JPS59154299U - Model helicopter rotor head - Google Patents

Model helicopter rotor head

Info

Publication number
JPS59154299U
JPS59154299U JP4867883U JP4867883U JPS59154299U JP S59154299 U JPS59154299 U JP S59154299U JP 4867883 U JP4867883 U JP 4867883U JP 4867883 U JP4867883 U JP 4867883U JP S59154299 U JPS59154299 U JP S59154299U
Authority
JP
Japan
Prior art keywords
hub
shaft
center
attached
pin
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
Application number
JP4867883U
Other languages
Japanese (ja)
Other versions
JPH0236558Y2 (en
Inventor
古市 精克
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 JP4867883U priority Critical patent/JPS59154299U/en
Publication of JPS59154299U publication Critical patent/JPS59154299U/en
Application granted granted Critical
Publication of JPH0236558Y2 publication Critical patent/JPH0236558Y2/ja
Granted 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) [Abstract] 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図はこの考案の側面図。第2図は第1図の平面図で
各内部構造を点線で示す。第3図はダンパーゴムの側面
図である。 図中、1・・・軸管、14・・・操舵腕、15・・・操
舵盤、2・・・センターハブ、21・・・シーソーピン
、22・・・センターハブの中心線、3・・・当金、4
・・・側ハブ、41・・・ハブ軸、42・・・フラッピ
ングピン、43・・・ハブ軸の中心線、44・・・当た
り板、45・・・ビス、46・・・操作腕、47・・・
ユニバーサルホール、48・・・ドラッグピン、5・・
・ダンパーゴム、6・・・プロペラ翼。
Figure 1 is a side view of this invention. FIG. 2 is a plan view of FIG. 1, and each internal structure is shown by dotted lines. FIG. 3 is a side view of the damper rubber. In the figure, 1... shaft tube, 14... steering arm, 15... steering board, 2... center hub, 21... seesaw pin, 22... center line of center hub, 3...・・Cash, 4
... Side hub, 41... Hub axle, 42... Flapping pin, 43... Center line of hub axle, 44... Contact plate, 45... Screw, 46... Operating arm ,47...
Universal hole, 48...Drag pin, 5...
・Damper rubber, 6... Propeller blade.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 模型ヘリコプタ−のローター軸の上端に連結する軸管1
の上端に、下面に横に「コ」字形のハブ軸取付穴を設け
たセンターハブ2を、内部中央に軸管1を嵌入させ、シ
ーソーピン21で、両端の昇降を自在に連結して取付け
、軸管1のシーソ−ピン21下部の前後両側面に当金3
を固定して取付け、センタ−ハブ2両端内部に、翼取付
用の側ハブ4をセンターハブ2に連結するハブ軸41の
内端部をフラッピングピン42で上下の方向への翔動を
自在に、中心線43をセンターハブ2の中心線22より
僅かに回転方向の前側に位置させて取付け、ハブ軸41
内端の回転方向の前側に、当たり板44を取付けて、軸
管1の前後両側面に取付けた当たり金3の下面に接触さ
せ、軸管1の両側面と、ハブ軸41内端とセンターハブ
2の内面との間にダンパーゴム5を介在させ、ハブ軸4
1にプロペラ翼6取付用の側ハブ4をハブ軸41との間
にベアリング及びスラストベアリングを介在させて、揺
動自在に、ハブ軸41外端に締着するビス45で脱落を
防いで取付け、側ハブ4内端の回転方向の前側に操作腕
46を取付けて、外端をユニバーサルボール47を介し
て、ヘリコプタ−の操舵腕14と連結し、側ハブ4の先
端に、プロペラ翼6をドラッグピン48で揺動自在に取
付ける様にした、模型ヘリコプタ−のローターヘッド。
Shaft tube 1 connected to the upper end of the rotor shaft of a model helicopter
Attach the center hub 2, which has a U-shaped hub axle mounting hole on the upper end and the lower surface, by inserting the axle tube 1 into the center of the interior, and connect the vertical movement of both ends with a seesaw pin 21. , bolts 3 are placed on both front and rear sides of the lower part of the seesaw pin 21 of the shaft tube 1.
The inner end of the hub shaft 41 that connects the side hub 4 for attaching the wings to the center hub 2 is attached to the inside of both ends of the center hub 2 with a flapping pin 42 so that it can freely fly in the vertical direction. , the center line 43 of the center hub 2 is positioned slightly forward of the center line 22 of the center hub 2 in the rotational direction, and the hub axle 41
A contact plate 44 is attached to the front side of the inner end in the rotational direction, and is brought into contact with the lower surface of the contact plate 3 attached to both the front and rear sides of the shaft tube 1, and is attached to both sides of the shaft tube 1, the inner end of the hub shaft 41, and the center. A damper rubber 5 is interposed between the inner surface of the hub 2 and the hub shaft 4.
1, the side hub 4 for attaching the propeller blade 6 is attached to the hub shaft 41 with a bearing and a thrust bearing interposed between the hub 4 and the hub shaft 41 so that it can swing freely and is prevented from falling off using a screw 45 that is fastened to the outer end of the hub shaft 41. , an operating arm 46 is attached to the front side of the inner end of the side hub 4 in the rotational direction, the outer end is connected to the steering arm 14 of the helicopter via a universal ball 47, and a propeller blade 6 is attached to the tip of the side hub 4. A model helicopter rotor head that is swingably mounted with a drag pin 48.
JP4867883U 1983-03-31 1983-03-31 Model helicopter rotor head Granted JPS59154299U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4867883U JPS59154299U (en) 1983-03-31 1983-03-31 Model helicopter rotor head

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4867883U JPS59154299U (en) 1983-03-31 1983-03-31 Model helicopter rotor head

Publications (2)

Publication Number Publication Date
JPS59154299U true JPS59154299U (en) 1984-10-16
JPH0236558Y2 JPH0236558Y2 (en) 1990-10-04

Family

ID=30179201

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4867883U Granted JPS59154299U (en) 1983-03-31 1983-03-31 Model helicopter rotor head

Country Status (1)

Country Link
JP (1) JPS59154299U (en)

Also Published As

Publication number Publication date
JPH0236558Y2 (en) 1990-10-04

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