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ENGINE INTAKE SHUTTER TO BE MOUNTED AT AIRCRAFT ENGINE AIR INTAKE AND AIRCRAFT ENGINE WITH SUCH INTAKE SHUTTER AND AIRCRAFT SYSTEM
ENGINE INTAKE SHUTTER TO BE MOUNTED AT AIRCRAFT ENGINE AIR INTAKE AND AIRCRAFT ENGINE WITH SUCH INTAKE SHUTTER AND AIRCRAFT SYSTEM
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机译:带有这种进气门和飞机系统的发动机进气门将安装在飞机进气口和飞机发动机上
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摘要
FIELD: transport.;SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft engine air intake shutter. Intake shutter K has first end E1 and second end E2 arranged spaced therefrom and opposite thereto and along its lengthwise axis L. Note here that lengthwise axis L in this configuration is directed across direction D of air flow fed to the engine. Sutter K has main case 1 with hinged to connect main case 1 to air intake case or air intake duct extending along second end E2 with hinge pin A, elongated part 2 of said shutter integrated in main case 1 and has and second side part 5, 6. Side parts 5, 6 extend from main case 1 to two side edges 1a, 1b of the shutter K and to oppose each other in lengthwise direction L, and multiple transverse rods 11 or lengthwise rods.;EFFECT: optimised inlet airflow, prevented air intake icing.;15 cl, 5 dwg
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