| 摘要 |
FIELD: aviation. ^ SUBSTANCE: proposed aircraft has fuselage with cabin located in its center, cantilever wing, horizontal and vertical tails, tricycle retractable landing gear with nose undercarriage and opposite or radial piston engine secured on engine mount and covered with cowling. Aircraft is provided with motor and cowling connected with fuselage frame over skew joint whose lower part is located in front of nose undercarriage and upper part is located in front of cabin canopy. ^ EFFECT: extended range of engines. ^ 2 dwg |
