JPS6385500U - - Google Patents
Info
- Publication number
- JPS6385500U JPS6385500U JP17925586U JP17925586U JPS6385500U JP S6385500 U JPS6385500 U JP S6385500U JP 17925586 U JP17925586 U JP 17925586U JP 17925586 U JP17925586 U JP 17925586U JP S6385500 U JPS6385500 U JP S6385500U
- Authority
- JP
- Japan
- Prior art keywords
- air intake
- refrigerant
- flexible plate
- state quantity
- actuators
- 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.)
- Pending
Links
- 239000003507 refrigerant Substances 0.000 claims 4
- 238000001816 cooling Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Testing Of Engines (AREA)
Description
第1図は、本考案の一実施例としての空気取入
口の断面図、第2図は、従来の空気取入口の断面
図、第3図は、本考案の他の実施例にかかる空気
取入口の断面図、第4図は、第3図丸A部の拡大
図、第5図は、第3図の可撓板上での流入空気の
状態量を示す模式図、第6図は、第2図の空気取
入口内壁における流入空気の状態量を示す模式図
である。
1……可撓板、2……アクチユエータ、3……
ヒンジ、7,8……状態量センサ。
FIG. 1 is a sectional view of an air intake as an embodiment of the present invention, FIG. 2 is a sectional view of a conventional air intake, and FIG. 3 is an air intake according to another embodiment of the present invention. A sectional view of the inlet, FIG. 4 is an enlarged view of circle A in FIG. 3, FIG. 5 is a schematic diagram showing the state quantity of the incoming air on the flexible plate in FIG. FIG. 3 is a schematic diagram showing the state quantity of incoming air on the inner wall of the air intake port in FIG. 2; 1... Flexible plate, 2... Actuator, 3...
Hinge, 7, 8...state quantity sensor.
Claims (1)
部にヒンジを介してエンジン本体内壁に複数個配
設されたアクチユエータと、該空気取入口内部に
アクチユエータを介して内張りされる可撓板と、
可撓板に接してアクチユエータ側に設けられる流
通管と、前記流通管に冷媒を供給する冷媒源と、
可撓板等の空気取入口内壁に設けられた流入空気
の状態量計測器と、前記状態量計測器の出力を入
力し、空気取入口の最適形状及び冷媒の最適冷却
条件を演算してアクチユエータ及び冷媒源に制御
信号を出力する制御器を具備するエンジンの空気
取入口。 At the air intake of the engine, a plurality of actuators are disposed on the inner wall of the engine body via hinges inside the air intake, and a flexible plate is lined inside the air intake via the actuators.
a flow pipe provided on the actuator side in contact with the flexible plate; a refrigerant source supplying refrigerant to the flow pipe;
The state quantity measuring device of the incoming air provided on the inner wall of the air intake port, such as a flexible plate, and the output of the state quantity measuring device are input, and the optimum shape of the air intake port and the optimum cooling conditions of the refrigerant are calculated, and the actuator and a controller for outputting a control signal to a refrigerant source.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17925586U JPS6385500U (en) | 1986-11-21 | 1986-11-21 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17925586U JPS6385500U (en) | 1986-11-21 | 1986-11-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6385500U true JPS6385500U (en) | 1988-06-03 |
Family
ID=31122156
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP17925586U Pending JPS6385500U (en) | 1986-11-21 | 1986-11-21 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6385500U (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004084669A (en) * | 2002-08-27 | 2004-03-18 | General Electric Co <Ge> | System and method for actively changing effective flow-through area of intake part region of aircraft engine |
JP2008524060A (en) * | 2004-12-20 | 2008-07-10 | エアバス フランス | Air intake device for ventilation |
JP2008309152A (en) * | 2007-06-13 | 2008-12-25 | United Technol Corp <Utc> | Nacelle assembly, gas turbine engine, and method of increasing effective boundary layer thickness of inlet lip section of nacelle |
JP2013227977A (en) * | 2012-04-24 | 2013-11-07 | General Electric Co <Ge> | Gas turbine inlet system and method |
JP2017523089A (en) * | 2014-08-14 | 2017-08-17 | ガルフストリーム エアロスペース コーポレーション | System and method for controlling the pressure field around an aircraft in flight |
-
1986
- 1986-11-21 JP JP17925586U patent/JPS6385500U/ja active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004084669A (en) * | 2002-08-27 | 2004-03-18 | General Electric Co <Ge> | System and method for actively changing effective flow-through area of intake part region of aircraft engine |
JP2008524060A (en) * | 2004-12-20 | 2008-07-10 | エアバス フランス | Air intake device for ventilation |
JP2008309152A (en) * | 2007-06-13 | 2008-12-25 | United Technol Corp <Utc> | Nacelle assembly, gas turbine engine, and method of increasing effective boundary layer thickness of inlet lip section of nacelle |
JP2013227977A (en) * | 2012-04-24 | 2013-11-07 | General Electric Co <Ge> | Gas turbine inlet system and method |
EP2657460A3 (en) * | 2012-04-24 | 2018-04-25 | General Electric Company | Gas turbine inlet system and method |
JP2017523089A (en) * | 2014-08-14 | 2017-08-17 | ガルフストリーム エアロスペース コーポレーション | System and method for controlling the pressure field around an aircraft in flight |