发明公开
- 专利标题: THRUST CONTROL VALVE AND FLYING OBJECT
- 专利标题(中): 推力控制阀和导弹
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申请号: EP13891432申请日: 2013-10-18
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公开(公告)号: EP3009650A4公开(公告)日: 2016-05-25
- 发明人: HIDAKA SHOZO , MORIWAKI ATSUSHI , FUTAHASHI KENSUKE , HOSAKA SHUHEI , NAGASE MASAAKI , KOJIMA KOHEI , INADA MITSURU
- 申请人: MITSUBISHI HEAVY IND LTD
- 专利权人: MITSUBISHI HEAVY IND LTD
- 当前专利权人: MITSUBISHI HEAVY IND LTD
- 优先权: JP2013167921 2013-08-12
- 主分类号: F02K9/80
- IPC分类号: F02K9/80 ; F02K9/86 ; F16K1/54
摘要:
A thrust control valve equipped with: a valve element (15), in which a gas injection passage (L), through which an operating gas (G) is injected, is formed, with a valve-seating surface (P1) being formed in the gas injection passage (L); and a valve stem (16), which is provided in the interior of the gas injection passage (L) and has a seated surface (P5) that makes contact with the valve-seating surface (P1). A guide surface (P4) which makes contact with the inner circumferential surface of the gas injection passage of the valve element (15) is formed on the outer circumferential surface of the valve stem (16). The guide surface (P4) is formed downstream from the seated surface (P5) in the direction of flow of the operating gas (G). A V-groove (31) through which the operating gas (G) flows is formed at the tip of the valve stem (16), downstream from the seated surface (P5) in which the guide surface (P4) is formed.
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