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1. 发明授权

US11267550B2 Combined seat/stair arrangement for a multideck vehicle, in particular a multi-deck aircraft or spacecraft 有权
公开(公告)号：US11267550B2
公开(公告)日：2022-03-08
申请号：US16273245
申请日：2019-02-12
申请人： AIRBUS OPERATIONS GMBH
发明人： Eric Prenzel
IPC分类号： B64C1/24 , B64D11/06 , B64C1/18 , B64C1/00
摘要： A combined seat/stair arrangement for a multi-deck vehicle, in particular a multi-deck aircraft or spacecraft, include a foldable passenger seat; a stair which is designed to connect an upper deck to a lower deck via a stair hatch and at least one floor flap which movable between a use position of the stair with the stair hatch open and a use position of the foldable passenger seat with the stair hatch closed, wherein, in the use position of the foldable passenger seat, the at least one floor flap closes at least a partial region of the stair hatch, and wherein the floor flap is designed with a seat attachment, to which the foldable passenger seat is attached.

2. 发明授权

US11254431B2 Airstair system with deployable upper step 有权
公开(公告)号：US11254431B2
公开(公告)日：2022-02-22
申请号：US16699033
申请日：2019-11-28
申请人： BOMBARDIER INC.
发明人： John Richard Savidge , Peter Lyver , Remi Crozier , Patrick Serres
IPC分类号： B64C1/14 , B64C1/24 , B64D9/00
摘要： Airstair systems and associated methods are disclosed. In one embodiment, the airstair comprises a deployable upper step, a primary deployment device and a secondary deployment device. The upper step is movable between a stowed configuration when a door of the aircraft is closed and a deployed configuration when the door is open. The primary deployment device resiliently biases the upper step toward the deployed configuration. The secondary deployment device is movable in coordination with a movement of the door and configured to drive the deployable upper step toward the deployed configuration during opening of the door and during a failure of the primary deployment device.

3. 发明授权

US11220352B2 Unmanned aerial vehicle landing station with centering mechanism 有权
公开(公告)号：US11220352B2
公开(公告)日：2022-01-11
申请号：US17337823
申请日：2021-06-03
申请人： Easy Aerial Inc.
发明人： Ivan Stamatovski
IPC分类号： B64C1/24 , B64F1/24 , B64C39/02 , B64F1/00 , B64F1/22 , B64F1/18
摘要： A landing station for an unmanned aerial vehicle includes a landing surface and a centering wheel. The centering wheel is coupled to the landing surface and has a spoke extending therefrom. The spoke is positioned to rotate relative to the landing surface in response to rotation of the centering wheel relative to the landing surface. The spoke is configured to rotate into engagement with a landing leg of the unmanned aerial vehicle to impart centrifugal force onto the landing leg sufficient to rotate the unmanned aerial vehicle toward a predetermined position on the landing surface.

4. 发明授权

US10807693B2 Aircraft air stair support 有权
公开(公告)号：US10807693B2
公开(公告)日：2020-10-20
申请号：US16813238
申请日：2020-03-09
申请人： Gulfstream Aerospace Corporation
发明人： Michael Harp , Quent Mikeal
IPC分类号： B64C1/14 , B64C1/24 , B64D9/00 , B63B27/14
摘要： Air stair support systems, stair support cable assemblies, and hooks are disclosed herein. A stair support system includes, but is not limited to, an aircraft fuselage, a door seal, a stair door, and a stair support cable assembly. The aircraft fuselage defines a door frame and a stair hook receptacle. The stair door has a retracted position within the door frame and an extended position that forms an entry/exit stairway. The stair support cable assembly includes a cable and two hooks. The first hook includes a curved end portion configured to hook onto the stair hook receptacle, a cable end portion secured to the cable, and an intermediate portion having first and second intermediate legs that extend the intermediate portion away from the door seal when installed on the door frame and the stair door. The second hook is configured to hook on the stair door.

5. 发明申请

US20190256187A1 COMBINED SEAT/STAIR ARRANGEMENT FOR A MULTI-DECK VEHICLE, IN PARTICULAR A MULTI-DECK AIRCRAFT OR SPACECRAFT 审中-公开
公开(公告)号：US20190256187A1
公开(公告)日：2019-08-22
申请号：US16273245
申请日：2019-02-12
申请人： AIRBUS OPERATIONS GMBH
发明人： Eric PRENZEL
IPC分类号： B64C1/24 , B64C1/18 , B64D11/06
摘要： A combined seat/stair arrangement for a multi-deck vehicle, in particular a multi-deck aircraft or spacecraft, include a foldable passenger seat; a stair which is designed to connect an upper deck to a lower deck via a stair hatch and at least one floor flap which movable between a use position of the stair with the stair hatch open and a use position of the foldable passenger seat with the stair hatch closed, wherein, in the use position of the foldable passenger seat, the at least one floor flap closes at least a partial region of the stair hatch, and wherein the floor flap is designed with a seat attachment, to which the foldable passenger seat is attached.

6. 发明申请

US20180105253A1 GALLEY FOOTSTEP SYSTEMS AND METHODS 审中-公开
公开(公告)号：US20180105253A1
公开(公告)日：2018-04-19
申请号：US15297454
申请日：2016-10-19
申请人： THE BOEING COMPANY
发明人： Christopher B. Singleton , Joshua Yu-Hu Lee , Scott Edward Coburn
IPC分类号： B64C1/24 , B64D11/04
CPC分类号： B64C1/24 , B64D11/04
摘要： A compartment door of a galley within an internal cabin of a vehicle (such as an aircraft) includes a front panel having a front outer surface, and a footstep system secured to the front panel. The footstep system is moveable between a retracted position and an extended support position. The footstep system is vertically oriented in the retracted position. The footstep system outwardly extends and folds to provide a step surface in the extended support position.

7. 发明申请

US20170283030A1 ENTRY HANDLE 审中-公开
公开(公告)号：US20170283030A1
公开(公告)日：2017-10-05
申请号：US15468650
申请日：2017-03-24
申请人： Textron Aviation Inc.
发明人： James D. TERRY , Rodd William FULLER
IPC分类号： B64C1/14 , B64C1/24 , E05B1/00
CPC分类号： B64C1/1461 , B64C1/1423 , B64C1/24 , B64F1/30 , E05B1/0015 , E05B1/0053
摘要： Embodiments of the present disclosure provide an entry assist system for an aircraft doorway. The system includes a securement member configured to be secured into at least one aperture of the doorway, a handle portion pivotally attached to the securement member, and a releasable locking feature for locking the handle portion. A mounting device is used for securing the stationary member to an existing aperture in the doorway and for removing the entry assist system when no longer needed. The securement member forms a stationary portion along an inner edge of the doorway. The handle portion includes a hub configured for rotating about an axle that is coupled to an interface of the securement member. The hub and interface interconnect to form the releasable locking feature for locking the handle in a collapsed position adjacent the securement member or in an extended position protruding outside the doorway.

8. 发明申请

US20160214701A1 AIRCRAFT WITH INWARDLY FOLDABLE REAR DOOR 有权
标题翻译：具有正面可折叠后门的飞机
公开(公告)号：US20160214701A1
公开(公告)日：2016-07-28
申请号：US15005265
申请日：2016-01-25
申请人： AIRBUS HELICOPTERS DEUTSCHLAND GMBH
发明人： Stefan PROBST , Wolfgang HUENECKE , Frank LOESER , Johannes FRESE , Sebastian MORES , Michael MATT
IPC分类号： B64C1/14 , B64C1/24 , B64D11/00
CPC分类号： B64C1/1415 , B64C1/24 , B64D11/00
摘要： An aircraft comprising a rear opening and a rear door to close such rear opening, wherein the rear door is attached to the fuselage of the aircraft by means of an arrangement having two links due to which the rear door can be displaced longitudinally and in elevation up to a position at the interior of the fuselage.
摘要翻译：一种飞机，包括后开口和后门以关闭这种后开口，其中后门通过具有两个连杆的装置附接到飞机的机身上，由此可以使后门纵向移动并且向上升高到机身内部的位置。

9. 发明授权

US09221540B2 Removable step for an aircraft, and an aircraft 有权
标题翻译：一架飞机和一架飞机可以拆卸
公开(公告)号：US09221540B2
公开(公告)日：2015-12-29
申请号：US14247662
申请日：2014-04-08
申请人： AIRBUS HELICOPTERS
发明人： Richard Olive
IPC分类号： B64C1/24 , B64D9/00
CPC分类号： B64D9/00 , B64C1/24
摘要： A step (10) comprising a portable support assembly (30) having a vertical body (40) carrying a tread (31). The step includes at least two pegs (20) fastened to a fuselage (2). The body (40) includes one fastener orifice (50) per peg (20), said body (40) being carried by said pegs (20). The step includes at least one locking system (60) carried by said body (40) for automatically locking the position of at least one peg (20) in a fastener orifice (50), and manual unlocking means (86) connected to the locking system (60) for enabling the body (40) to be manually separated from the pegs (20).
摘要翻译：包括具有承载胎面（31）的垂直体（40）的便携式支撑组件（30）的台阶（10）。该步骤包括固定到机身（2）上的至少两个栓钉（20）。主体（40）包括每个钉（20）的一个紧固件孔口（50），所述主体（40）由所述栓钉（20）承载。所述步骤包括由所述主体（40）承载的至少一个锁定系统（60），用于将至少一个栓钉（20）的位置自动锁定在紧固件孔口（50）中，以及手动解锁装置（86），其连接到锁定系统（60），用于使主体（40）能够与钉（20）手动分离。

10. 发明授权

US08622337B2 Airship for transportation 有权
标题翻译：飞艇运输
公开(公告)号：US08622337B2
公开(公告)日：2014-01-07
申请号：US13052748
申请日：2011-03-21
申请人： Mohammed Hariri
发明人： Mohammed Hariri
IPC分类号： B64B1/06 , B64C1/14 , B64C1/24
CPC分类号： B64B1/06 , B64B1/22 , B64B1/30 , B64B2201/00
摘要： An airship for facilitating transportation to and from one or more locations which are difficult to access or operate such as high above the ground level is disclosed. The airship can also be used in surface missions, The airship includes a cabin and a platform. The cabin is configured on a top portion of the airship. The platform is operatively connected to the cabin. The platform facilitates easy access to the cabin.
摘要翻译：公开了一种用于便利运送到难以进入或操作的一个或多个位置的飞艇，例如高于地面高度的高度。飞艇也可以用于地面任务，飞艇包括一个客舱和一个平台。机舱配置在飞艇的顶部。平台可操作地连接到机舱。该平台便于轻松进入客舱。

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