567 A US 1793567A US 306985 A US306985 A US 306985A US 30698528 A US30698528 A US 30698528A US 1793567 A US1793567 A US 1793567A
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United States
Prior art keywords
firing pin
casing
striker
fuse
vane
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Expired - Lifetime
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US306985A
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Alfred F Teitscheid
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Individual
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    • 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
    • F42C15/29Arming-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 fluidic oscillators; operated by dynamic fluid pressure, e.g. ram-air operated
    • 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

Definitions

  • the subject of this invention is a supersensitive fuse for projectiles.
  • the principal object of the invention is to provide a novel mechanism for holding an air balanceable striker in the unarmed position.
  • Fig. 1 is a longitudinal sectional view of the improved fuse shown in the unarmed position
  • Fig. 2 is a similar view of the fuse in the armed position
  • Fig. 8 is a plan view of the vane
  • Fig. 4 is a detail sectional view of the striker.
  • the fuse container consists of a hollow onepiece casing 5 threaded externally at its rear end for attachment to a projectile and threaded internally at its rear end for attachment of a diaphragm 6 to which is secured an explosivetrain 7 having a primer 8 and a booster charge 9.
  • the diaphragm is formed with a central aperture 10 to permit passage of a firing pin 11 which is provided with a threaded stem 12.
  • the stem is fixed to an airbalanceable striker 13 formed with an annular recess 14 in its under side and this recess is in communication with the atmosphere by means of ducts 15 leading to a recess 16 in the forward face of the striker and also by means of apertures 17 in the side walls of the striker.
  • the striker is further formed with a flange 18 which is engageable with the inturned lip 19 of the casing 5 to limit extrusion of. the striker.
  • the firing pin carries a collar 20 which rests on segmental blocks 21 embracing the firing pin and seated on the diaphragm.
  • .blocks are normally held against separation by means of a cage 22 whose forward end 23 is secured to a vane 24 and the hub 25 of the vane is threaded on the stem 12 of the firing pin.
  • the lower portion of the cage 22 is formed into'an annular disk 26 which extends laterally to the inner wall of the casing and overlies the diaphragm.
  • a pin 27 mounted in the diaphragm is normally held by a split ring 28 in an aperture in the disk 26 to prevent rotation of the cage and. vane. This in is withdrawn on setback when the pro ectile isfired.
  • the striker unit is retained in the armed position by reason of the flow of air which passes through the apertures 17 in the side walls of the striker and also by the air which is banked up between the disk 26 and diaphragm 6.
  • escape ports30 may be formed in the wall of the casing 5 between the vane 24 and disk 26 when unarmed and in position to be in rear of the disk and partially obturated after the disk has been forwardly displaced. This will insure a flow of air through the apertures 17 which is necessary to maintain the striker in the armed position.
  • a fuse embodying a hollow casing having a centrally apertured diaphragm, an explosive train carrier secured within the casing, an air balanceable striker in the nose of the casing, a firing pin having a threaded stem fixed to the striker, a collar on the firing pin, centrifugally releasable blocks embracing the firing pin between the collar and the diaphragm, a vane'threadedly mounted on the stem of the firing pin, a cage secured to the vane and confining the blocks and releasable means for normally holding thecage against rotation.
  • a firing pin having a threaded stem secured to the striker, centri'fugally releasable means for retaining the firing pin against inward movement, ava-ne disposed within the casing and threaded tothe stem of the firing pin, a cage carried by the vane and confinin the firing pin retaining means and means engagin the cage for normally holdo ing it against rotation.
  • a fuse embodying a hollow casing, an air halanceable striker inthe nose of the casing, a firing pin having a threaded stem secured to the striker, centrifugally releasable means for retaining the firing pin against inward movement, a vane disposed within the casing and threaded to the stem of the firing pin, a cage carried by the vane and confining the firing pin retaining means and said casing having an air escape port in rear of the vane and positioned to be inrear of the cage when the cage is elevated.
  • a fuse In a fuse, a hollow casing having communication with the atmosphere, an air balanceable striker in the nose of the casing, a firing pin having a threaded stem secured to the striker and normally held in the safe position and a vane within the casing mounted on the threaded stem and controlling re lease of the firing pin.
  • a casing having communicae tion with the atmosphere, an element of a firing mechanism movably mounted in the casing and normally held immovable, and a vane mounted formovement axially within the casingto' control release of the firing pin.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Filtering Of Dispersed Particles In Gases (AREA)
  • Lock And Its Accessories (AREA)

Description

1 613:24; 1931. A TE|T$cHE|D 1,793,567
SUPERSENSITIVE FUSE FOR PROJECTILES Filed Sept 19, 1928 -l rm abtomq Patented Feb. 24, 1931 UNHTED STATES ALFRED F. TEITSCHEID, OF WHARTON, NEW JERSEY SUPERSENSITIVE FUSE FOR IPROd'ECTILES Application filed September 19, 1928. Serial No. 306,985.
(GRANTED UNDER ran ACT or MARCH aissa, ASTAMENDED APRIL so, 1928; 3760. are? The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the payment to me of any royalty thereon.
The subject of this invention is a supersensitive fuse for projectiles.
The principal object of the invention is to provide a novel mechanism for holding an air balanceable striker in the unarmed position.
With the foregoing and other objects in View, my invention resides in the novel arrangement and combination of parts and in the details of construction hereinafter de- 1 scribed 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 invention is illustrated in the accompanying drawings, wherein:
Fig. 1 is a longitudinal sectional view of the improved fuse shown in the unarmed position;
Fig. 2 is a similar view of the fuse in the armed position;
Fig. 8 is a plan view of the vane;
Fig. 4: is a detail sectional view of the striker.
Referring to the drawings by numerals of reference:
The fuse container consists of a hollow onepiece casing 5 threaded externally at its rear end for attachment to a projectile and threaded internally at its rear end for attachment of a diaphragm 6 to which is secured an explosivetrain 7 having a primer 8 and a booster charge 9. The diaphragm is formed with a central aperture 10 to permit passage of a firing pin 11 which is provided with a threaded stem 12. The stem is fixed to an airbalanceable striker 13 formed with an annular recess 14 in its under side and this recess is in communication with the atmosphere by means of ducts 15 leading to a recess 16 in the forward face of the striker and also by means of apertures 17 in the side walls of the striker. The striker is further formed with a flange 18 which is engageable with the inturned lip 19 of the casing 5 to limit extrusion of. the striker.
The firing pin carries a collar 20 which rests on segmental blocks 21 embracing the firing pin and seated on the diaphragm. The .i.
.blocks are normally held against separation by means of a cage 22 whose forward end 23 is secured to a vane 24 and the hub 25 of the vane is threaded on the stem 12 of the firing pin. The lower portion of the cage 22 is formed into'an annular disk 26 which extends laterally to the inner wall of the casing and overlies the diaphragm. A pin 27 mounted in the diaphragm is normally held by a split ring 28 in an aperture in the disk 26 to prevent rotation of the cage and. vane. This in is withdrawn on setback when the pro ectile isfired.
The air currents which are admitted to the interior of the hollow casing 5 during flight I stopped by lack of threads on the firing pin r 1.2 but when it has reached this point the cage will have uncovered the segmental blocks 21 which are then free to be thrown outwardly by centrifugal force to release the firing pin.
The striker unit is retained in the armed position by reason of the flow of air which passes through the apertures 17 in the side walls of the striker and also by the air which is banked up between the disk 26 and diaphragm 6.
If desired, escape ports30 may be formed in the wall of the casing 5 between the vane 24 and disk 26 when unarmed and in position to be in rear of the disk and partially obturated after the disk has been forwardly displaced. This will insure a flow of air through the apertures 17 which is necessary to maintain the striker in the armed position.
I claim:
1. A fuse embodying a hollow casing having a centrally apertured diaphragm, an explosive train carrier secured within the casing, an air balanceable striker in the nose of the casing, a firing pin having a threaded stem fixed to the striker, a collar on the firing pin, centrifugally releasable blocks embracing the firing pin between the collar and the diaphragm, a vane'threadedly mounted on the stem of the firing pin, a cage secured to the vane and confining the blocks and releasable means for normally holding thecage against rotation. I
2. A fuse embodying a hollow casing, an
air-balanceable striker in-the' nose of the 10 casing, a firing pin having a threaded stem secured to the striker, centri'fugally releasable means for retaining the firing pin against inward movement, ava-ne disposed within the casing and threaded tothe stem of the firing pin, a cage carried by the vane and confinin the firing pin retaining means and means engagin the cage for normally holdo ing it against rotation.
3. A fuse embodying a hollow casing, an air halanceable striker inthe nose of the casing, a firing pin having a threaded stem secured to the striker, centrifugally releasable means for retaining the firing pin against inward movement, a vane disposed within the casing and threaded to the stem of the firing pin, a cage carried by the vane and confining the firing pin retaining means and said casing having an air escape port in rear of the vane and positioned to be inrear of the cage when the cage is elevated. e
' 4:. In a fuse, a hollow casing having communication with the atmosphere, an air balanceable striker in the nose of the casing, a firing pin having a threaded stem secured to the striker and normally held in the safe position and a vane within the casing mounted on the threaded stem and controlling re lease of the firing pin. g V I 5. In a fuse, a casing having communicae tion with the atmosphere, an element of a firing mechanism movably mounted in the casing and normally held immovable, and a vane mounted formovement axially within the casingto' control release of the firing pin.
' ALFRED F. TEITSGHEID.
US306985A 1928-09-19 1928-09-19 Supersensitive fuse for projectiles Expired - Lifetime US1793567A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2755737A (en) * 1947-11-25 1956-07-24 Allen S Clarke Rocket generator power supply
US2777392A (en) * 1952-12-24 1957-01-15 Laakso Aaro Kalevi Striker mechanism for a fuse
US2795190A (en) * 1945-06-04 1957-06-11 Ralph N Harmon Turbine driven fuze
US3710722A (en) * 1971-03-30 1973-01-16 Us Navy Fluid flow velocity actuated safety and arming device
FR2927695A1 (en) * 2008-02-19 2009-08-21 Tda Armements Sas Soc Par Acti MUNITION SPOUSE WITH SAFETY ARMING
EP2626665A1 (en) 2012-02-08 2013-08-14 MBDA France Method for lifting a firing safety and projectile implementing said method
EP3153812A1 (en) * 2015-10-07 2017-04-12 JUNGHANS Microtec GmbH Wind wheel, drive and igniter

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2795190A (en) * 1945-06-04 1957-06-11 Ralph N Harmon Turbine driven fuze
US2755737A (en) * 1947-11-25 1956-07-24 Allen S Clarke Rocket generator power supply
US2777392A (en) * 1952-12-24 1957-01-15 Laakso Aaro Kalevi Striker mechanism for a fuse
US3710722A (en) * 1971-03-30 1973-01-16 Us Navy Fluid flow velocity actuated safety and arming device
FR2927695A1 (en) * 2008-02-19 2009-08-21 Tda Armements Sas Soc Par Acti MUNITION SPOUSE WITH SAFETY ARMING
WO2009103707A1 (en) * 2008-02-19 2009-08-27 Tda Armements S.A.S Ammunition fuse with arming safety
EP2626665A1 (en) 2012-02-08 2013-08-14 MBDA France Method for lifting a firing safety and projectile implementing said method
WO2013117829A1 (en) 2012-02-08 2013-08-15 Mbda France Method for lifting a firing safety detent and projectile using this method
US9182206B2 (en) 2012-02-08 2015-11-10 Mbda France Method for lifting a firing safety detent and projectile using this method
EP3153812A1 (en) * 2015-10-07 2017-04-12 JUNGHANS Microtec GmbH Wind wheel, drive and igniter

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