Projectile with propelling charge holder
IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0609235
(2003-06-27)
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발명자
/ 주소 |
- Dryer,Richard
- Hinsdale,Andrew J.
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출원인 / 주소 |
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대리인 / 주소 |
Renner, Otto, Boiselle &
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인용정보 |
피인용 횟수 :
2 인용 특허 :
4 |
초록
▼
A projectile, such as a mortar projectile, includes a self-discarding or self-consumable propelling charge holder. A self-discarding propelling charge holder is made up of multiple segments. The propelling charge holder is maintained in place during launch by an igniter holder, and by folding fins o
A projectile, such as a mortar projectile, includes a self-discarding or self-consumable propelling charge holder. A self-discarding propelling charge holder is made up of multiple segments. The propelling charge holder is maintained in place during launch by an igniter holder, and by folding fins of the projectile. The propelling charge increments are consumed during the launch process. After launch, as the folding fins deploy, the segments of the propelling charge holder separate from each other and from the remainder of the projectile, and the igniter holder is forcibly removed from the propelling charge holder segments. Alternatively, the propelling charge holder may be self-consumable, being made of a material that is consumed along with the propelling charge increments.
대표청구항
▼
What is claimed is: 1. A projectile comprising: a projectile body; a propelling charge holder separably rigidly mechanically connected to the projectile body; and external propelling charge increments at least partially surrounding the propelling charge holder; wherein the propelling charge holder
What is claimed is: 1. A projectile comprising: a projectile body; a propelling charge holder separably rigidly mechanically connected to the projectile body; and external propelling charge increments at least partially surrounding the propelling charge holder; wherein the propelling charge holder includes multiple propelling charge holder segments that are separable from the projectile body and from one another during flight of the projectile, after the projectile has exited from a launcher. 2. The projectile of claim 1, further comprising an internal propelling charge increment in a chamber enclosed by the propelling charge holder; wherein the chamber is defined by and within the multiple propelling charge holder segments. 3. The projectile of claim 2, wherein the segments have holes therein that allow communication between the chamber and the external propelling charge increments. 4. The projectile of claim 2, further comprising an igniter holder and an igniter that are both at least partially in the chamber. 5. The projectile of claim 1, further comprising fins hingedly coupled to the body forward of the propelling charge holder; wherein the fins may be retracted or deployed. 6. A projectile comprising: a projectile body; a propelling charge holder separably mechanically connected to the projectile body; and external propelling charge increments at least partially surrounding the propelling charge holder, wherein the propelling charge holder includes multiple propelling charge holder segments; and fins hingedly coupled to the body forward of the propelling charge holder; wherein the fins are retractable and deployable; and wherein the fins, when retracted, press against the propelling charge holder segments of the propelling charge holder. 7. The projectile of claim 6, wherein the fins press against a central portion of the propelling charge holder segments; and wherein the central portion of the propelling charge holder segments is closer to a centerline of the projectile than ends of the propelling charge holder segments. 8. The projectile of claim 7, wherein one of the ends of each of the propelling charge holder segments is a hooked end that engages an aft protrusion of the projectile body. 9. The projectile of claim 8, wherein the aft protrusion includes a flange that is engaged by the hooked ends. 10. The projectile of claim 8, wherein the fins each have a notch into which the hooked ends at least partially protrude when the fins are retracted. 11. A projectile comprising: a projectile body; a propelling charge holder separably coupled to the projectile body; and external propelling charge increments at least partially surrounding the propelling charge holder; wherein the propelling charge holder includes multiple propelling charge holder segments; wherein each of the propelling charge holder segments has a curved free shape with a central portion closer to a centerline of the projectile, and with ends located at opposite ends of the central portion, with the ends bowed radially outward away from the center line of the projectile; and wherein an inward radial force provided by the propelling charge increments is applied to the propelling charge holder segments to combine the propelling charge holder segments to form the propelling charge holder. 12. The projectile of claim 11, further comprising fins hingedly coupled to the body; wherein the fins may be retracted or deployed; and wherein at least part of the inward radial force is supplied by the fins when the fins are retracted. 13. The projectile of claim 11, further comprising an igniter holder with an annular flange; wherein at least part of the inward radial force is supplied by the annular flange. 14. The projectile of claim 11, wherein hooked ends of the propelling charge holder segments engage a flange on an aft protrusion of the body, when the inward radial force is applied to the propelling charge holder segments; and wherein removal of the inward radial force causes disengagement of the hooked ends from the flange. 15. A projectile comprising: a projectile body; a propelling charge holder separably coupled to the projectile body; external propelling charge increments at least partially surrounding the propelling charge holder; and fins hingedly coupled to the body; wherein the propelling charge holder includes multiple propelling charge holder segments that are separable from one another during flight of the projectile wherein the fins are retractable and deployable; and wherein blades of the fins each have a notch into which parts of the propelling charge holder segments protrude therein when the fins are retracted. 16. The projectile of claim 15, wherein the separable segments are at least partially surrounded by the propelling charge increments. 17. The projectile of claim 15 wherein the external propelling charge increments have recesses for receiving therein the fins. 18. A projectile of claim 15, wherein each of the external propelling charge increments includes a shell with a propellant within the shell; and wherein the shell is made of a material that is consumed by combustion of the propellant. 19. The projectile of claim 18, wherein the material includes felted nitrocellulose. 20. The projectile of claim 18, wherein the propelling charge holder is also made of a material that is consumed by combustion of the propellant. 21. The projectile of claim 15, wherein the propelling charge holder is made of a material that is substantially consumed during combustion of the propelling charge increments. 22. The projectile of claim 21, wherein the propelling charge holder is threadedly engaged with the projectile body. 23. The projectile of claim 21, wherein the propelling charge holder includes resilient fingers that engage the projectile body.
이 특허에 인용된 특허 (4)
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Andersson Bernt (Eskilstuna SEX), Device in a launch unit for a mortar projectile.
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Asikainen Niilo (Tampere FIX), Ignition cartridge system.
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Frost John J. (Alexandria VA), Mortar training ammunition device having independently rotatable vent closure rings.
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Jensen, Jens C., Practice projectile with variable range.
이 특허를 인용한 특허 (2)
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Harjula, Timo Pekka; Pesonen, Ville-Pekka, Increment charge for fin-stabilized mortar projectile.
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Decker, Ryan; Yakimenko, Oleg; Hollis, Michael; Chesnulovitch, Douglas; Chaplin, Raymond; Dundon, Gary; Farbanish, Gregory, Mortar projectile with guided deceleration system for delivering a payload.
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