IPC분류정보
| 국가/구분 |
United States(US) Patent
등록
|
| 국제특허분류(IPC7판) |
|
| 출원번호 |
US-0214484
(2002-08-05)
|
|
발명자
/ 주소 |
|
| 출원인 / 주소 |
- The United States of America as represented by the Secretary of the Navy
|
| 대리인 / 주소 |
Kasischke, James M.Oglo, Michael F.Nasser, Jean-Paul A.
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| 인용정보 |
피인용 횟수 :
2 인용 특허 :
8 |
초록
▼
A missile launch assembly for underwater vehicles includes a launch tank having mounted therein an expandable elastomeric disc and a turbine, a water inlet conduit, an impulse tank interconnecting the water inlet conduit and a missile launch tube, and a pump inducer mounted in the water inlet condui
A missile launch assembly for underwater vehicles includes a launch tank having mounted therein an expandable elastomeric disc and a turbine, a water inlet conduit, an impulse tank interconnecting the water inlet conduit and a missile launch tube, and a pump inducer mounted in the water inlet conduit and drivable by the turbine. Movement of the disc from an expanded to a non-expanded condition causes water in the launch tank to drive the turbine to drive the pump inducer to pump water from the water inlet conduit to the impulse tank and thence to the launch tube to effect launch of a missile therein.
대표청구항
▼
A missile launch assembly for underwater vehicles includes a launch tank having mounted therein an expandable elastomeric disc and a turbine, a water inlet conduit, an impulse tank interconnecting the water inlet conduit and a missile launch tube, and a pump inducer mounted in the water inlet condui
A missile launch assembly for underwater vehicles includes a launch tank having mounted therein an expandable elastomeric disc and a turbine, a water inlet conduit, an impulse tank interconnecting the water inlet conduit and a missile launch tube, and a pump inducer mounted in the water inlet conduit and drivable by the turbine. Movement of the disc from an expanded to a non-expanded condition causes water in the launch tank to drive the turbine to drive the pump inducer to pump water from the water inlet conduit to the impulse tank and thence to the launch tube to effect launch of a missile therein. 58, 19941000, Helmstetter, 273/167.H; US-5358249, 19941000, Mendralla, 273/173; US-5362047, 19941100, Shaw et al., 273/077.A; US-5362055, 19941100, Rennie, 273/167.H; US-5390924, 19950200, Antonious, 273/169; US-5395113, 19950300, Antonious, 273/169; US-5397126, 19950300, Allen, 273/167.H; US-5401021, 19950300, Allen, 273/077.A; US-5405136, 19950400, Hardman, 473/342; US-5405137, 19950400, Vincent et al., 273/173; US-5407202, 19950400, Igarashi, 273/169; US-RE34925, 19950500, McKeighen, 273/167.H; US-5417419, 19950500, Anderson et al., 273/078; US-5417559, 19950500, Schmidt, 428/186; US-5423535, 19950600, Shaw et al., 273/077.A; US-5429357, 19950700, Kobayashi, 273/080.2; US-5431396, 19950700, Shieh, 273/078; US-5433440, 19950
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