JPS6399U - - Google Patents
Info
- Publication number
- JPS6399U JPS6399U JP9411486U JP9411486U JPS6399U JP S6399 U JPS6399 U JP S6399U JP 9411486 U JP9411486 U JP 9411486U JP 9411486 U JP9411486 U JP 9411486U JP S6399 U JPS6399 U JP S6399U
- Authority
- JP
- Japan
- Prior art keywords
- leading edge
- actuators
- edge flap
- lift device
- aircraft
- 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
- 238000007796 conventional method Methods 0.000 description 1
Description
第１図は本考案の一実施例を示す平面図、第２
図は第１図のＡ―Ａ断面図、第３図は同他の実施
例を示す平面図、第４図は従来技例を示す平面図
である。
１……主翼、２ａ〜２ｅ……前縁フラツプ片、
５ａ〜５ｅ，１５ａ〜１５ｅ……アクチユエータ
、７，１７……コマンドユニツト。
Fig. 1 is a plan view showing one embodiment of the present invention;
The drawings are a sectional view taken along the line AA in FIG. 1, FIG. 3 is a plan view showing another embodiment, and FIG. 4 is a plan view showing a conventional technique. 1... Main wing, 2a to 2e... Leading edge flap piece,
5a to 5e, 15a to 15e... actuator, 7, 17... command unit.
Claims (1)
らなる前縁フラツプを備える航空機の高揚力装置
において、前記複数の前縁フラツプ片に対しそれ
ぞれ配設された複数のアクチユエータと、前記複
数のアクチユエータに対し出力端がそれぞれ結線
され操舵信号を与えるコマンドユニツトとを具備
してなることを特徴とする航空機の高揚力装置。 In a high lift device for an aircraft equipped with a leading edge flap consisting of a plurality of leading edge flap pieces divided in the span direction, a plurality of actuators respectively disposed for the plurality of leading edge flap pieces, and a plurality of actuators for the plurality of actuators are provided. 1. A high-lift device for an aircraft, comprising a command unit whose output ends are connected to each other and which give a steering signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9411486U JPS6399U (en) | 1986-06-20 | 1986-06-20 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9411486U JPS6399U (en) | 1986-06-20 | 1986-06-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6399U true JPS6399U (en) | 1988-01-05 |
Family
ID=30957264
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9411486U Pending JPS6399U (en) | 1986-06-20 | 1986-06-20 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6399U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007525370A (en) * | 2004-02-27 | 2007-09-06 | ザ・ボーイング・カンパニー | Aircraft leading edge system and corresponding sizing method |
-
1986
- 1986-06-20 JP JP9411486U patent/JPS6399U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007525370A (en) * | 2004-02-27 | 2007-09-06 | ザ・ボーイング・カンパニー | Aircraft leading edge system and corresponding sizing method |
| JP4703638B2 (en) * | 2004-02-27 | 2011-06-15 | ザ・ボーイング・カンパニー | Aircraft leading edge system and corresponding sizing method |