Airframe for a highly maneuvrable multi-mode aircraft
The invention relates to heavier-than-air aircraft and is intended for use primarily in highly maneuverable multi-mode aircraft operating at both subsonic and supersonic speeds. The aim of the invention is to provide the necessary durability and rigidity of the frame of the airframe with only a negl...
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| creator | LAPSHIN MIHAIL EVGENYEVICH STRELETS MIHAIL YURIEVICH DAVIDENKO ALEKSANDR NIKOLAEVICH BLINOV ALEKSANDR IVANOVICH KOGAN YURIY ARONOVICH RUNISHEV VLADIMIR ALEKSANDROVICH |
| description | The invention relates to heavier-than-air aircraft and is intended for use primarily in highly maneuverable multi-mode aircraft operating at both subsonic and supersonic speeds. The aim of the invention is to provide the necessary durability and rigidity of the frame of the airframe with only a negligible increase in the mass thereof and the inclusion of large cutouts in the lower part of the fuselage for cargo compartments. At the same time, the technical result of redistributing the stresses in the load-bearing members of the aircraft airframe which are caused by external loads is achieved as a result of the judicious arrangement of the load-bearing members of the frame of the airframe. The structural layout of the fuselage includes transverse and longitudinal load-bearing members in the form of fuselage bulkheads (17-25) and longitudinal walls (26-29), respectively.; A set of longitudinal walls (26-29) passes through the entire middle part (3) and rear part (5) of the fuselage. The centre section (12) is a |
| format | Patent |
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The aim of the invention is to provide the necessary durability and rigidity of the frame of the airframe with only a negligible increase in the mass thereof and the inclusion of large cutouts in the lower part of the fuselage for cargo compartments. At the same time, the technical result of redistributing the stresses in the load-bearing members of the aircraft airframe which are caused by external loads is achieved as a result of the judicious arrangement of the load-bearing members of the frame of the airframe. The structural layout of the fuselage includes transverse and longitudinal load-bearing members in the form of fuselage bulkheads (17-25) and longitudinal walls (26-29), respectively.; A set of longitudinal walls (26-29) passes through the entire middle part (3) and rear part (5) of the fuselage. 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| language | chi ; eng |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | Airframe for a highly maneuvrable multi-mode aircraft |
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