-
公开(公告)号：US20130099053A1
公开(公告)日：2013-04-25
申请号：US13276357
申请日：2011-10-19
IPC分类号： B64D11/00 , B64C1/20 , B64D13/02 , B64D27/12 , B64C1/06 , B64C5/02 , B64C1/26 , B64C9/00 , B64C1/10 , B64C25/10 , B64C11/00
CPC分类号： B64D11/06 , B64C1/10 , B64C1/26 , B64C2001/0027 , B64C2001/0045 , B64C2025/125 , Y02T50/12 , Y02T50/46
摘要： An airplane comprises a twin-deck fuselage in which an upper deck support structure is utilized for carry-through of a mid-mount main wing box. The main landing gear of the airplane is mounted to the fuselage and is stowed in a non-pressurized area below the main wing box (enabled due to an optimized wing box geometry). A pressurized passageway/cargo/galley complex separates the main landing gear box and the main wing box. The upper deck is continuous, while the lower deck is separated by the wheel wells into two distinct fore and aft areas (for either cargo or passengers). The airplane further comprises an integrated vertical fin and an aft-extended pressurized deck area for reduced double-deck wetted area. More specifically, the double-deck pressurized fuselage structure is extended to form a blending structure to which a structural box of the vertical fin is attached.
摘要翻译： 一架飞机包括一个双层机身，其中上甲板支撑结构用于中档安装的主翼箱的穿通。 飞机的主起落架安装在机身上，并存放在主机箱下方的非加压区域（由于优化的机翼箱几何形状而启用）。 加压通道/货物/厨房复合体分离主起落架和主翼箱。 上甲板是连续的，而下甲板由轮井分隔成两个不同的前后区域（货物或乘客）。 飞机还包括集成的垂直翼片和用于减小双层接液面积的后延伸的加压甲板区域。 更具体地，双层加压机身结构被延伸以形成连接垂直翅片的结构箱的混合结构。
-
公开(公告)号：US08746616B2
公开(公告)日：2014-06-10
申请号：US13276357
申请日：2011-10-19
CPC分类号： B64D11/06 , B64C1/10 , B64C1/26 , B64C2001/0027 , B64C2001/0045 , B64C2025/125 , Y02T50/12 , Y02T50/46
摘要： An airplane comprises a twin-deck fuselage in which an upper deck support structure is utilized for carry-through of a mid-mount main wing box. The main landing gear of the airplane is mounted to the fuselage and is stowed in a non-pressurized area below the main wing box (enabled due to an optimized wing box geometry). A pressurized passageway/cargo/galley complex separates the main landing gear box and the main wing box. The upper deck is continuous, while the lower deck is separated by the wheel wells into two distinct fore and aft areas (for either cargo or passengers). The airplane further comprises an integrated vertical fin and an aft-extended pressurized deck area for reduced double-deck wetted area. More specifically, the double-deck pressurized fuselage structure is extended to form a blending structure to which a structural box of the vertical fin is attached.
摘要翻译： 一架飞机包括一个双层机身，其中上甲板支撑结构用于中档安装的主翼箱的穿通。 飞机的主起落架安装在机身上，并存放在主机箱下方的非加压区域（由于优化的机翼箱几何形状而启用）。 加压通道/货物/厨房复合体分离主起落架和主翼箱。 上甲板是连续的，而下甲板由轮井分隔成两个不同的前后区域（货物或乘客）。 飞机还包括集成的垂直翼片和用于减小双层接液面积的后延伸的加压甲板区域。 更具体地，双层加压机身结构被延伸以形成连接垂直翅片的结构箱的混合结构。
-
公开(公告)号：US20120168561A1
公开(公告)日：2012-07-05
申请号：US12722848
申请日：2010-03-12
CPC分类号： B64C25/12 , B64C25/18 , B64C25/26 , B64C2025/125
摘要： A landing gear for an aircraft. The landing gear may have a wheel/truck assembly, an oleo strut/support frame for supporting the wheel/truck assembly, and a retraction assembly attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a deployed position and a retracted position. The retraction assembly may have a pivoting trunnion brace attached to the oleo strut/support frame and to a fuselage of the aircraft for positioning the wheel/truck assembly, the oleo strut/support frame and the retraction assembly at least substantially fully within the fuselage of the aircraft in the retracted position.
摘要翻译： 飞机起落架。 起落架可以具有轮/卡车组件，用于支撑车轮/卡车组件的油支架/支撑框架和连接到油支架/支撑框架的缩回组件，该缩回组件用于将起落架移动在展开位置 和缩回位置。 缩回组件可以具有连接到油支架/支撑框架和机身的机身的枢转耳轴支架，用于将车轮/卡车组件，油支架/支撑框架和缩回组件至少基本上完全地设置在机身内 飞机处于缩回位置。
-
公开(公告)号：US08523107B2
公开(公告)日：2013-09-03
申请号：US12722848
申请日：2010-03-12
IPC分类号： B64C25/10
CPC分类号： B64C25/12 , B64C25/18 , B64C25/26 , B64C2025/125
摘要： A landing gear for an aircraft. The landing gear may have a wheel/truck assembly, an oleo strut/support frame for supporting the wheel/truck assembly, and a retraction assembly attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a deployed position and a retracted position. The retraction assembly may have a pivoting trunnion brace attached to the oleo strut/support frame and to a fuselage of the aircraft for positioning the wheel/truck assembly, the oleo strut/support frame and the retraction assembly at least substantially fully within the fuselage of the aircraft in the retracted position.
摘要翻译： 飞机起落架。 起落架可以具有轮/卡车组件，用于支撑车轮/卡车组件的油支架/支撑框架和连接到油支架/支撑框架的缩回组件，该缩回组件用于将起落架移动在展开位置 和缩回位置。 缩回组件可以具有连接到油支架/支撑框架和机身的机身的枢转耳轴支架，用于将车轮/卡车组件，油支架/支撑框架和缩回组件至少基本上完全地设置在机身内 飞机处于缩回位置。
-
公开(公告)号：US08876999B2
公开(公告)日：2014-11-04
申请号：US11761744
申请日：2007-06-12
CPC分类号： B29C70/44 , B29C35/0227 , B29L2031/3076 , B29L2031/3085 , Y02T50/43
摘要： Techniques and apparatus for providing a flexible shape low volume autoclave are disclosed. In one embodiment, an autoclave includes an elongated pressure vessel that is sealed on both ends and has a circumferential joint between a first portion and a second portion. The autoclave further includes the portions defining an interior configured for accepting an elongated part, the joint being configured to create an angle between the portions and further creating an opening with a seal, the opening facilitating an insertion of the part into the interior, and the seal enabling pressurization of the interior.
摘要翻译： 公开了用于提供柔性形状的低容量高压釜的技术和设备。 在一个实施例中，高压釜包括细长的压力容器，其在两端被密封并且在第一部分和第二部分之间具有圆周接头。 高压釜还包括限定内部的部分，所述内部构造成用于接收细长部分，所述接头构造成在所述部分之间产生角度并进一步产生具有密封件的开口，所述开口有助于将部件插入内部， 密封能够使内部加压。
-
公开(公告)号：US20120091273A1
公开(公告)日：2012-04-19
申请号：US12905581
申请日：2010-10-15
CPC分类号： B64C1/20 , B64D9/00 , B64D2009/006 , Y10T29/49716
摘要： Different advantageous embodiments provide a method and apparatus to increase a clearance of a cargo area of an aircraft. The apparatus and method may comprise an aircraft with a cargo area. A tray system may have a plurality of segment trays with each segment tray positioned between a plurality of floor beams located underneath a surface of the floor of the cargo area. A plurality of rollers in the tray system may be configured to allow an object to be moved across the cargo area.
摘要翻译： 不同的有利实施例提供了增加飞行器货物区域的间隙的方法和装置。 该装置和方法可以包括具有货物区域的飞行器。 托盘系统可以具有多个分段托盘，每个分段托盘定位在位于货物区域的地板表面下方的多个地板梁之间。 托盘系统中的多个辊子可以被配置成允许物体移动穿过货物区域。
-
公开(公告)号：US20080308224A1
公开(公告)日：2008-12-18
申请号：US11761744
申请日：2007-06-12
IPC分类号： B29C65/02
CPC分类号： B29C70/44 , B29C35/0227 , B29L2031/3076 , B29L2031/3085 , Y02T50/43
摘要： Techniques and apparatus for providing a flexible shape low volume autoclave are disclosed. In one embodiment, an autoclave includes an elongated pressure vessel that is sealed on both ends and has a circumferential joint between a first portion and a second portion. The autoclave further includes the portions defining an interior configured for accepting an elongated part, the joint being configured to create an angle between the portions and further creating an opening with a seal, the opening facilitating an insertion of the part into the interior, and the seal enabling pressurization of the interior.
摘要翻译： 公开了用于提供柔性形状的低容量高压釜的技术和设备。 在一个实施例中，高压釜包括细长的压力容器，其在两端被密封并且在第一部分和第二部分之间具有圆周接头。 高压釜还包括限定内部的部分，所述内部构造成用于接收细长部分，所述接头构造成在所述部分之间产生角度并进一步产生具有密封件的开口，所述开口有助于将部件插入内部， 密封能够对内部进行加压。
-
公开(公告)号：US08596580B1
公开(公告)日：2013-12-03
申请号：US12891394
申请日：2010-09-27
IPC分类号： B64D39/00
CPC分类号： B64D39/04
摘要： Apparatuses, systems, and methods described herein provide for a refueling boom having vertical control surfaces extending primarily downward below the horizontal control surfaces out of the auxiliary power unit (APU) exhaust and airframe-induced turbulent flow fields, while reducing the torque moments applied to the boom beam and increasing control authority. According to one aspect of the disclosure provided herein, a refueling boom includes a boom beam, at least one horizontal control surface, and a pair of vertical control surfaces. The vertical control surfaces are positioned on opposing ends of the horizontal control surfaces and each include an upper portion and a longer lower portion projecting downward below the horizontal control surface. Aspects further improve the aerodynamic characteristics of the boom beam, reducing the drag associated with the refueling boom.
摘要翻译： 本文所述的装置，系统和方法提供了一种加油悬臂，其具有垂直控制表面，其垂直控制表面主要向下延伸到辅助动力单元（APU）排气和机体引起的湍流流场外的水平控制表面之下，同时减小施加到 繁荣梁和增加的控制权。 根据本文提供的本公开的一个方面，加油吊杆包括吊臂梁，至少一个水平控制表面和一对垂直控制表面。 垂直控制表面位于水平控制表面的相对端上，并且每个包括在水平控制表面下方向下突出的上部和较长的下部。 方面进一步改善了起重臂梁的空气动力特性，减少了与加油臂相关联的阻力。
-
公开(公告)号：US08220741B2
公开(公告)日：2012-07-17
申请号：US12147731
申请日：2008-06-27
IPC分类号： B64D11/06
CPC分类号： B64D11/00 , B64D11/0601
摘要： A method may be present for configuring an aircraft. A design may be identified for the aircraft. A passenger area may be configured using a set of synthetic aisles to meet a desired passenger density for the design.
摘要翻译： 可能存在用于配置飞行器的方法。 可以为飞机识别出设计。 可以使用一组合成通道来配置乘客区域，以满足设计所需的乘客密度。
-
公开(公告)号：US08561946B2
公开(公告)日：2013-10-22
申请号：US12905581
申请日：2010-10-15
IPC分类号： B64C1/20
CPC分类号： B64C1/20 , B64D9/00 , B64D2009/006 , Y10T29/49716
摘要： Different advantageous embodiments provide a method and apparatus to increase a clearance of a cargo area of an aircraft. The apparatus and method may comprise an aircraft with a cargo area. A tray system may have a plurality of segment trays with each segment tray positioned between a plurality of floor beams located underneath a surface of the floor of the cargo area. A plurality of rollers in the tray system may be configured to allow an object to be moved across the cargo area.
-
-
-
-
-
-
-
-
-
搜索结果
11 条记录 (耗时 0.02 秒)
