JPS63154399U - - Google Patents
Info
- Publication number
- JPS63154399U JPS63154399U JP4694987U JP4694987U JPS63154399U JP S63154399 U JPS63154399 U JP S63154399U JP 4694987 U JP4694987 U JP 4694987U JP 4694987 U JP4694987 U JP 4694987U JP S63154399 U JPS63154399 U JP S63154399U
- Authority
- JP
- Japan
- Prior art keywords
- main wing
- pressure gas
- gas source
- slit
- reduction device
- 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
- 238000010586 diagram Methods 0.000 description 3
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Toys (AREA)
Description
第１図は本考案の一実施例の立面を示す説明図
、第２図は同実施例の平面を示す説明図、第３図
は主翼平面形状を示す平面図、第４図は従来の誘
導抵抗減少装置の説明図である。
図面中、１は主翼、２はエンジン、３はバルブ
、４は配管、５はスリツト、６は高圧ガス、８は
端板、９はウイングレツト、をそれぞれ示す。
Fig. 1 is an explanatory diagram showing an elevation of one embodiment of the present invention, Fig. 2 is an explanatory diagram showing a plan view of the embodiment, Fig. 3 is a plan view showing the planar shape of the main wing, and Fig. 4 is an explanatory diagram showing the planar shape of the main wing. It is an explanatory view of an induced resistance reduction device. In the drawings, 1 is a main wing, 2 is an engine, 3 is a valve, 4 is a pipe, 5 is a slit, 6 is a high pressure gas, 8 is an end plate, and 9 is a winglet.
Claims (1)
ト、高圧ガス源及び高圧ガス源をスリツトに導く
配管からなることを特徴とする航空機の誘導抵抗
減少装置。 1. An induced drag reduction device for an aircraft, comprising a slit provided at the end of each main wing and opening into the main wing surface, a high-pressure gas source, and piping that guides the high-pressure gas source to the slit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4694987U JPH0437839Y2 (en) | 1987-03-31 | 1987-03-31 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4694987U JPH0437839Y2 (en) | 1987-03-31 | 1987-03-31 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63154399U true JPS63154399U (en) | 1988-10-11 |
| JPH0437839Y2 JPH0437839Y2 (en) | 1992-09-04 |
Family
ID=30867090
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4694987U Expired JPH0437839Y2 (en) | 1987-03-31 | 1987-03-31 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0437839Y2 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007523003A (en) * | 2004-02-20 | 2007-08-16 | ザ・ボーイング・カンパニー | Rear wake flow control device and control method |
| JP2013530098A (en) * | 2010-07-14 | 2013-07-25 | エアバス オペレーションズ リミテッド | Wing tip equipment |
| JP2018505818A (en) * | 2015-03-03 | 2018-03-01 | アマゾン テクノロジーズ インコーポレイテッド | Unmanned air transport means with a three-way wing configuration |
-
1987
- 1987-03-31 JP JP4694987U patent/JPH0437839Y2/ja not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007523003A (en) * | 2004-02-20 | 2007-08-16 | ザ・ボーイング・カンパニー | Rear wake flow control device and control method |
| JP2013530098A (en) * | 2010-07-14 | 2013-07-25 | エアバス オペレーションズ リミテッド | Wing tip equipment |
| JP2018505818A (en) * | 2015-03-03 | 2018-03-01 | アマゾン テクノロジーズ インコーポレイテッド | Unmanned air transport means with a three-way wing configuration |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0437839Y2 (en) | 1992-09-04 |
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