公开(公告)号：US20170247100A1

公开(公告)日：2017-08-31

申请号：US15441510

申请日：2017-02-24

Applicant: Airbus Operations SAS

Inventor： Olivier Cazals ,  Jaime GENTY DE LA SAGNE

IPC: B64C1/14 ,  B64C1/24 ,  B64D27/14 ,  B64C39/10

CPC classification number: B64C1/1423 ,  B64C1/143 ,  B64C1/24 ,  B64C39/10 ,  B64C2039/105 ,  B64D27/14 ,  Y02T50/12

Abstract: 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.

公开(公告)号：US20160368594A1

公开(公告)日：2016-12-22

申请号：US15182709

申请日：2016-06-15

Applicant: Airbus Operations (SAS)

Inventor： Olivier Cazals ,  Thierry Druot

IPC: B64C23/06 ,  B64C5/10 ,  B64C3/38

CPC classification number: B64C23/072 ,  B64C3/38 ,  B64C3/385 ,  B64C3/42 ,  B64C5/10 ,  Y02T50/164

Abstract: An aircraft wing, including a main part and a wing tip mounted mobile in attack relative to the main part.

Abstract translation: 一架飞机机翼，包括一个主要部分和一个机翼尖端，相对于主要部分移动攻击。

公开(公告)号：US10329010B2

公开(公告)日：2019-06-25

申请号：US15182709

申请日：2016-06-15

Applicant: Airbus Operations (SAS)

Inventor： Olivier Cazals ,  Thierry Druot

IPC: B64C3/42 ,  B64C3/38 ,  B64C5/10 ,  B64C23/06

Abstract: An aircraft wing, including a main part and a wing tip mounted mobile in attack relative to the main part.

公开(公告)号：US20170183077A1

公开(公告)日：2017-06-29

申请号：US15385379

申请日：2016-12-20

Applicant: Airbus Operations SAS

Inventor： Olivier Cazals ,  Jaime GENTY DE LA SAGNE

IPC: B64C1/14 ,  B64C39/10 ,  B64C1/22

Abstract: 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.

公开(公告)号：US20160176533A1

公开(公告)日：2016-06-23

申请号：US14974660

申请日：2015-12-18

Applicant: Airbus Operations SAS

Inventor： Olivier Cazals ,  Thierry Druot ,  Julien Guillemaut

IPC: B64D27/24 ,  B64D41/00 ,  B64D29/02 ,  B64C3/32 ,  B64C11/00

CPC classification number: B64D27/24 ,  B64C3/32 ,  B64C11/00 ,  B64C11/001 ,  B64D7/00 ,  B64D27/26 ,  B64D29/02 ,  B64D41/00 ,  B64D2041/002 ,  Y02T50/62

Abstract: An auxiliary power device may be exteriorly removably connected to an aircraft in order to allow the increase of the performance data of the aircraft, namely at take-off and landing. The auxiliary power device includes a propeller (or fan) connected to an electric engine fed by an electric power supply.

Abstract translation: 辅助动力装置可以在外部可拆卸地连接到飞行器，以允许增加飞行器的性能数据，即起飞和降落。 辅助动力装置包括连接到由电力供给的电动发动机的螺旋桨（或风扇）。

公开(公告)号：US10597135B2

公开(公告)日：2020-03-24

申请号：US15385379

申请日：2016-12-20

Applicant: Airbus Operations SAS

Inventor： Olivier Cazals ,  Jaime Genty De La Sagne

IPC: B64C1/14 ,  B64C1/22 ,  B64C39/10 ,  B64C1/00

Abstract: 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.

公开(公告)号：US10407151B2

公开(公告)日：2019-09-10

申请号：US15441510

申请日：2017-02-24

Applicant: Airbus Operations SAS

Inventor： Olivier Cazals ,  Jaime Genty De La Sagne

IPC: B64C1/14 ,  B64C39/10 ,  B64C1/24 ,  B64D27/14

Abstract: 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 located on a wall other than 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.

公开(公告)号：US20170167437A1

公开(公告)日：2017-06-15

申请号：US15378739

申请日：2016-12-14

Applicant: Airbus Operations SAS

Inventor： Olivier Cazals ,  Julien GUILLEMAUT

IPC: F02K1/52 ,  F02K1/56

CPC classification number: F02K1/52 ,  B64D27/14 ,  B64D27/20 ,  F02C6/20 ,  F02K1/566 ,  F02K3/06 ,  F05D2220/323 ,  F05D2250/314 ,  Y02T50/44 ,  Y02T50/671

Abstract: A jet engine comprises at least three zones including an air intake zone and an exhaust zone. The axis of the air intake zone is not coincident with the axis of the exhaust zone of the engine, the engine as a result, having at least two intersecting axes and being referred to as a multiaxial engine. Therefore, the jet engine has at least two zones with different longitudinal axis orientations: by choosing an axial orientation of the zones of the engine that are more sensitive to a detachment or breakage of elements of the gas generator, it is possible to also choose a direction of the possible paths of these detached elements, to avoid them striking the opposite engine.