JPS6354599U - - Google Patents

Info

Publication number
JPS6354599U
JPS6354599U JP15050886U JP15050886U JPS6354599U JP S6354599 U JPS6354599 U JP S6354599U JP 15050886 U JP15050886 U JP 15050886U JP 15050886 U JP15050886 U JP 15050886U JP S6354599 U JPS6354599 U JP S6354599U
Authority
JP
Japan
Prior art keywords
aircraft
wing
low speed
attack
expands
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
Application number
JP15050886U
Other languages
Japanese (ja)
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP15050886U priority Critical patent/JPS6354599U/ja
Publication of JPS6354599U publication Critical patent/JPS6354599U/ja
Pending legal-status Critical Current

Links

Description

【図面の簡単な説明】[Brief explanation of drawings]

図面はこの考案の実施例を示すもので、第1図
Aは第1実施例の高速巡航時の外観構成を示す正
面図、第1図Bは同第1実施例の低速時の外観構
成を示す正面図、第2図は第2実施例の外観構成
を示す正面図、第3図は第3実施例の外観構成を
示す正面図である。 10……飛行機、11……主翼、12……スポ
イラ、13……補助翼、14……翼端板、15…
…フラツプ、16……揚力分布。
The drawings show an embodiment of this invention. FIG. 1A is a front view showing the external configuration of the first embodiment at high speed cruising, and FIG. 1B is a front view showing the external configuration of the first embodiment at low speed. FIG. 2 is a front view showing the external structure of the second embodiment, and FIG. 3 is a front view showing the external structure of the third embodiment. 10... Airplane, 11... Main wing, 12... Spoiler, 13... Aileron, 14... Wing end plate, 15...
...flap, 16...lift force distribution.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 航空機の主翼端部に設けられ、航空機が低速時
、大迎角時にのみ展開して揚力を発生させること
を特徴とする翼端板。
A wing end plate that is installed at the end of an aircraft's main wing and expands only when the aircraft is at low speed or at a large angle of attack to generate lift.
JP15050886U 1986-09-30 1986-09-30 Pending JPS6354599U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15050886U JPS6354599U (en) 1986-09-30 1986-09-30

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15050886U JPS6354599U (en) 1986-09-30 1986-09-30

Publications (1)

Publication Number Publication Date
JPS6354599U true JPS6354599U (en) 1988-04-12

Family

ID=31066716

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15050886U Pending JPS6354599U (en) 1986-09-30 1986-09-30

Country Status (1)

Country Link
JP (1) JPS6354599U (en)

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