JPS61196899U - - Google Patents

Info

Publication number
JPS61196899U
JPS61196899U JP8168485U JP8168485U JPS61196899U JP S61196899 U JPS61196899 U JP S61196899U JP 8168485 U JP8168485 U JP 8168485U JP 8168485 U JP8168485 U JP 8168485U JP S61196899 U JPS61196899 U JP S61196899U
Authority
JP
Japan
Prior art keywords
axis
folded
elevators
wing
span
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
JP8168485U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP8168485U priority Critical patent/JPS61196899U/ja
Publication of JPS61196899U publication Critical patent/JPS61196899U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Cage And Drive Apparatuses For Elevators (AREA)
  • Types And Forms Of Lifts (AREA)

Description

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

第1図……機体組立時の斜視図、第2図……折
り畳み完了時の斜視図、第3図……組立時の主翼
折り畳み部分正面断面図、第4〜7図……折り畳
み各段階の正面断面図。 1……胴体一部、2……中央桁突出部、3……
主翼桁、6……ガイドシヤフト、7……屈折部、
8……屈折部枢軸。
Figure 1: Perspective view when the fuselage is assembled, Figure 2: Perspective view when folding is complete, Figure 3: Front sectional view of the main wing folded part during assembly, Figures 4 to 7: Each stage of folding Front sectional view. 1...Part of the fuselage, 2...Central spar protrusion, 3...
Main wing spar, 6... Guide shaft, 7... Bent part,
8... Refraction axis.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 主翼を折り畳み得る超軽量飛行機に於て、昇降
舵を折り畳む構造を有し、片翼毎に、翼をスパン
(X軸)方向に一定量引き抜き、X軸廻りに回転
して翼弦を略垂直(Y軸)となし、X軸線上に設
けたる関節部より後方に向つて略機軸(Z軸)に
平行位置まで回転し得ることを特長とする折り畳
み構造。
Ultra-light airplanes with foldable main wings have a structure in which the elevators are folded, and each wing is pulled out a certain amount in the span (X-axis) direction and rotated around the X-axis to raise the chord approximately vertically. (Y-axis), and is capable of rotating rearward from a joint provided on the X-axis to a position substantially parallel to the machine axis (Z-axis).
JP8168485U 1985-05-30 1985-05-30 Pending JPS61196899U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8168485U JPS61196899U (en) 1985-05-30 1985-05-30

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8168485U JPS61196899U (en) 1985-05-30 1985-05-30

Publications (1)

Publication Number Publication Date
JPS61196899U true JPS61196899U (en) 1986-12-08

Family

ID=30628696

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8168485U Pending JPS61196899U (en) 1985-05-30 1985-05-30

Country Status (1)

Country Link
JP (1) JPS61196899U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021079844A (en) * 2019-11-20 2021-05-27 株式会社Subaru Air-ground use movable body
DE112020005430T5 (en) 2019-11-06 2022-08-25 Subaru Corporation ROAD-READY AIRCRAFT

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE112020005430T5 (en) 2019-11-06 2022-08-25 Subaru Corporation ROAD-READY AIRCRAFT
US11958600B2 (en) 2019-11-06 2024-04-16 Subaru Corporation Roadable aircraft
JP2021079844A (en) * 2019-11-20 2021-05-27 株式会社Subaru Air-ground use movable body

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KEIDEL et al. The Horizon: A blended wing aircraft configuration design project, volume 3(Final Report, 1987- 1988)