AIRCRAFT AIR INTAKE
申请(专利)号: RU2024119428
专利号: RU2714555C1 主分类号: B64D33/02 申请权利人: FEDERALNOE
GOSUDARSTVENNOE UNITARNOE PREDPRIYATIE \AEROGIDRODINAMICHESKIJ
INSTITUT IMENI PROFESSORA N.E.
ZHUKOVSKOGO\(FGUP \公开国代码: RU 优先权国家: RU
摘 要:
FIELD: engine building.;SUBSTANCE: invention relates to air intakes of aircraft engines. Air intake of airplane comprises curvilinear air channel (1). Plate (5) is installed along width of channel (1) along its central line, at least in point of bend of channel (1). Plate (5) is installed along length of channel (1) in range from 0.25 L to 1 L, where L is length of channel (1), with shift relative to central line of channel (1) at distance ±0.15 of diameter D of inlet (4) into engine. Plate (5) is made using sound-absorbing material, has constant thickness of main part and smoothed (rounded) profiles of front and / or rear ends.;EFFECT: invention improves
aerodynamic characteristics of air intake
申请日: %Y-%m-%d 公开公告日: %Y-%m-%d
分类号: B64D33/02
发明设计人: ANISIMOV KIRILL
SERGEEVICH (RU); LYSENKOV ALEKSANDR
VALEREVICH (RU)
申请国代码: RU
优先权: 20240621 RU
2024119428
摘 要 附 图:
of aircraft due to reduction of losses of full pressure at input to engine in range of working flows through engine.;6 cl, 1 dwg 主权项:
1. Воздухозаборник самолета, включающий криволинейный воздушный канал, отличающийся тем, что по шири
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