-
公开(公告)号:US12071215B2
公开(公告)日:2024-08-27
申请号:US17759655
申请日:2021-01-26
申请人: LATECOERE
发明人: Emmanuel Rouzade , Gregory Dubosc
IPC分类号: B64C1/14
CPC分类号: B64C1/1423
摘要: An aircraft door including an external opening/closing lever (7) and an internal opening/closing lever (9) which are coupled by an engaging mechanism (12) which includes: a stop (24) which entrains a counter-stop (23) when the internal opening/closing lever (9) is in its closed position and the external opening/closing lever (7) is pivoted from its closed position to its open position; a lug (22) that rotates as one with the internal opening/closing lever; an engaging pawl (15) which is spaced apart from the path of the lug (22) in a passive position, and disposed on the path of the lug (22) in an active position; a support base (16) designed to push the engaging pawl (15) back into its passive position when the external opening/closing lever (7) is in its closed position.
-
公开(公告)号:US20240150004A1
公开(公告)日:2024-05-09
申请号:US18327002
申请日:2023-05-31
申请人: The Boeing Company
CPC分类号: B64C1/1423 , B64D11/0602
摘要: A door is provided for a furniture structure of a vehicle cabin. The door includes a frame configured to expand and collapse along a longitudinal axis of the door between a collapsed position and an expanded position. The door includes a cover extending over at least a portion of the frame.
-
公开(公告)号:US20240092503A1
公开(公告)日:2024-03-21
申请号:US18273463
申请日:2022-01-21
IPC分类号: B64F1/00
CPC分类号: B64F1/005 , B64C1/1423
摘要: A removable canopy, such as for placement above an entry into a vehicle, includes a brace having releasable mounting features for mounting to the vehicle. The canopy further includes a linkage extending from the brace and convertible from a folded configuration to an extended configuration and a cross bar connected to the linkage so as to be nearer the brace when the linkage is in the folded configuration than when the linkage is in the extended configuration. A sheet is connected to the cross bar and the linkage so as to be folded when the linkage is in the folded configuration and extended when the linkage is in the extended configuration.
-
公开(公告)号:US20240026717A1
公开(公告)日:2024-01-25
申请号:US17868330
申请日:2022-07-19
CPC分类号: E05C17/14 , B64C1/1423
摘要: Disclosed is an apparatus for maintaining a position of a vehicle door relative to a vehicle frame may include a link and a fastener. The link may have a first end and a second end. The first end may have a loop and the first end may be at an opposite end of the link from the second end. The fastener may be on a surface of the link and may be configured to fasten the link to the vehicle frame. A hook may be on the second end. The loop may be an arc or an incomplete circular portion. The vehicle may be a rotorcraft vehicle.
-
公开(公告)号:US11781357B2
公开(公告)日:2023-10-10
申请号:US17262135
申请日:2019-07-23
申请人: LATECOERE
发明人: Nicolas Capron
CPC分类号: E05F1/105 , B64C1/1423 , E05Y2201/474 , E05Y2201/686 , E05Y2800/252 , E05Y2900/502
摘要: An emergency opening device for an aircraft door provided with an opening mechanism includes an actuation device (2, 5) for actuating the opening mechanism, having: a tubular operating member (2) equipped with a second locking end (4) that includes a radial retaining finger (19); flexible compression device (5); a retaining member (9) for the second locking end (4), the retaining member (9) including a hook (28) which has a stop surface, the retaining member (9) being rotatable about the movement axis of the operating member (2); activation device (31) for the actuation device (2, 5), adapted to cause the retaining member (9) to open.
-
公开(公告)号:US11745845B2
公开(公告)日:2023-09-05
申请号:US17262122
申请日:2019-07-23
申请人: LATECOERE
发明人: Didier Molinari
CPC分类号: B64C1/1423 , B64C1/1407 , E05F1/105 , E05Y2800/252 , E05Y2900/502
摘要: 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:US20230272654A1
公开(公告)日:2023-08-31
申请号:US18006600
申请日:2021-07-23
申请人: LATECOERE
CPC分类号: E05F1/08 , B64C1/1423 , E05Y2201/474 , E05Y2800/252 , E05Y2900/502 , E05Y2900/531
摘要: A device for emergency opening of an aircraft door having: a tubular actuating member (7) which includes a first end plate (8) and a second end plate (9); an elastic compression device having a tubular spring (10) compressed between the first end plate (8) and the second end plate (9); an expansion regulator (17, 18) arranged inside the tubular spring (10); a retaining member which includes at least one peripheral attachment connecting the first end plate (8) to the second end plate (9), the peripheral attachment being radially outside the tubular spring (10).
-
公开(公告)号:US11725420B2
公开(公告)日:2023-08-15
申请号:US17829802
申请日:2022-06-01
发明人: Logan Butler
CPC分类号: E05B63/0017 , B64C1/1423 , E05B63/0065 , E05B63/06 , E05C19/06 , Y10T292/06 , Y10T292/096 , Y10T292/097 , Y10T292/098 , Y10T292/0962 , Y10T292/0969 , Y10T292/0977 , Y10T292/11
摘要: A collinear latching and locking system is disclosed. In embodiments, the system includes a strike with a lock bolt disposed at or defined by an end of the strike. The system further includes a latch pawl configured to surround at least a portion of the strike. The strike and the latch pawl are configured to actuate linearly along the same axis. In this regard, the strike and the latch pawl have a collinear configuration and actuation path. The system further includes a latch cam configured to actuate the latch pawl from a latched position to an unlatched position when the latch cam is turned.
-
公开(公告)号:US11697500B2
公开(公告)日:2023-07-11
申请号:US16726765
申请日:2019-12-24
CPC分类号: B64D11/00 , B64C1/10 , B64C1/1423 , B64C1/22 , B64C39/00 , B64C39/10 , B64D25/14 , B64C2039/105
摘要: Technologies for providing emergency egress routes for a blended wing body aircraft are described herein. In some examples, the emergency egress routes are through a side cabin bulkhead and aft one or more cargo holds. In some examples, the blended wing body aircraft has wings that are high geometry wings. In these examples, the emergency egress routes do not penetrate an aft spar, reducing weight and increasing the integrity of the aircraft.
-
公开(公告)号:US11643200B2
公开(公告)日:2023-05-09
申请号:US17014702
申请日:2020-09-08
发明人: Keun Seok Lee , Hyun Woo Jun , Se Hwan Park , Jae Hyung Kim
CPC分类号: B64C29/0033 , B64C1/1423 , B64C29/0025 , B64D9/00
摘要: An air mobility craft is provided. The air mobility craft includes a fuselage that has a boarding space and a boarding gate and a plurality of wings disposed on the fuselage. A plurality of rotors are disposed on the wings. A first number of the plurality of rotors are tilting rotors configured to tilt upward or downward for lifting or cruising of the fuselage and a remaining number of the rotors are lifting rotors.
-
-
-
-
-
-
-
-
-