JPS63145797U - - Google Patents
Info
- Publication number
- JPS63145797U JPS63145797U JP3839987U JP3839987U JPS63145797U JP S63145797 U JPS63145797 U JP S63145797U JP 3839987 U JP3839987 U JP 3839987U JP 3839987 U JP3839987 U JP 3839987U JP S63145797 U JPS63145797 U JP S63145797U
- Authority
- JP
- Japan
- Prior art keywords
- control surface
- drive unit
- power
- torque tube
- gear box
- 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
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Transmission Devices (AREA)
- Retarders (AREA)
Description
第1図は本考案の一実施例の平面図、第2図は
その制御概念図、第3図はその作動例を示す説明
図、第4図は従来の例の平面図である。
図面中、1は前縁フラツプ、2は主翼、3はギ
ヤード・ロータリー・アクチユエータ、4はパワ
ー・ドライブ・ユニツト、5はトルク・チユーブ
、6は変速ギヤ・ボツクスをそれぞれ示す。
FIG. 1 is a plan view of an embodiment of the present invention, FIG. 2 is a conceptual diagram of its control, FIG. 3 is an explanatory diagram showing an example of its operation, and FIG. 4 is a plan view of a conventional example. In the drawings, 1 is a leading edge flap, 2 is a main wing, 3 is a geared rotary actuator, 4 is a power drive unit, 5 is a torque tube, and 6 is a transmission gear box.
Claims (1)
・ドライブ・ユニツト、同パワー・ドライブ・ユ
ニツトからの回転力を伝達するトルク・チユーブ
、トルク・チユーブにより伝えられた回転を減速
して各舵面を作動させる機械式アクチユエータ、
各アクチユエータの中間に置かれた変速比可変の
変速ギア・ボツクスなどから構成され、パワー・
ドライブ・ユニツトへの駆動信号と変速ギア・ボ
ツクスへのギア比設定信号の組み合わせにより、
分割された各舵面の作動角度を自由に設定できる
ようにしたことを特徴とする航空機舵面の作動装
置。 A control surface divided into two or more parts, a power drive unit that serves as the drive source, a torque tube that transmits the rotational force from the power drive unit, and a control surface that decelerates the rotation transmitted by the torque tube to each rudder. mechanical actuator to actuate the surface;
It consists of a variable gear box with a variable transmission ratio placed between each actuator, and the power
By combining the drive signal to the drive unit and the gear ratio setting signal to the transmission gear box,
An operating device for an aircraft control surface, characterized in that the operating angle of each divided control surface can be freely set.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3839987U JPS63145797U (en) | 1987-03-18 | 1987-03-18 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3839987U JPS63145797U (en) | 1987-03-18 | 1987-03-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63145797U true JPS63145797U (en) | 1988-09-26 |
Family
ID=30850606
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3839987U Pending JPS63145797U (en) | 1987-03-18 | 1987-03-18 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63145797U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4638444B2 (en) * | 2003-11-12 | 2011-02-23 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | Load limiting method in drive system for aircraft high lift device |
-
1987
- 1987-03-18 JP JP3839987U patent/JPS63145797U/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4638444B2 (en) * | 2003-11-12 | 2011-02-23 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | Load limiting method in drive system for aircraft high lift device |