FIELD: aeronautical engineering. SUBSTANCE: landing gear includes leg with breaker strut, wheeled truck with shock absorber which is articulated with leg by means of lever. Landing gear is provided with truck turning mechanism which consists of hinged bell cranks and rods. Double-arm bell crank is articulated on leg and its one arm is connected with rod and other end is connected with bell crank by means of rod. EFFECT: enhanced reliability. 2 cl, 7 dwg
| Title | Year | Author | Number |
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SU593400A1 |
| 0 |
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SU544363A3 | |
| AIRCRAFT TWO-SEAT CABIN CANOPY JETTISON SYSTEM | 1997 |
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RU2130857C1 |
