公开(公告)号：US20210261233A1

公开(公告)日：2021-08-26

申请号：US17262122

申请日：2019-07-23

Applicant: LATECOERE

Inventor： Didier Molinari

IPC: B64C1/14 ,  E05F1/10

Abstract: An emergency opening device for an aircraft door provided with an opening mechanism including an actuating device (2, 5) for the opening mechanism, which includes a tubular operating member (2); elastic compression device (5); an activation device (31) for the actuation device (2,5); the operating member (2) includes a first end element (10) and a second end element (11) which are freely translatable movable relative to each other along the movement axis (X).

公开(公告)号：US11781356B2

公开(公告)日：2023-10-10

申请号：US17262128

申请日：2019-07-23

Applicant: LATECOERE

Inventor： Didier Molinari

IPC: E05F1/00 ,  E05F1/10 ,  B64C1/14

CPC classification number: E05F1/105 ,  B64C1/1423 ,  E05Y2201/474 ,  E05Y2201/686 ,  E05Y2800/252 ,  E05Y2900/502

Abstract: Device for opening an aircraft door in emergencies, said door being provided with an opening mechanism, including a device (2, 5) for actuating the opening mechanism, having: a tubular maneuvering member (2), and a second locking end (4) which has a stop surface (43); resilient compression device (5); a member for holding the second locking end (4), the holding member including a rotary lock (9) and a lever (44) which is suitable for cooperating with the stop surface (43), the rotary lock (9) being rotatable about the displacement axis of the maneuvering member (2); device (31) for activating the actuation device (2, 5) which are suitable for driving the rotary lock (9).

公开(公告)号：US11745845B2

公开(公告)日：2023-09-05

申请号：US17262122

申请日：2019-07-23

Applicant: LATECOERE

Inventor： Didier Molinari

IPC: E05F1/10 ,  B64C1/14

CPC classification number: B64C1/1423 ,  B64C1/1407 ,  E05F1/105 ,  E05Y2800/252 ,  E05Y2900/502

Abstract: An emergency opening device for an aircraft door provided with an opening mechanism including an actuating device (2, 5) for the opening mechanism, which includes a tubular operating member (2); elastic compression device (5); an activation device (31) for the actuation device (2,5); the operating member (2) includes a first end element (10) and a second end element (11) which are freely translatable movable relative to each other along the movement axis (X).

公开(公告)号：US20210348430A1

公开(公告)日：2021-11-11

申请号：US17262128

申请日：2019-07-23

Applicant: LATECOERE

Inventor： Didier Molinari

IPC: E05F1/10 ,  B64C1/14

Abstract: Device for opening an aircraft door in emergencies, said door being provided with an opening mechanism, including a device (2, 5) for actuating the opening mechanism, having: a tubular maneuvering member (2), and a second locking end (4) which has a stop surface (43); resilient compression device (5); a member for holding the second locking end (4), the holding member including a rotary lock (9) and a lever (44) which is suitable for cooperating with the stop surface (43), the rotary lock (9) being rotatable about the displacement axis of the maneuvering member (2); device (31) for activating the actuation device (2, 5) which are suitable for driving the rotary lock (9).