JPH0216399U - - Google Patents
Info
- Publication number
- JPH0216399U JPH0216399U JP9506388U JP9506388U JPH0216399U JP H0216399 U JPH0216399 U JP H0216399U JP 9506388 U JP9506388 U JP 9506388U JP 9506388 U JP9506388 U JP 9506388U JP H0216399 U JPH0216399 U JP H0216399U
- Authority
- JP
- Japan
- Prior art keywords
- diverter
- fuselage
- air intake
- type air
- flush type
- 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
- 238000010586 diagram Methods 0.000 description 2
- 238000005192 partition Methods 0.000 description 1
Landscapes
- Wind Motors (AREA)
- Ventilation (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9506388U JPH0216399U (ru) | 1988-07-20 | 1988-07-20 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9506388U JPH0216399U (ru) | 1988-07-20 | 1988-07-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0216399U true JPH0216399U (ru) | 1990-02-01 |
Family
ID=31319678
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9506388U Pending JPH0216399U (ru) | 1988-07-20 | 1988-07-20 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0216399U (ru) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008105671A (ja) * | 2006-10-26 | 2008-05-08 | Boeing Co:The | 高速の浮揚する可動式プラットフォームに関連して用いられ、ジェット航空機の胴体上で用いられる空気入口装置、航空機、および、ジェット航空機の胴体の外面上に入口を形成するための方法 |
-
1988
- 1988-07-20 JP JP9506388U patent/JPH0216399U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008105671A (ja) * | 2006-10-26 | 2008-05-08 | Boeing Co:The | 高速の浮揚する可動式プラットフォームに関連して用いられ、ジェット航空機の胴体上で用いられる空気入口装置、航空機、および、ジェット航空機の胴体の外面上に入口を形成するための方法 |