JPS5819900U - Aircraft closed space temperature control device - Google Patents
Aircraft closed space temperature control deviceInfo
- Publication number
- JPS5819900U JPS5819900U JP11490381U JP11490381U JPS5819900U JP S5819900 U JPS5819900 U JP S5819900U JP 11490381 U JP11490381 U JP 11490381U JP 11490381 U JP11490381 U JP 11490381U JP S5819900 U JPS5819900 U JP S5819900U
- Authority
- JP
- Japan
- Prior art keywords
- closed space
- heat
- control device
- aircraft
- temperature control
- 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
Landscapes
- Temperature-Responsive Valves (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
図はこの考案にかかる実施例装置の要部の模式説明図で
ある。
1・・・エンジン、2・・・抽気管路、4・・・貨物室
(閉空間)、6・・・ヒートパイプ、7・・・吸熱部、
8・・・放熱部、9・・・バルブ、10・・・補助ヒー
トパイプ、11・・・吸熱部、12・・・放熱部、15
・・・温度感応体、16・・・リンク。The figure is a schematic explanatory diagram of the main parts of the embodiment device according to the invention. DESCRIPTION OF SYMBOLS 1... Engine, 2... Air extraction pipe line, 4... Cargo compartment (closed space), 6... Heat pipe, 7... Heat absorption part,
8... Heat radiation part, 9... Valve, 10... Auxiliary heat pipe, 11... Heat absorption part, 12... Heat radiation part, 15
...Temperature sensitive body, 16...link.
Claims (1)
パイプの吸熱部を挿入し、その放熱部を機体の閉空間の
内部に挿入するとともに、前記ヒートパイプにその流路
面積を制御するバルブを介在させ、さらにこのバルブめ
作動機構とリンクを介して連結する温度感応体を設け、
かつこの温度感応体と前記閉空間との間にそれぞれを放
熱側、吸熱側とする補助ヒートパイプを設けてなり、前
記温度感応体の温度便化に伴う体積変化により前記リン
クを介して前記バルブの作動機構をして前記ヒートパイ
プの流路面積を制御せしめるようにした航空機の閉空間
の温度制御装置。The heat absorbing part of the heat pipe is inserted into the air extraction pipe that extracts high temperature, high pressure air from the engine, and the heat dissipating part is inserted into the closed space of the aircraft, and a valve is interposed in the heat pipe to control the flow path area. Further, a temperature sensitive body is provided which is connected to the valve operating mechanism via a link.
Further, an auxiliary heat pipe is provided between the temperature sensitive body and the closed space, and has a heat radiation side and a heat absorption side, respectively. A temperature control device for a closed space of an aircraft, wherein the operating mechanism is used to control the flow path area of the heat pipe.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11490381U JPS6030160Y2 (en) | 1981-07-31 | 1981-07-31 | Aircraft closed space temperature control device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11490381U JPS6030160Y2 (en) | 1981-07-31 | 1981-07-31 | Aircraft closed space temperature control device |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5819900U true JPS5819900U (en) | 1983-02-07 |
JPS6030160Y2 JPS6030160Y2 (en) | 1985-09-10 |
Family
ID=29909181
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11490381U Expired JPS6030160Y2 (en) | 1981-07-31 | 1981-07-31 | Aircraft closed space temperature control device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6030160Y2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59149819A (en) * | 1983-02-15 | 1984-08-27 | Shiraki Kinzoku Kogyo Kk | Air cleaner |
-
1981
- 1981-07-31 JP JP11490381U patent/JPS6030160Y2/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59149819A (en) * | 1983-02-15 | 1984-08-27 | Shiraki Kinzoku Kogyo Kk | Air cleaner |
Also Published As
Publication number | Publication date |
---|---|
JPS6030160Y2 (en) | 1985-09-10 |
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