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
Description
第１図は本考案の第１実施例の図でａは左側面
図、ｂは下面図、第２図は本考案の第２実施例の
図でａは左側面図、ｂは下面図、第３図は第１図
に対応して示した従来例のスクープ型の図、第４
図は同じく従来例のフラツシユ型の図である。
５…境界層、６…胴体、１１…ダイバータ、１
２…隔板、１３…フラツシユ型空気取入口、１４
…リツプ。
Fig. 1 is a view of the first embodiment of the present invention, a is a left side view, b is a bottom view, and Fig. 2 is a view of the second embodiment of the present invention, a is a left side view, b is a bottom view, Figure 3 is a scoop-type diagram of the conventional example shown corresponding to Figure 1;
The figure is also a diagram of a conventional flash type. 5... Boundary layer, 6... Body, 11... Diverter, 1
2... Partition plate, 13... Flush type air intake, 14
…Rip.
Claims (1)
排除可能に設けられたダイバータと、同ダイバー
タの外方にほゞ胴体表面に沿つて設けられた隔板
と、同隔板から胴体内方にむかつて設けられたフ
ラツシユ型空気取入口とを具備してなることを特
徴とするダイバータ付フラツシユ型空気取入口。 A diverter is installed along the fuselage surface of the aircraft to remove boundary layer flow with small resistance, a bulkhead is installed outside the diverter along the fuselage surface, and a flow from the divider to the inside of the fuselage is provided. 1. A flush type air intake with a diverter, comprising: a flush type air intake provided in one direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9506388U JPH0216399U (en) | 1988-07-20 | 1988-07-20 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9506388U JPH0216399U (en) | 1988-07-20 | 1988-07-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0216399U true JPH0216399U (en) | 1990-02-01 |
Family
ID=31319678
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9506388U Pending JPH0216399U (en) | 1988-07-20 | 1988-07-20 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0216399U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008105671A (en) * | 2006-10-26 | 2008-05-08 | Boeing Co:The | Air inlet apparatus used in relation to high-speed airborne mobile platform and used on fuselage of jet aircraft, aircraft and method for forming inlet on outer surface of fuselage of jet aircraft |
-
1988
- 1988-07-20 JP JP9506388U patent/JPH0216399U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008105671A (en) * | 2006-10-26 | 2008-05-08 | Boeing Co:The | Air inlet apparatus used in relation to high-speed airborne mobile platform and used on fuselage of jet aircraft, aircraft and method for forming inlet on outer surface of fuselage of jet aircraft |