US2981192A - Extensible bore safety pin - Google Patents
Extensible bore safety pin Download PDFInfo
- Publication number
- US2981192A US2981192A US821613A US82161359A US2981192A US 2981192 A US2981192 A US 2981192A US 821613 A US821613 A US 821613A US 82161359 A US82161359 A US 82161359A US 2981192 A US2981192 A US 2981192A
- Authority
- US
- United States
- Prior art keywords
- pin
- bore
- safety
- tube
- safety pin
- 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
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/20—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin
- F42C15/21—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin using spring action
Definitions
- Movement of this pin a predetermined distancereleases a slider which interposes a primer between the charge of the projectile and afiringpin arranged to be actuated upon impact of the projectile with the target.
- This arrangement has the disadvantage that the time interval between launching and arming ofthe projectile is limited by the bore-safety pin length that moves past the slider.
- any desired time delay between the launching and arming of a projectile is achieved by means of an extensible bore-safety pin.
- Figs. 1 to 5 illustrate the various positions assumed in the operation of a bore-safety pin or assemblage of the telescopic type
- Fig. 6 illustrates the relation between the bore-safety pin and the slider by which the projectile is armed
- Fig. 7 depicts a bore-safety pin or assemblage of the lanyard type
- Fig. 8 is an exploded view of the assemblage of Fig. 7.
- the bore safety assemblage of Figs. 1 to 5 includes a pin 10 which is recessed near one of its ends to receive a locking pin 11.
- the pin 11 is biased into the recess of pin 10 by a spring 12 and functioning to hold the pin 10 against a force exerted on its head by a spring 13.
- a tube 14 Concentric with the pin 10 is a tube 14 which is slotted near its inner end so that it may move outwardly without interference with the pin 11.
- the pin 10 has near its inner end a longitudinal slot 15 which is designed to cooperate with a ball 16 for locking the pin 10 and the tube 14 together when the pin has reached the end of its travels with respect to the tube. Thereafter the pin and tube move together releasing a slider which is mounted in an opening 17.
- Fig. 6 shows this slider as viewed longitudinally of the pin 10. It includes a body 18 which is biased against the pin 10 by a spring 19 and bears a primer 20 alined with an aperture 21.
- the slider moves to a point where the primer 20 is aligned with a firing pin 22 and the opening 21 is aligned with an opening 23 atent through which the charge of the projectile is ignited.
- the fuze of the projectile is identified by the nu meral 24 and the gun barrel by the numeral 25.
- Figs. 1 to 5 depict the different steps involved in the operation of the bore-safety assemblage.
- Fig. 2 shows this assemblage in its standby position.
- Fig. l is a section taken on the line 1--1 of Fig. 2.
- Fig. 3 illustrates the situation immediately following set-back with the pin 10 released and contacting the inner surface of the gun barrel.
- Fig. 4 shows the pin 10 as having cleared the muzzle of the gun and ready to actuate the ball release by which it is locked to the tube 14.
- Fig. 5 shows the bore-safety assemblage as altogether free of the fuze which is now armed.
- this telescoping assemblage practically doubles the time interval between launching and lanyard is fixed to the pin 10 and the other'end is fixed to the outer tube 27.
- the spring 13 Between the head of the bolt 10 and a shoulder 29 on the outer tube 27 is the spring 13 which is maintained in its illustrated condition either 'by a cord 30 or by the insertion of thepin into the fuze as shown in Fig. 2.
- the slider 18 (Fig. 6) engages the outer casing 27 (Fig. 7).
- the pin 10 In the operation of the lanyard type bore-safety assemblage, the pin 10 is released by the set-back force and the spring 13forces its head into engagement with the interior of the gun barrel as previously explained. When the pin 10 reaches the end of the barrel, it is ejected from the inner tube 26 trailing after it the lanyard 28. Complete uncoiling of the lanyard 28 tautens it so that the tube 27 is disengaged from the slider and the projectile fuze is armed as explained in connection with the telescopic bore-safety assemblage of Figs. 1 to 6.
- the above described bore-safety assemblages have the advantage that (1') they provide a greatly extended time delay between the launching and arming of the projectile, (2) they are not affected by temperature variations or set-back forces, and (3) they are economical to manufacture and install, having an outer configuration exactly the same as the configuration of the bore-safety pin.
- a projectile mechanism for controllably' increasing the time interval between the launching and arming of a projectile, said mechanism comprising in combination a bore safety pin transversely mounted within a fuze of the projectile, said fuze having a peripheral cut-away portion intermediate its ends, said safety pin having: a head at an outer end disposed generally outside the peripheral cut-away portion and an abutment at its inner end and a longitudinal slot contacting the abutment and extending outwardly along the safety pin and a recess near its abutment end spaced from said longitudinal slot; said fuze having a bore therein generally parallel with the axis of the fuze, a locking pin partially disposed and axially movable within said bore, a first helical spring seated in said bore and contacting the locking pin to urge said locking pin into said safety pin recess, a tube assembly generally concentrically telescopically mounted about said safety pin, a second helical spring having an outer end contacting the head of
- the deviceof claim 1 cut-away, portion and surjectile, said locking pin iscaused to be'withdrawn from of said safety pin by said first helical spring and said releasable locking ball'is causedto engage said safety.
- pin longitudinal'slot for contacting the safetypin abut- I mentlt'olock said outwardly movingj'safety pinto said telescoping'tube'assembly disposed immediately forwardly -of said locking pin' re- .cessin said safety pin and extending completely rearwar'dly of said telescoping tube assembly, said locking pin recess in said safety pin and saidtelescoping tube I I I *lorigitudinal slot being aligned to permit unimpeded out- I ward movementof said telescoping tube assembly.
- a projectile mechanism for controllably increasing the time interval between the firing and. arming of a projectile, said mechanism comprising incombination a bore safety'pin transversely: mounted within a fuze of the projectile, said tuze having a peripheral cut-away portion intermediate its. ends, said safety pin having ahead at an outer end disposed generally outside the peripheral cutaway portion and a recess adjacent an inner end, said I I fuze having a bore therein generally parallel with the axisof said fuze, a locking pin partially disposed and I further characterized by said I telescoping tube assembly having a longitudinal slot ,axially movable within said bore, a first helical spring seated in :said bore and contacting said 'lockingpin to.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Emergency Lowering Means (AREA)
Description
April 25, 1961 A. J.. GRANDY 2,981,192
EXTENSIBLE BORE SAFETY PIN Filed June 19, 1959 2 Sheets-Sheet 2 INVENTOR. ANDREW J. GRANDY BY X. W, a 4. MW
ATTORNEYS tates EXTENSIBLE BORE SAFETY PIN Andrew J. Grandy, North Hills, Pa., assignor to the .United States of America as represented by the Secretary of the Army Filed June 19, 1959, Ser. No. 821,613
. I '3 Claims. (Cl. 10278) 7 (Granted under Title 35, US. Code (1952), sec. 266) ,tofithe firing, i.e. launching from the weapon, .of the V projectile and is utilized to unlock a bore-safety pin.
Movement of this pin a predetermined distancereleases a slider which interposes a primer between the charge of the projectile and afiringpin arranged to be actuated upon impact of the projectile with the target. This arrangement has the disadvantage that the time interval between launching and arming ofthe projectile is limited by the bore-safety pin length that moves past the slider.
' In accordance with the present invention, any desired time delay between the launching and arming of a projectile is achieved by means of an extensible bore-safety pin.
The invention will be better understood from the following description when considered in connection with the accompanying drawings and its scope is indicated by the appended claims.
Referring to the drawings:
Figs. 1 to 5 illustrate the various positions assumed in the operation of a bore-safety pin or assemblage of the telescopic type,
Fig. 6 illustrates the relation between the bore-safety pin and the slider by which the projectile is armed,
' Fig. 7 depicts a bore-safety pin or assemblage of the lanyard type, and
Fig. 8 is an exploded view of the assemblage of Fig. 7.
The bore safety assemblage of Figs. 1 to 5 includes a pin 10 which is recessed near one of its ends to receive a locking pin 11. The pin 11 is biased into the recess of pin 10 by a spring 12 and functioning to hold the pin 10 against a force exerted on its head by a spring 13.
Concentric with the pin 10 is a tube 14 which is slotted near its inner end so that it may move outwardly without interference with the pin 11. As indicated more clearly in Fig. 1, the pin 10 has near its inner end a longitudinal slot 15 which is designed to cooperate with a ball 16 for locking the pin 10 and the tube 14 together when the pin has reached the end of its travels with respect to the tube. Thereafter the pin and tube move together releasing a slider which is mounted in an opening 17.
Fig. 6 shows this slider as viewed longitudinally of the pin 10. It includes a body 18 which is biased against the pin 10 by a spring 19 and bears a primer 20 alined with an aperture 21. When the pin 10 and tube 14 are withdrawn as previously explained the slider moves to a point where the primer 20 is aligned with a firing pin 22 and the opening 21 is aligned with an opening 23 atent through which the charge of the projectile is ignited.
'1 to 5 the fuze of the projectile is identified by the nu meral 24 and the gun barrel by the numeral 25.
Figs. 1 to 5 depict the different steps involved in the operation of the bore-safety assemblage. Thus Fig. 2 shows this assemblage in its standby position. Fig. l is a section taken on the line 1--1 of Fig. 2. Fig. 3 illustrates the situation immediately following set-back with the pin 10 released and contacting the inner surface of the gun barrel. Fig. 4 shows the pin 10 as having cleared the muzzle of the gun and ready to actuate the ball release by which it is locked to the tube 14. Fig. 5 shows the bore-safety assemblage as altogether free of the fuze which is now armed. As can be readily understood, the use ofthis telescoping assemblage practically doubles the time interval between launching and lanyard is fixed to the pin 10 and the other'end is fixed to the outer tube 27. Between the head of the bolt 10 and a shoulder 29 on the outer tube 27 is the spring 13 which is maintained in its illustrated condition either 'by a cord 30 or by the insertion of thepin into the fuze as shown in Fig. 2. When so inserted the slider 18 (Fig. 6) engages the outer casing 27 (Fig. 7).
In the operation of the lanyard type bore-safety assemblage, the pin 10 is released by the set-back force and the spring 13forces its head into engagement with the interior of the gun barrel as previously explained. When the pin 10 reaches the end of the barrel, it is ejected from the inner tube 26 trailing after it the lanyard 28. Complete uncoiling of the lanyard 28 tautens it so that the tube 27 is disengaged from the slider and the projectile fuze is armed as explained in connection with the telescopic bore-safety assemblage of Figs. 1 to 6.
As can be readily understood, the above described bore-safety assemblages have the advantage that (1') they provide a greatly extended time delay between the launching and arming of the projectile, (2) they are not affected by temperature variations or set-back forces, and (3) they are economical to manufacture and install, having an outer configuration exactly the same as the configuration of the bore-safety pin.
I claim? v 1. A projectile mechanism for controllably' increasing the time interval between the launching and arming of a projectile, said mechanism comprising in combination a bore safety pin transversely mounted within a fuze of the projectile, said fuze having a peripheral cut-away portion intermediate its ends, said safety pin having: a head at an outer end disposed generally outside the peripheral cut-away portion and an abutment at its inner end and a longitudinal slot contacting the abutment and extending outwardly along the safety pin and a recess near its abutment end spaced from said longitudinal slot; said fuze having a bore therein generally parallel with the axis of the fuze, a locking pin partially disposed and axially movable within said bore, a first helical spring seated in said bore and contacting the locking pin to urge said locking pin into said safety pin recess, a tube assembly generally concentrically telescopically mounted about said safety pin, a second helical spring having an outer end contacting the head of the bore safety pin'and an inner end contacting an inner 2. The deviceof claim 1 cut-away, portion and surjectile, said locking pin iscaused to be'withdrawn from of said safety pin by said first helical spring and said releasable locking ball'is causedto engage said safety. pin longitudinal'slot for contacting the safetypin abut- I mentlt'olock said outwardly movingj'safety pinto said telescoping'tube'assembly disposed immediately forwardly -of said locking pin' re- .cessin said safety pin and extending completely rearwar'dly of said telescoping tube assembly, said locking pin recess in said safety pin and saidtelescoping tube I I I *lorigitudinal slot being aligned to permit unimpeded out- I ward movementof said telescoping tube assembly.
3,. A projectile mechanism for controllably increasing the time interval between the firing and. arming of a projectile, said mechanism comprising incombination a bore safety'pin transversely: mounted within a fuze of the projectile, said tuze having a peripheral cut-away portion intermediate its. ends, said safety pin having ahead at an outer end disposed generally outside the peripheral cutaway portion and a recess adjacent an inner end, said I I fuze having a bore therein generally parallel with the axisof said fuze, a locking pin partially disposed and I further characterized by said I telescoping tube assembly having a longitudinal slot ,axially movable within said bore, a first helical spring seated in :said bore and contacting said 'lockingpin to. t i
5 tube concentrically mounted :about said inner tube in telescopingrrelation, therewith, spring holding means af- I :fixed about said outer tube a lanyard having a first end I andasecond end, said lanyard being generally helically: wound about said inner tube and enclosed by said outer r urge said locking pin into said 'safety pin recess, a telescoping. tube assembly, said* tube assembly compris-= 'ing an' inner tube concentrically mounted about said i safety pin intermediate its head and recess, an outer.
tube, saidlanyard firstend bcing'fastenedto said safety I pin at a point adjacent an outer endof said inner tubeand said lanyardsecond end being'fastened-to said outer tube at a point adjacent an inner end of saidlouter tube,
- a second: helical spring :disposedabout saidouter tube between its spring holding means and thesafety pin I head for urging said safety pin outwardly, an arming slide Within said fuze operable in response to ejection of: said boresafety :pin and outer tube of said l'QICSCQP-r ing assembly. 2 I t I ReferencesCited in the file of this patent I I i f a UNITED STATES PATENTS I I I I
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US821613A US2981192A (en) | 1959-06-19 | 1959-06-19 | Extensible bore safety pin |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US821613A US2981192A (en) | 1959-06-19 | 1959-06-19 | Extensible bore safety pin |
Publications (1)
Publication Number | Publication Date |
---|---|
US2981192A true US2981192A (en) | 1961-04-25 |
Family
ID=25233831
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US821613A Expired - Lifetime US2981192A (en) | 1959-06-19 | 1959-06-19 | Extensible bore safety pin |
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US (1) | US2981192A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3451306A (en) * | 1967-01-26 | 1969-06-24 | Susquehanna Corp | Safe and arm ejection system |
US3706282A (en) * | 1970-01-21 | 1972-12-19 | Us Air Force | Abort mechanism |
US3995556A (en) * | 1974-06-04 | 1976-12-07 | Hanns-Juergen Diederichs Kg | Percussion fuse for an explosive munitions shell |
US4449454A (en) * | 1981-11-03 | 1984-05-22 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Safety mechanism for an explosive body |
US5159150A (en) * | 1991-02-20 | 1992-10-27 | Buck Werke Gmbh & Co. | Arrangement to prevent a premature ignition of an active charge of a projectile |
US20080072781A1 (en) * | 2006-09-25 | 2008-03-27 | Chang Industry, Inc. | System and method for safing and arming a bore-launched projectile |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1272759A (en) * | 1918-02-04 | 1918-07-16 | John F C Yttrup | Hand-grenade. |
US1318954A (en) * | 1918-04-18 | 1919-10-14 | Explosive devices | |
US1375466A (en) * | 1918-07-30 | 1921-04-19 | Secretary Of War Trustee For G | Impact-fuse |
US1393585A (en) * | 1917-10-18 | 1921-10-11 | Clarence C Williams | Fuse for projectiles |
US1726325A (en) * | 1927-07-19 | 1929-08-27 | Varaud Andre | Percussion fuse for projectiles |
GB301517A (en) * | 1927-12-02 | 1929-09-05 | Ercole Galassini | Improvements in or relating to percussion fuses for bombs or similar projectiles |
US1806877A (en) * | 1931-05-26 | Point detonating fitse | ||
US2705921A (en) * | 1949-12-15 | 1955-04-12 | Jr John W Moseman | Fuze for non-rotating shaped charge projectiles |
-
1959
- 1959-06-19 US US821613A patent/US2981192A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1806877A (en) * | 1931-05-26 | Point detonating fitse | ||
US1393585A (en) * | 1917-10-18 | 1921-10-11 | Clarence C Williams | Fuse for projectiles |
US1272759A (en) * | 1918-02-04 | 1918-07-16 | John F C Yttrup | Hand-grenade. |
US1318954A (en) * | 1918-04-18 | 1919-10-14 | Explosive devices | |
US1375466A (en) * | 1918-07-30 | 1921-04-19 | Secretary Of War Trustee For G | Impact-fuse |
US1726325A (en) * | 1927-07-19 | 1929-08-27 | Varaud Andre | Percussion fuse for projectiles |
GB301517A (en) * | 1927-12-02 | 1929-09-05 | Ercole Galassini | Improvements in or relating to percussion fuses for bombs or similar projectiles |
US2705921A (en) * | 1949-12-15 | 1955-04-12 | Jr John W Moseman | Fuze for non-rotating shaped charge projectiles |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3451306A (en) * | 1967-01-26 | 1969-06-24 | Susquehanna Corp | Safe and arm ejection system |
US3706282A (en) * | 1970-01-21 | 1972-12-19 | Us Air Force | Abort mechanism |
US3995556A (en) * | 1974-06-04 | 1976-12-07 | Hanns-Juergen Diederichs Kg | Percussion fuse for an explosive munitions shell |
US4449454A (en) * | 1981-11-03 | 1984-05-22 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Safety mechanism for an explosive body |
US5159150A (en) * | 1991-02-20 | 1992-10-27 | Buck Werke Gmbh & Co. | Arrangement to prevent a premature ignition of an active charge of a projectile |
US20080072781A1 (en) * | 2006-09-25 | 2008-03-27 | Chang Industry, Inc. | System and method for safing and arming a bore-launched projectile |
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