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1.发明授权公开(公告)号：US08439310B2
公开(公告)日：2013-05-14
申请号：US12702869
申请日：2010-02-09
CPC分类号： B64C39/068
摘要： An aircraft comprises: a fuselage; a front pair of wings; a rear pair of wings; and a pair of bodies, each body interconnecting, at a distance from the fuselage, the front and rear wings that are situated on the same side of the fuselage.
摘要翻译： 飞机包括：机身; 一对前翅; 一对后翅; 以及一对身体，每个身体在与机身一定距离处相互连接，前后翼位于机身的同一侧。
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公开(公告)号：US08297551B2
公开(公告)日：2012-10-30
申请号：US12721083
申请日：2010-03-10
IPC分类号： B64C25/14
CPC分类号： B64C25/12 , B64C25/34 , B64C2025/125
摘要： The airplane comprises a fuselage having frames, and at least two undercarriages each comprising a support and at least one wheel, the support being carried directly by the fuselage and being hinged to the fuselage about an axis that lies outside the frames.The undercarriage is movable between an operational position in which the or each wheel is vertical, and a rest position.The support and the wheel have a configuration such that, in the rest position, the undercarriage extends circumferentially relative to the fuselage and outside the frames.
摘要翻译： 飞机包括具有框架的机身，并且至少两个底架，每个底架包括支撑件和至少一个车轮，所述支撑件由机身直接承载并且围绕位于框架外部的轴线铰接到机身。 起落架可在其中每个车轮垂直的操作位置和静止位置之间移动。 支撑件和车轮具有这样的构造，使得在静止位置，起落架相对于机身并且在框架外部周向延伸。
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公开(公告)号：USD621776S1
公开(公告)日：2010-08-17
申请号：US29355518
申请日：2010-02-09
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公开(公告)号：US09051042B2
公开(公告)日：2015-06-09
申请号：US13477270
申请日：2012-05-22
摘要： An aircraft including a fuselage which extends along a longitudinal axis. The fuselage includes a substantially cylindrical central portion and a rear portion that may have a flattened or conventional shape. This rear portion which comprises the rear end of the fuselage includes a support surface which bears at least one horizontal stabilizer and/or vertical stabilizer. The rear portion is able to pivot in relation to the central portion around an axis such as the pitch axis, at least one stabilizer or the support surface being equipped with at least one control surface.
摘要翻译： 一种飞机，包括沿着纵向轴线延伸的机身。 机身包括基本上圆柱形的中心部分和可以具有扁平或常规形状的后部部分。 该后部包括机身的后端，其包括支撑表面，该支承表面至少具有一个水平稳定器和/或垂直稳定器。 后部能够围绕诸如俯仰轴线的轴线相对于中心部分枢转，至少一个稳定器或支撑表面配备有至少一个控制表面。
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公开(公告)号：US08550400B2
公开(公告)日：2013-10-08
申请号：US12494845
申请日：2009-06-30
IPC分类号： B64C1/00
CPC分类号： B64C1/068 , B64C25/04 , B64C2001/0045
摘要： An aircraft has a fuselage of elongated form along a longitudinal axis X corresponding essentially to the longitudinal axis of the aircraft. In a first forward section, the fuselage includes a cockpit in front of a cockpit bulkhead and a front landing gear associated with a landing gear compartment located behind the cockpit bulkhead. The front landing gear and the landing gear compartment are at least partially beneath a floorboard of a compartment of a lower space of the fuselage and in a bulge that increases a volume available for installation of the landing gear.
摘要翻译： 飞行器具有沿着基本上与飞行器的纵向轴线对应的纵向轴线X的细长形式的机身。 在第一个前部，机身包括在驾驶舱舱壁前面的驾驶舱和与位于驾驶舱舱壁后面的起落架舱相关联的前起落架。 前起落架和起落架舱至少部分地位于机身较低空间的隔间的地板下方，并且在凸起中增加可用于安装起落架的体积。
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公开(公告)号：USD621335S1
公开(公告)日：2010-08-10
申请号：US29355516
申请日：2010-02-09
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公开(公告)号：USD621334S1
公开(公告)日：2010-08-10
申请号：US29355515
申请日：2010-02-09
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公开(公告)号：US09102395B2
公开(公告)日：2015-08-11
申请号：US12789761
申请日：2010-05-28
IPC分类号： F02K3/02 , F02K1/00 , F02K1/54 , B64C29/00 , B64C15/02 , B64D35/04 , F02K1/58 , F02K1/60 , F02K1/76 , F02K1/12 , F02K1/70 , F02K1/72
CPC分类号： B64C15/02 , B64D35/04 , F02K1/008 , F02K1/12 , F02K1/1223 , F02K1/58 , F02K1/60 , F02K1/70 , F02K1/72 , F02K1/763 , Y02T50/671
摘要： A propulsive system for aircraft that has a jet engine and a nacelle surrounding the aforementioned jet engine. The nacelle has a front section fixed relative to the jet engine, and a rear extremity behind the front section, and has a rear section with two petals hinged relative to the front section. Each of the two petals in a position called zero-setting forms an extension of the front section of the nacelle in which the inside and outside surfaces of the petals and, respectively, determine the aerodynamic forms of the rear section, which are in geometric continuity with the inside and outside surfaces and, respectively, that determine the aerodynamic forms of the front section. The petals can be set individually at a positive or negative setting angle to put into play the reverser, APU, air brake, vectorial, and taxiing modes of the propulsive system.
摘要翻译： 用于具有喷气发动机和围绕上述喷气发动机的机舱的飞行器的推进系统。 机舱具有相对于喷气发动机固定的前部分，并且在前部后方具有后端，并且具有后部，其具有相对于前部铰接的两个瓣。 位于称为零位置的两个花瓣中的每一个形成机舱的前部的延伸部，其中花瓣的内侧和外侧表面分别确定后部的空气动力学形状，其具有几何连续性 内表面和外表面分别确定前部的空气动力学形式。 花瓣可以以正或负设置角度单独设置，以投入推进系统的反向器，APU，空气制动，矢量和滑行模式。
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公开(公告)号：US08651414B2
公开(公告)日：2014-02-18
申请号：US13255720
申请日：2010-03-12
IPC分类号： B64C1/00
CPC分类号： B64C1/068 , B64C1/26 , B64C5/06 , B64C2001/0045 , B64D27/20 , B64D29/04 , Y02T50/12 , Y02T50/44
摘要： An airplane, including a fuselage having an elongate shape along a longitudinal axis of the airplane, and at least one wing attached to the fuselage between front and back ends of the fuselage and a substantially cylindrical central portion and a rear scaleable portion on which a vertical tail assembly and a rear propulsion assembly are attached. Between a section for connecting the rear portion to the central portion of the fuselage and the back end: the maximum width of each fuselage section is constant or increases towards the rear up to a maximum fuselage width L; the height of each fuselage section decreases towards the rear, such that the back end of the fuselage forms a thin trailing edge substantially horizontal in the indicating line of the airplane and substantially rectilinear; a reactor for the propulsion assembly is provided in a so-called semi-buried configuration in the fuselage.
摘要翻译： 一种飞机，包括沿着飞机的纵向轴线具有细长形状的机身，以及至少一个机翼，其附接到机身的前端和后端之间的机身，以及基本上圆柱形的中心部分和后可缩放部分，垂直 尾部组件和后推进组件。 在用于将后部连接到机身中心部分的部分和后端之间：每个机身部分的最大宽度是恒定的或者朝向后方增加到最大机身宽度L; 每个机身部分的高度朝向后方减小，使得机身的后端在飞机的指示线上形成基本上水平的薄的后缘，并且基本上是直线的; 用于推进组件的反应器以机身中的所谓半埋式构造提供。
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公开(公告)号：USD621775S1
公开(公告)日：2010-08-17
申请号：US29355508
申请日：2010-02-09
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