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公开(公告)号：US20170183077A1
公开(公告)日：2017-06-29
申请号：US15385379
申请日：2016-12-20
摘要： In order to simplify the connection of a door to the outer envelope of an aircraft cell, it is provided to dispose the door into a portion of the outer envelope having tilted sides, as is the case at the nose cones and the tail cones of conventional airplanes, and in various portions of blended wing body airplanes and flying wings. Thus, the door can be configured to displace, in rectilinear translation, from one of its extreme opening and closing positions to the other, without requiring that the door protrudes outside of the outer envelope in the closing position.
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2.发明申请公开(公告)号：US20180009532A1
公开(公告)日：2018-01-11
申请号：US15643793
申请日：2017-07-07
CPC分类号： B64D11/0602 , B64D11/0689 , B64D43/00 , B64D2011/0046 , Y02T50/46
摘要： An aircraft cockpit module (10) that incorporates, on the one hand, a single pilot seat (12) and, on the other hand, at least a part of the piloting equipment and controls necessary for flying an aircraft, the module (10). The aircraft cockpit module forms an assembly which can be moved unitarily and to be incorporated in a single operation in an aircraft cockpit. The module is dedicated to a single pilot and makes it possible to simplify the integration of the cockpit.
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3.发明申请公开(公告)号：US20170247100A1
公开(公告)日：2017-08-31
申请号：US15441510
申请日：2017-02-24
CPC分类号： B64C1/1423 , B64C1/143 , B64C1/24 , B64C39/10 , B64C2039/105 , B64D27/14 , Y02T50/12
摘要： An aircraft of flying wing or blended wing body type comprising, for access to a pressurized housing, a non-pressurized door in the trailing edge of the aircraft and a pressurized door on the pressurized housing. The distance between the center of the pressurized door and a plane of symmetry of the aircraft is less than or equal to the distance between the center of the non-pressurized door and the plane of symmetry, and the pressurized door is outside a rear wall of the pressurized housing or upstream of a rear extremum point of the housing in the absence of any such rear wall. This aircraft has optimum aerodynamic performance and the circulation of passengers between the pressurized housing and the exterior of the aircraft may be fluid.
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