Design method of wing fuel tank structure and wing
The invention belongs to the technical field of aircraft wing fuel tank structures, and discloses a design method of a wing fuel tank structure and a wing, the design method comprises the following steps: firstly obtaining a sweeping path of blasting fragments of a rotor of an engine, and obtaining...
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| creator | FANG YANING QIU HECHEN CHEN MENG FAN WEICHAO SUN QIAN |
| description | The invention belongs to the technical field of aircraft wing fuel tank structures, and discloses a design method of a wing fuel tank structure and a wing, the design method comprises the following steps: firstly obtaining a sweeping path of blasting fragments of a rotor of an engine, and obtaining an arrangement position of a main load-bearing structure of the wing; the position relation of sweeping paths of blasting fragments of an inner side interface rib plate, a middle interface rib plate and an outer side interface rib plate relative to a rotor of the engine is determined, the inner side interface rib plate, the middle interface rib plate and the outer side interface rib plate are wing ribs in a main force bearing structure of a wing, and the positions and the number of fuel tank partition plates are determined; and then the inner side interface rib plate, the oil tank partition plate, the middle interface rib plate and the outer side interface rib plate are connected to form a stepped interface partiti |
| format | Patent |
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the position relation of sweeping paths of blasting fragments of an inner side interface rib plate, a middle interface rib plate and an outer side interface rib plate relative to a rotor of the engine is determined, the inner side interface rib plate, the middle interface rib plate and the outer side interface rib plate are wing ribs in a main force bearing structure of a wing, and the positions and the number of fuel tank partition plates are determined; and then the inner side interface rib plate, the oil tank partition plate, the middle interface rib plate and the outer side interface rib plate are connected to form a stepped interface partiti</description><language>chi ; eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; 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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | Design method of wing fuel tank structure and wing |
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