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
Links
Landscapes
- Cage And Drive Apparatuses For Elevators (AREA)
- Types And Forms Of Lifts (AREA)
Description
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)
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).
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)
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 |
-
1985
- 1985-05-30 JP JP8168485U patent/JPS61196899U/ja active Pending
Cited By (3)
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) |