Thrust control valve and flying object

Patent metadata

Field	Value
Publication number	US-10138844-B2
Application number	US-201314908349-A
Country	US
Kind code	B2
Filing date	Oct 18, 2013
Priority date	Aug 12, 2013
Publication date	Nov 27, 2018
Grant date	Nov 27, 2018

Abstract

A thrust control valve equipped with: a valve element, in which a gas injection passage, through which an operating gas is injected, is formed, with a valve-seating surface being formed in the gas injection passage; and a valve stem, which is provided in the interior of the gas injection passage and has a seated surface that makes contact with the valve-seating surface. A guide surface which makes contact with the inner circumferential surface of the gas injection passage of the valve element is formed on the outer circumferential surface of the valve stem. The guide surface is formed downstream from the seated surface in the direction of flow of the operating gas. A V-groove through which the operating gas flows is formed at the tip of the valve stem, downstream from the seated surface in which the guide surface is formed.

First claim

The invention claimed is:

1. A thrust control valve comprising:
a valve element in which a gas injection passage, through which an operating gas to be injected flows, is formed and a valve-seating surface is formed in the gas injection passage;
a valve stem that is provided inside the gas injection passage and has a valve-seated surface that makes contact with the valve-seating surface;
a guide surface that is formed at an outer circumferential surface of a tip of the valve stem located on the downstream side of the valve-seated surface in the gas flow direction of the operating gas and that makes contact with an inner circumferential surface of the gas injection passage of the valve element even in a case where the valve-seated surface has been separated from the valve-seating surface; and
a gas flow part, through which the operating gas flows, formed in the tip;
wherein
an area of the flow path between the gas flow part and an inner surface of the gas injection passage varies depending on a distance between the valve-seating surface of the valve element and the valve-seated surface of the valve stem, and
the thrust control valve is closed when the valve-seated surface of the valve stem comes in contact with the valve-seating surface of the valve element.

2. The thrust control valve according to claim 1 ,
wherein the valve stem has a gas flow part, through which the operating gas flows, in the tip.

3. The thrust control valve according to claim 2 ,
wherein the gas flow part is a V-groove that has a top part on an upstream side and widens from the top part toward the downstream side.

4. The thrust control valve according to claim 3 ,
wherein the gas flow part is a plurality of the V-grooves made to intersect each other so as to pass through the center of the valve stem.

5. The thrust control valve according to claim 3 ,
wherein the tip has a blocking part provided between the top part of the V-groove and the valve-seated surface.

6. The thrust control valve according to claim 2 ,
wherein the gas flow part has a groove that is formed in an outer circumferential surface of the tip from the upstream side in the gas flow direction to the downstream side.

7. The thrust control valve according to claim 2 ,
wherein a gas inflow port that allows the operating gas to flow into the gas injection passage is connected to the gas injection passage, and
wherein the flow path area of the gas flow part nearer to the gas inflow port is smaller than the flow path area of the gas flow part farther from the gas inflow port.

8. The thrust control valve according to claim 1 , further comprising:
a flow straightening plate that is provided on the upstream side of the valve-seated surface in the gas flow direction and straightens the flow of the operating gas that flows through the gas injection passage.

9. A flying object comprising:
the thrust control valve according claim 1 .

10. A thrust control valve comprising:
a valve element in which a gas injection passage, through which an operating gas to be injected flows, is formed and a valve-seating surface is formed in the gas injection passage;
a valve stem that is provided inside the gas injection passage and has a valve-seated surface that makes contact with the valve-seating surface;
a guide surface that is formed at an outer circumferential surface of a tip of the valve stem located on the downstream side of the valve-seated surface in the gas flow direction of the operating gas and that makes contact with an inner circumferential surface of the gas injection passage of the valve element even in a case where the valve-seated surface has been separated from the valve-seating surface;
a gas flow part, through which the operating gas flows, formed in the tip; and
a flow straightening plate that is provided on the upstream side of the valve-seated surface in the gas flow direction of the operating gas and straightens the flow of the operating gas that flows through the gas injection passage,
wherein
an area of the flow path between the gas flow part and an inner surface of the gas injection passage varies depending on a distance between the valve-seating surface of the valve element and the valve-seated surface of the valve stem, and
the thrust control valve is closed when the valve seated-surface of the valve stem comes in contact with the valve-seating surface of the valve element.

11. A flying object comprising:
the thrust control valve according to claim 10 .

Assignees

• Mitsubishi Heavy Ind Ltd

Inventors

• Hidaka Shozo
• Moriwaki Atsushi
• Futahashi Kensuke
• Hosaka Shuhei
• Nagase Masaaki
• Kojima Kohei
• Inada Mitsuru

Classifications

• B64D31/00

  Power plant control systems; Arrangement of power plant control systems in aircraft · CPC title

• B64D27/023

  of rocket type, e.g. for assisting taking-off or braking · CPC title

• F02K9/94

  Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants · CPC title

• F02K9/86 Primary

  using nozzle throats of adjustable cross- section {(F02K9/978 takes precedence)} · CPC title

• F05D2250/75

  given by its similarity to a letter, e.g. T-shaped · CPC title