FIELD: aviation; manufacture of superlight aeroplanes. SUBSTANCE: microaircraft includes low-aspect-ratio wing whose center section is formed by two side beams . Fin with rudder and all-moving stabilizer secured on front portion of beams, platform between them being used for pilot. Engine with propeller is mounted on frame on longitudinal beams in circular channel. EFFECT: enhanced reliability. 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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| LIGHT AIRCRAFT | 1993 |
|
RU2095285C1 |
| POWER HANG GLIDER | 1998 |
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|
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|
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| MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
|
RU2207968C2 |
| UNMANNED AERIAL VEHICLE OF VERTICAL TAKE-OFF AND LANDING AND METHOD OF MANUFACTURING THEREOF | 2023 |
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RU2819460C1 |
Authors
Dates
1997-11-10—Published
1993-05-05—Filed