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    • 3. 发明申请
    • PASSENGER SEAT WITH WIRE-FRAME SUPPORT
    • 乘客座椅带有线框支持
    • WO2012064924A1
    • 2012-05-18
    • PCT/US2011/060112
    • 2011-11-10
    • WEBER AIRCRAFT LLCAGUIRRE, Raul, Daniel FloresSALAZAR, Jesus Eduardo Rosales
    • AGUIRRE, Raul, Daniel FloresSALAZAR, Jesus Eduardo Rosales
    • B64D11/06
    • B64D11/06B64D11/062B64D11/064B64D11/0647B64D11/0649Y10T29/49826
    • Described are passenger seats (100) comprising a seat body (102); at least one wire- frame support (104) comprising a base (116) coupled to the seat body and at least one wire- frame member (118) pivotally coupled to the base; and at least one seat cover (106) coupled to the seat body, wherein the at least one wire- frame support is at least partially enclosed between the at least one seat cover and the seat body. The at least one seat cover may be formed of an elastic fiber or plastic. The at least one wire- frame support may be positioned on the seat body in a location configured to provide support for a passenger's neck or lumbar area. Also described are passenger seats comprising a seat body; at least one wire- frame sub-assembly (124); and at least one seat cover coupled to the seat body, wherein the at least one wire- frame sub-assembly is at least partially enclosed between the at least one seat cover and the seat body.
    • 描述了包括座椅主体(102)的乘客座位(100)。 至少一个线框架支撑件(104)包括联接到所述座椅本体的基部(116)和枢转地联接到所述基座的至少一个线框构件(118) 以及联接到所述座椅主体的至少一个座椅盖(106),其中所述至少一个线框架支撑件至少部分地封闭在所述至少一个座椅盖和所述座椅主体之间。 所述至少一个座盖可由弹性纤维或塑料形成。 至少一个线框架支撑件可以被定位在座椅本体上,该位​​置被配置成为乘客的颈部或腰部区域提供支撑。 还描述了包括座椅主体的乘客座椅; 至少一个线框子组件(124); 以及联接到所述座椅主体的至少一个座盖,其中所述至少一个线框子组件至少部分地封闭在所述至少一个座椅盖和所述座椅本体之间。
    • 6. 发明申请
    • PASSENGER SEAT ASSEMBLY
    • 乘客座椅组装
    • WO2011068828A2
    • 2011-06-09
    • PCT/US2010058495
    • 2010-12-01
    • WEBER AIRCRAFT LLCWESTERINK RIKWEGENKA JEFF
    • WESTERINK RIKWEGENKA JEFF
    • B64D11/06
    • B64D11/064B64D11/06
    • Embodiments of the present invention include a seat back pivotally coupled to a seat frame via a pivot shaft, wherein a lower end of the seat back does not extend below the pivot shaft, a seat pan fixedly coupled to the seat frame, at least one quadrant arm fixedly coupled to the seat back and pivotally coupled to the pivot shaft, and a recline lock coupled to the one quadrant arm and the seat frame. The pivot shaft is coupled to the seat frame at a high pivot location, wherein the seat back is configured to pivot adjacent a lumbar region of a passenger's back. The seat pan may optionally include an extension from the seat pan that is configured to couple to the pivot shaft and fill a seat back aperture located between the lower end of the seat back and the seat pan.
    • 本发明的实施例包括经由枢轴可枢转地连接到座椅框架的座椅靠背,其中座椅靠背的下端不延伸到枢轴下方,座椅底座固定地连接到座椅框架,至少一个象限 固定地联接到座椅靠背并枢转地联接到枢轴的臂,以及联接到所述一个象限臂和座椅框架的斜倚锁。 枢转轴在高枢转位置处联接到座椅框架,其中座椅靠背构造成在乘客背部的腰部区域附近枢转。 座板可以可选地包括从座板的延伸部,该延伸部被构造成联接到枢轴并且填充位于座椅靠背的下端和座板之间的座椅靠背孔。
    • 8. 发明申请
    • DEPLOYMENT APPARATUSES
    • 部署设备
    • WO2010117758A2
    • 2010-10-14
    • PCT/US2010/029147
    • 2010-03-30
    • WEBER AIRCRAFT LLCWESTERINK, Rik
    • WESTERINK, Rik
    • B64D11/06
    • B64D11/00153B60N3/001B64D11/0015B64D11/0638Y10T16/5453Y10T16/546
    • Embodiments of the present invention include a deployment apparatus comprising a deployment object, a deployment arm, a deployment link, a pivot housing, at least two linear guides, and a gas spring. The deployment object is coupled to the deployment arm, which is pivotally coupled to the deployment link. An opposing end of the deployment link is fixedly coupled to a structure. The pivot housing is adjacent the connection between the deployment link and the deployment arm. The pivot housing is slidingly engaged with the at least two linear guides. The gas spring is coupled to the pivot housing, which pushes the pivot housing to an upper end of the at least two linear guides and causes the deployment link to rotate the deployment arm from a stowed angle to a released angle and results in a displaced vertical distance.
    • 本发明的实施例包括一种包括展开对象,展开臂,展开连杆,枢轴壳体,至少两个直线导向件和气体弹簧的展开装置。 部署对象被联接到部署臂,枢转地联接到部署链接。 部署链接的相对端固定地联接到结构。 枢轴壳体与部署连杆和部署臂之间的连接相邻。 枢转壳体与至少两个直线导轨滑动接合。 气弹簧联接到枢转壳体,枢轴壳体将枢轴壳体推动到至少两个线性引导件的上端,并且使得展开连杆将展开臂从收起角度旋转到释放角度,并导致位移垂直 距离。