JPS595996U - model airplane structure - Google Patents

model airplane structure

Info

Publication number
JPS595996U
JPS595996U JP10204082U JP10204082U JPS595996U JP S595996 U JPS595996 U JP S595996U JP 10204082 U JP10204082 U JP 10204082U JP 10204082 U JP10204082 U JP 10204082U JP S595996 U JPS595996 U JP S595996U
Authority
JP
Japan
Prior art keywords
model airplane
stabilizer
wing
airplane structure
chord length
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
JP10204082U
Other languages
Japanese (ja)
Other versions
JPS6125840Y2 (en
Inventor
二宮　康明
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 JP10204082U priority Critical patent/JPS595996U/en
Publication of JPS595996U publication Critical patent/JPS595996U/en
Application granted granted Critical
Publication of JPS6125840Y2 publication Critical patent/JPS6125840Y2/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]

第１図は従来例模型飛行機を示す図。第２図は第１図の
模型飛行機の尾翼部分の正面図。第３図は第２図を等価
振動系で表した図。第４図は本考案に係る模型飛行機の
実施例を示す図。第５図、第６図、第７図は本考案に係
る模型飛行機の他の実施例を示す図。第８図は参考例の
模型飛行機を示す図。 １１・・・水平尾翼、１２・・・垂直尾翼、１４・・・
胴体、Ｌ１□・・・水平尾翼の翼弦長、Ｌ□２・・・垂
直尾翼の翼弦長。FIG. 1 is a diagram showing a conventional model airplane. Figure 2 is a front view of the tail section of the model airplane shown in Figure 1. Figure 3 is a diagram representing Figure 2 as an equivalent vibration system. FIG. 4 is a diagram showing an embodiment of a model airplane according to the present invention. FIG. 5, FIG. 6, and FIG. 7 are views showing other embodiments of the model airplane according to the present invention. FIG. 8 is a diagram showing a model airplane as a reference example. 11...Horizontal stabilizer, 12...Vertical stabilizer, 14...
Fuselage, L1□...Horizontal tail wing chord length, L□2...Vertical tail wing chord length.

Claims (1)

【実用新案登録請求の範囲】 少なくとも翼部分の材料が紙またはプラスチックシート
のいずれかであり、主翼または水平尾翼のいずれかの先
端部に垂直尾翼が接着された横木の模型飛行機において
、 上記垂直尾翼が取り付けられた上記主翼または上記水平
尾翼の先端接合部の翼弦長が上記垂直尾翼の翼弦長より
も大きいことを特徴とする模型飛行機の構造。[Claims for Utility Model Registration] In a cross-piece model airplane in which the material of at least the wing portion is either paper or plastic sheet, and the vertical stabilizer is glued to the tip of either the main wing or the horizontal stabilizer, the above-mentioned vertical stabilizer A structure of a model airplane, characterized in that a chord length of a tip joint portion of the main wing or the horizontal stabilizer to which the wing is attached is greater than the chord length of the vertical stabilizer.
JP10204082U 1982-07-05 1982-07-05 model airplane structure Granted JPS595996U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10204082U JPS595996U (en) 1982-07-05 1982-07-05 model airplane structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10204082U JPS595996U (en) 1982-07-05 1982-07-05 model airplane structure

Publications (2)

Publication Number Publication Date
JPS595996U true JPS595996U (en) 1984-01-14
JPS6125840Y2 JPS6125840Y2 (en) 1986-08-04

Family

ID=30240702

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10204082U Granted JPS595996U (en) 1982-07-05 1982-07-05 model airplane structure

Country Status (1)

Country Link
JP (1) JPS595996U (en)

Also Published As

Publication number Publication date
JPS6125840Y2 (en) 1986-08-04

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