Embedded type air inlet channel with stealth function

The invention belongs to the technical field of aviation aircraft design, and discloses an embedded air inlet channel with a stealth function, which comprises a forward flow guide port, side edges, side edge inclined plates, a rear lip and rear lip side plates, the front end of the forward flow guid...

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Bibliographische Detailangaben
Hauptverfasser: FAN LI, YU CONG, REN ZHIWEN, WANG TIANSUI, QU DONGPING, ZHAO SHENG, ZHOU JUNWEI, YANG JIABI, LU JIE, WAN ZHIMING, WEN GE, CHO JUNG-HYUNG, CHEN ZUNJING, XIAO YI, WAN LIYING, WANG CHUNLI, AN PING, GAO JUNDONG, WAN JUNDAN
Format: Patent
Sprache:chi ; eng
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Zusammenfassung:The invention belongs to the technical field of aviation aircraft design, and discloses an embedded air inlet channel with a stealth function, which comprises a forward flow guide port, side edges, side edge inclined plates, a rear lip and rear lip side plates, the front end of the forward flow guide port is in direct smooth rounding connection with the surface of an aircraft, the side edges are arranged on the two sides of the forward flow guide port, and the rear lip side plates are arranged on the side edges. The side edge extends backwards to be smoothly connected with the rear lip; wherein the side edge and the rear lip are both lower than the surface of the aircraft, the side edge is in transition connection with the surface of the aircraft through a side edge inclined plate, and the rear lip is in transition connection with the surface of the aircraft through a rear lip side plate. According to the invention, the side edge and the rear lip both adopt an unconventional curvature continuous fairing desig