JPH043299U - - Google Patents
Info
- Publication number
- JPH043299U JPH043299U JP3902090U JP3902090U JPH043299U JP H043299 U JPH043299 U JP H043299U JP 3902090 U JP3902090 U JP 3902090U JP 3902090 U JP3902090 U JP 3902090U JP H043299 U JPH043299 U JP H043299U
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- thrust
- combustion gas
- fixed nozzle
- nozzles
- 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.)
- Granted
Links
- 239000000567 combustion gas Substances 0.000 claims 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
Landscapes
- Nozzles (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Description
第１図は本考案の作用の説明図、第２図は本考
案の第１実施例の側面図、第３図は本考案の第２
実施例の側面図、第４図は本考案の第３実施例の
側面図、第５図は従来例の側面図である。
１……固定ノズル、２……横方向成分ノズル、
２ａ……ノズル、３……横方向成分ノズル用弁、
４……アクチユエータ、６……チヤンバ（燃焼室
）、７……ロール方向成分用ノズル、８……外筒
、９……バルブ、１２……管。
Figure 1 is an explanatory diagram of the operation of the present invention, Figure 2 is a side view of the first embodiment of the present invention, and Figure 3 is the second embodiment of the present invention.
FIG. 4 is a side view of the third embodiment of the present invention, and FIG. 5 is a side view of the conventional example. 1... Fixed nozzle, 2... Horizontal component nozzle,
2a... nozzle, 3... lateral component nozzle valve,
4... actuator, 6... chamber (combustion chamber), 7... nozzle for roll direction component, 8... outer cylinder, 9... valve, 12... pipe.
Claims (1)
射させて飛しよう体の推力方向を変える推力偏向
装置において、チヤンバ後方に機軸に沿つて連接
された固定ノズルと、チヤンバから固定ノズルに
至る範囲の所定の位置に機軸と非平行に設けられ
た複数のノズルと、同複数のノズルに上記燃焼ガ
スを送給・遮断可能に設けられたバルブと、同バ
ルブの開度を変更可能なアクチユエータとを具備
してなることを特徴とする飛しよう体の推力偏向
装置。 In a thrust deflection device that changes the thrust direction of a flying object by injecting combustion gas burned in a chamber in multiple directions, there is a fixed nozzle connected along the axis behind the chamber, and a predetermined range from the chamber to the fixed nozzle. It is equipped with a plurality of nozzles provided non-parallel to the machine axis at positions, a valve provided to be able to supply and cut off the combustion gas to the plurality of nozzles, and an actuator capable of changing the opening degree of the valve. A thrust deflector for a flying body, which is characterized by:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1990039020U JP2522167Y2 (en) | 1990-04-13 | 1990-04-13 | Thrust deflection device for flying objects |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1990039020U JP2522167Y2 (en) | 1990-04-13 | 1990-04-13 | Thrust deflection device for flying objects |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH043299U true JPH043299U (en) | 1992-01-13 |
| JP2522167Y2 JP2522167Y2 (en) | 1997-01-08 |
Family
ID=31547545
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1990039020U Expired - Lifetime JP2522167Y2 (en) | 1990-04-13 | 1990-04-13 | Thrust deflection device for flying objects |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2522167Y2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7108223B2 (en) * | 2002-11-07 | 2006-09-19 | Raytheon Company | Missile control system and method |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59176197A (en) * | 1982-11-29 | 1984-10-05 | ソシエテ・ナシヨナ−ル・インダストリエル・アエロスパシエ−ル | Missile steering gear by gassy jet in lateral direction and missile |
| JPS62125896U (en) * | 1986-01-31 | 1987-08-10 |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4384690A (en) | 1981-03-06 | 1983-05-24 | The United States Of America As Represented By The Secretary Of The Navy | Thrust vector control for large deflection angles |
-
1990
- 1990-04-13 JP JP1990039020U patent/JP2522167Y2/en not_active Expired - Lifetime
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59176197A (en) * | 1982-11-29 | 1984-10-05 | ソシエテ・ナシヨナ−ル・インダストリエル・アエロスパシエ−ル | Missile steering gear by gassy jet in lateral direction and missile |
| JPS62125896U (en) * | 1986-01-31 | 1987-08-10 |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2522167Y2 (en) | 1997-01-08 |
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