| 摘要 |
FIELD: transport. ^ SUBSTANCE: invention relates to aircraft or spaceship tail design. Proposed tail comprises load-bearing structure to support aircraft or airship assembly unit, and dividing wall assembly unit to seal fuselage compartment that may be jointed with said structure and fuselage compartment. Said load-bearing structure comprises two pylons to form force flow path to support relevant engine. Said pylons represent parallelepiped structure made up of support beams. One support beam is arranged in said parallelepiped along its diagonal. ^ EFFECT: improved aerodynamics. ^ 6 cl, 7 dwg |
