FIELD: aeronautical engineering; superlight flying vehicles. SUBSTANCE: paraplane is made over leading edge in form of flexible high-aspect ratio wing, two triangular gores being secured over trailing edge. At landing, additional gore is thrown between these triangular gores which are stowed in folded state during flight on cab top. Rings secured in corners of gores are used for embracing the lines. When additional gore is stretched, rings slide over lines and lock it in upper position. EFFECT: enhanced reliability. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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