CN112257288A
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Method for calculating resistance of axial center type centrifugal ventilator
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CN112268695A
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A gear box structure for bevel gear failure test
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CN112287459A
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Aircraft engine fuel efficiency calculation method
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CN112254971A
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Test system and method for simulating performance of ventilating bearing cavity of oil pump of aircraft engine
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CN112283470A
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Detachable pipe joint
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CN112284478A
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Auxiliary device for flow measurement
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CN112257264A
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Method for estimating clamping energy caused by failure of high-pressure turbine of aircraft engine
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CN112284324A
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Method for solving geometric throat area of turbine guide blade
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CN112211683A
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Thermal shield for turbine rear casing
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CN112253262A
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Integrated form fuel feeding bleed structure
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CN112222915A
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Engine stator part limiting structure
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CN112177685A
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Tail seam cooling structure of high-pressure turbine rotor blade
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CN112253750A
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Flexible graphite braided sealing strip and mounting method thereof
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CN112228168A
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Gas collection drainage structure for cooling inner cavity of stator blade
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CN112240244A
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Self-sealing plug structure capable of adsorbing ferromagnetic metal chips
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CN112177779A
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Lubricating oil nozzle with filtering function
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CN112231835A
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Thrust performance and deflection efficiency integrated vectoring nozzle outlet area optimization method
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CN112254172A
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Double-oil-way nozzle with heat insulation structure
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CN112254170A
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Improved sealing structure of auxiliary oil way fuel nozzle valve
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CN112254169A
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Sealing structure of secondary oil way fuel nozzle valve
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