JPS6034895U - Flight direction control device for electric model helicopters - Google Patents

Flight direction control device for electric model helicopters

Info

Publication number
JPS6034895U
JPS6034895U JP12870183U JP12870183U JPS6034895U JP S6034895 U JPS6034895 U JP S6034895U JP 12870183 U JP12870183 U JP 12870183U JP 12870183 U JP12870183 U JP 12870183U JP S6034895 U JPS6034895 U JP S6034895U
Authority
JP
Japan
Prior art keywords
control device
direction control
flight direction
electric model
model helicopters
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
JP12870183U
Other languages
Japanese (ja)
Other versions
JPS6327758Y2 (en
Inventor
川合　迪夫
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 JP12870183U priority Critical patent/JPS6034895U/en
Publication of JPS6034895U publication Critical patent/JPS6034895U/en
Application granted granted Critical
Publication of JPS6327758Y2 publication Critical patent/JPS6327758Y2/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) [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 the drawing]

図面は本考案の一実施例を示しており、第１図は要部の
縦断面図、第２図Ａは前後スライド板を示す平面図、第
２図Ｂは作動状態を示す正面図、第３図Ａは横スライド
板を示す平面図、第３図Ｂは作動状態を示す正面図であ
る。 ７・・・機体、１２・・・前後方向ガイド杆、１３・・
・前後スライド板、１４・・・第１サーボ、１６・・・
横方向ガイド杆、１７・・・横スライド板、１８・・・
第２サーボ、２０・・・吊り下げ杆、２１・・・バッテ
リー、２２・・・重錘。 第２図 第３図The drawings show one embodiment of the present invention; FIG. 1 is a vertical sectional view of the main parts, FIG. 2A is a plan view showing the front and rear slide plates, FIG. 2B is a front view showing the operating state, and FIG. 3A is a plan view showing the horizontal slide plate, and FIG. 3B is a front view showing the operating state. 7... Airframe, 12... Fore-and-aft direction guide rod, 13...
・Front and rear slide plate, 14...1st servo, 16...
Lateral guide rod, 17... Lateral slide plate, 18...
2nd servo, 20... hanging rod, 21... battery, 22... weight. Figure 2 Figure 3

Claims (2)

【実用新案登録請求の範囲】[Scope of utility model registration request] （１）模型ヘリコプタ−の機体重心下部に第１サーボに
連結する前後スライド板と、第２サーボに連結する横ス
ライド板を十字状に重ね、該重ね状態で４箇所できる角
部上方の機体位置に上端を揺動自在に連結して４本の吊
り下げ杆を設け、該各吊り下げ杆下端に重錘を吊設する
ことを特徴とする模型ヘリコプタ−における飛行方向制
御装置。(1) The front and rear slide plates connected to the first servo and the horizontal slide plates connected to the second servo are stacked in a cross shape below the center of gravity of the model helicopter, and the fuselage position is located above the corner, which is created in four places in this stacked state. 1. A flight direction control device for a model helicopter, characterized in that four hanging rods are provided, the upper ends of which are swingably connected to each other, and a weight is suspended from the lower end of each of the hanging rods. （２）前記重錘がバッテリーであることを特徴とする実
用新案登録請求の範囲第１項記載の模型ヘリコプタ−に
おける飛行方向制御装置。(2) A flight direction control device for a model helicopter according to claim 1, wherein the weight is a battery.
JP12870183U 1983-08-19 1983-08-19 Flight direction control device for electric model helicopters Granted JPS6034895U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12870183U JPS6034895U (en) 1983-08-19 1983-08-19 Flight direction control device for electric model helicopters

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12870183U JPS6034895U (en) 1983-08-19 1983-08-19 Flight direction control device for electric model helicopters

Publications (2)

Publication Number Publication Date
JPS6034895U true JPS6034895U (en) 1985-03-09
JPS6327758Y2 JPS6327758Y2 (en) 1988-07-27

Family

ID=30291871

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12870183U Granted JPS6034895U (en) 1983-08-19 1983-08-19 Flight direction control device for electric model helicopters

Country Status (1)

Country Link
JP (1) JPS6034895U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02106496A (en) * 1988-10-15 1990-04-18 Yamaha Motor Co Ltd Remote control type helicopter
JP2002277351A (en) * 2001-03-19 2002-09-25 Kawasaki Heavy Ind Ltd Mechanism for moving center of gravity for unmanned operation vehicle
JP2006051892A (en) * 2004-08-12 2006-02-23 Seiko Epson Corp Small flight vehicle
JP2009137319A (en) * 2007-12-03 2009-06-25 Engineering System Kk Fixed pitch type coaxial double contra-rotating helicopter
JP2010088518A (en) * 2008-10-03 2010-04-22 Ccp:Kk Center of gravity adjustment apparatus

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54133936A (en) * 1978-04-07 1979-10-18 Tetsuya Kurohara Control system for model plane with rotary wings

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54133936A (en) * 1978-04-07 1979-10-18 Tetsuya Kurohara Control system for model plane with rotary wings

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02106496A (en) * 1988-10-15 1990-04-18 Yamaha Motor Co Ltd Remote control type helicopter
JP2002277351A (en) * 2001-03-19 2002-09-25 Kawasaki Heavy Ind Ltd Mechanism for moving center of gravity for unmanned operation vehicle
JP2006051892A (en) * 2004-08-12 2006-02-23 Seiko Epson Corp Small flight vehicle
JP2009137319A (en) * 2007-12-03 2009-06-25 Engineering System Kk Fixed pitch type coaxial double contra-rotating helicopter
JP2010088518A (en) * 2008-10-03 2010-04-22 Ccp:Kk Center of gravity adjustment apparatus

Also Published As

Publication number Publication date
JPS6327758Y2 (en) 1988-07-27

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