JPS5818598U - Aircraft rotor support system - Google Patents

Aircraft rotor support system

Info

Publication number
JPS5818598U
JPS5818598U JP11166181U JP11166181U JPS5818598U JP S5818598 U JPS5818598 U JP S5818598U JP 11166181 U JP11166181 U JP 11166181U JP 11166181 U JP11166181 U JP 11166181U JP S5818598 U JPS5818598 U JP S5818598U
Authority
JP
Japan
Prior art keywords
support system
rotor support
aircraft rotor
rotation axis
rotation
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
JP11166181U
Other languages
Japanese (ja)
Inventor
弘 萩原
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 by Individual filed Critical Individual
Priority to JP11166181U priority Critical patent/JPS5818598U/en
Publication of JPS5818598U publication Critical patent/JPS5818598U/en
Pending legal-status Critical Current

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Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

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

第1図はラジコンヘリコプタ−の側面図、第2図は従来
例を示す第1図の主回転翼部の平面図、第3図は第2図
のm−m’断面図、第4図は第2図に代わる本考案装置
の一実施例を示す平面図、第5図は同じく本考案装置の
他実施例を示す平面図、第6図は第4図、第5図のIV
−IV’断面図である。 2・・・・・・回転軸、5・・・・・・ドラッグヒンジ
、7・・四回転翼、10・・・・・・風圧中心、11・
・・・・・回転軸の中心、12・・・・・・基線、θ3
・・・・・・ずらし角度。
Fig. 1 is a side view of a radio-controlled helicopter, Fig. 2 is a plan view of the main rotor section of Fig. 1 showing a conventional example, Fig. 3 is a sectional view taken along line mm' in Fig. 2, and Fig. 4 is a FIG. 5 is a plan view showing another embodiment of the device of the present invention in place of FIG. 2, FIG. 6 is a plan view showing another embodiment of the device of the present invention, and FIG.
-IV' sectional view. 2...Rotation axis, 5...Drag hinge, 7...Four rotary blades, 10...Wind pressure center, 11...
... Center of rotation axis, 12 ... Base line, θ3
・・・・・・Shift angle.

Claims (2)

【実用新案登録請求の範囲】[Scope of utility model registration request] (1)回転翼と該翼の回転軸と番枢支ドラッグヒンジを
前記回転翼の風圧中心と前記回転軸の中心とを結ぶ基線
よりも回転方向側にずらしたことを特徴とする航空機の
回転翼支持装置。
(1) Rotation of an aircraft characterized in that a rotor blade, a rotation axis of the blade, and a pivot drag hinge are shifted toward the rotation direction side with respect to a base line connecting the wind pressure center of the rotor blade and the center of the rotation axis. Wing support device.
(2)ずらし角度を2°乃至3°にした実用新案登録請
求の範囲第1項記載の航空機の回転翼支持装置。
(2) The rotary wing support device for an aircraft according to claim 1, wherein the shift angle is 2° to 3°.
JP11166181U 1981-07-28 1981-07-28 Aircraft rotor support system Pending JPS5818598U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11166181U JPS5818598U (en) 1981-07-28 1981-07-28 Aircraft rotor support system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11166181U JPS5818598U (en) 1981-07-28 1981-07-28 Aircraft rotor support system

Publications (1)

Publication Number Publication Date
JPS5818598U true JPS5818598U (en) 1983-02-04

Family

ID=29906002

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11166181U Pending JPS5818598U (en) 1981-07-28 1981-07-28 Aircraft rotor support system

Country Status (1)

Country Link
JP (1) JPS5818598U (en)

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