JPS63133680U - - Google Patents
Info
- Publication number
- JPS63133680U JPS63133680U JP2527287U JP2527287U JPS63133680U JP S63133680 U JPS63133680 U JP S63133680U JP 2527287 U JP2527287 U JP 2527287U JP 2527287 U JP2527287 U JP 2527287U JP S63133680 U JPS63133680 U JP S63133680U
- Authority
- JP
- Japan
- Prior art keywords
- inner cylinder
- heat
- sensitive element
- spring
- fixed
- 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
- 239000012530 fluid Substances 0.000 claims 2
Landscapes
- Temperature-Responsive Valves (AREA)
- Control Of Temperature (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2527287U JPS63133680U (en:Method) | 1987-02-23 | 1987-02-23 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2527287U JPS63133680U (en:Method) | 1987-02-23 | 1987-02-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63133680U true JPS63133680U (en:Method) | 1988-09-01 |
Family
ID=30825269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2527287U Pending JPS63133680U (en:Method) | 1987-02-23 | 1987-02-23 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63133680U (en:Method) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013247215A (ja) * | 2012-05-25 | 2013-12-09 | Nabtesco Corp | 航空機搭載用電装品の液冷システム |
-
1987
- 1987-02-23 JP JP2527287U patent/JPS63133680U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2013247215A (ja) * | 2012-05-25 | 2013-12-09 | Nabtesco Corp | 航空機搭載用電装品の液冷システム |
| US9677832B2 (en) | 2012-05-25 | 2017-06-13 | Nabtesco Corporation | Liquid cooling system for electric component mounted in aircraft |