An aircraft nacelle 110 which comprises a structure 302, an upstream cowl 110a, an upper cowl 200 arranged to the rear of the upstream cowl 110a and having a starboard-side door 200a and a port-side door 200b, each being articulated between a closed position and an open position, each having a front edge (202a-b), a rear edge(204a-b), an inner edge (208a-b) and an outer edge(206a-b). The nacelle comprises, for each door (200a-b), an articulation (300) and a locking system (320). Each door (200a-b) is articulated at the level of its outer edge (206a-b) and, in the closed position, the inner edge (208a-b) of one door (200a-b) is contiguous with the inner edge (208b-a) of the other door (200b-a). Such a nacelle makes the technicians' work easier because the two articulated doors can be openedwide and give easy access under the cowl.
一种飞行器短舱(110),所述短舱包括结构体(302)、上游整流罩(110a)、上整流罩(200),所述上整流罩布置在所述上游整流罩(110a)的后部并且具有右舷侧门(200a)和左舷侧门(200b),每个门铰接在关闭位置与打开位置之间,每个门具有前部边缘(202a‑b)、后部边缘(204a‑b)、内边缘(208a‑b)和外边缘(206a‑b)。所述短舱包括每个门(200a‑b)的铰接部(300)和锁定系统(320)。每个门(200a‑b)在其外边缘(206a‑b)的水平高度处铰接,并且在所述关闭位置,一个门(200a‑b)的内边缘(208a‑b)与另一个门(200b‑a)的内边缘(208b‑a)毗连。因为这两个铰接门可以宽敞地打开并且使得易于触及所述整流罩下方,所以这种短舱使技术人员的工作更加容易。
Aircraft nacelle comprising a cover with two hinged flaps
包括具有两个铰接门的整流罩的飞行器短舱
2020-05-29
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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