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公开(公告)号：US07891608B2
公开(公告)日：2011-02-22
申请号：US11743929
申请日：2007-05-03
申请人： Blaine K. Rawdon , Robert E. Grip
发明人： Blaine K. Rawdon , Robert E. Grip
IPC分类号： B64C1/00
摘要： An aircraft for carrying cargo in one or more containers. The aircraft includes a fuselage structure having a plurality of nodes and a plurality of elements connecting the nodes to form a space frame in which to carry cargo. At least some of the nodes are positioned in the space frame based on dimensions of the one or more containers. The fuselage structure is more compact, lighter and less expensive compared to conventional semi-monocoque fuselages.
摘要翻译： 用于在一个或多个容器中运送货物的飞机。 飞机包括具有多个节点的机身结构和连接节点的多个元件以形成其中携带货物的空间框架。 基于一个或多个容器的尺寸，至少一些节点位于空间框架中。 与传统的半单壳机身相比，机身结构更紧凑，更轻，更便宜。
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公开(公告)号：US07743763B2
公开(公告)日：2010-06-29
申请号：US11829456
申请日：2007-07-27
IPC分类号： F24J2/00
CPC分类号： H01L31/052 , F28F2013/006 , Y02E10/50
摘要： In one embodiment, an assembly having bodies of different thermal expansion rates comprises a first body, a second body having a different thermal expansion rate than the first body, and a plurality of high conductivity members attached to both the first and second bodies. The high conductivity members are more flexible than the first and second bodies in order to allow for varied thermal expansion of the first and second bodies. The assembly may comprise a solar collector assembly, wherein the first body is a solar cell attached to a substrate, and the second body is a heat sink.
摘要翻译： 在一个实施例中，具有不同热膨胀率的主体的组件包括第一主体，具有与第一主体不同的热膨胀率的第二主体，以及附接到第一主体和第二主体两者的多个高导电构件。 高导电性构件比第一和第二主体更灵活，以允许第一和第二主体的变化的热膨胀。 组件可以包括太阳能收集器组件，其中第一主体是附接到基板的太阳能电池，并且第二主体是散热器。
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公开(公告)号：US20090025712A1
公开(公告)日：2009-01-29
申请号：US11829456
申请日：2007-07-27
IPC分类号： F24J2/46
CPC分类号： H01L31/052 , F28F2013/006 , Y02E10/50
摘要： In one embodiment, an assembly having bodies of different thermal expansion rates comprises a first body, a second body having a different thermal expansion rate than the first body, and a plurality of high conductivity members attached to both the first and second bodies. The high conductivity members are more flexible than the first and second bodies in order to allow for varied thermal expansion of the first and second bodies. The assembly may comprise a solar collector assembly, wherein the first body is a solar cell attached to a substrate, and the second body is a heat sink.
摘要翻译： 在一个实施例中，具有不同热膨胀率的主体的组件包括第一主体，具有与第一主体不同的热膨胀率的第二主体，以及附接到第一主体和第二主体两者的多个高导电构件。 高导电性构件比第一和第二主体更灵活，以允许第一和第二主体的变化的热膨胀。 组件可以包括太阳能收集器组件，其中第一主体是附接到基板的太阳能电池，并且第二主体是散热器。
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公开(公告)号：US20080272236A1
公开(公告)日：2008-11-06
申请号：US11743929
申请日：2007-05-03
申请人： Blaine K. Rawdon , Robert E. Grip
发明人： Blaine K. Rawdon , Robert E. Grip
IPC分类号： B64C1/06
摘要： An aircraft for carrying cargo in one or more containers. The aircraft includes a fuselage structure having a plurality of nodes and a plurality of elements connecting the nodes to form a space frame in which to carry cargo. At least some of the nodes are positioned in the space frame based on dimensions of the one or more containers. The fuselage structure is more compact, lighter and less expensive compared to conventional semi-monocoque fuselages.
摘要翻译： 用于在一个或多个容器中运送货物的飞机。 飞机包括具有多个节点的机身结构和连接节点的多个元件以形成其中携带货物的空间框架。 基于一个或多个容器的尺寸，至少一些节点位于空间框架中。 与传统的半单壳机身相比，机身结构更紧凑，更轻，更便宜。
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公开(公告)号：US08128025B2
公开(公告)日：2012-03-06
申请号：US12053345
申请日：2008-03-21
申请人： Blaine K. Rawdon , Robert E. Grip
发明人： Blaine K. Rawdon , Robert E. Grip
IPC分类号： B64C1/12
摘要： An aircraft including a space frame fuselage structure. A plurality of panels are connected with the structure and configured to form a skin over the structure. The panels are movable relative to one another so as to prevent loading of the structure from inducing loading in the skin.
摘要翻译： 一架飞机包括一个空间框架机身结构。 多个面板与该结构连接并且构造成在结构上形成皮肤。 所述面板可相对于彼此移动，以防止所述结构的加载导致皮肤中的负载。
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公开(公告)号：US20090236473A1
公开(公告)日：2009-09-24
申请号：US12053345
申请日：2008-03-21
申请人： Blaine K. Rawdon , Robert E. Grip
发明人： Blaine K. Rawdon , Robert E. Grip
IPC分类号： B64C1/00
摘要： An aircraft including a space frame fuselage structure. A plurality of panels are connected with the structure and configured to form a skin over the structure. The panels are movable relative to one another so as to prevent loading of the structure from inducing loading in the skin.
摘要翻译： 一架飞机包括一个空间框架机身结构。 多个面板与该结构连接并且构造成在结构上形成皮肤。 所述面板可相对于彼此移动，以防止所述结构的加载导致皮肤中的负载。
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公开(公告)号：US07845898B2
公开(公告)日：2010-12-07
申请号：US12421952
申请日：2009-04-10
IPC分类号： B65G67/00
CPC分类号： B65G69/006 , B64D9/00 , B64F1/32 , B65G67/20 , Y02T50/46
摘要： A system and method for cargo handling is provided. The system includes a transport vehicle including a cargo bay capable of housing a plurality of cargo containers, and a loading dock for coupling to the cargo bay. The system also includes at least one railcar and pylons positioned along a floor of the cargo bay. A predetermined number of pylons are operable to elevate and lower a cargo container within the cargo bay. The present invention also provides a railcar for transporting cargo containers, as well as an apparatus for positioning at least one cargo container within a transport vehicle. The present invention also provides a system for aligning a loading dock and a transport vehicle that includes a mechanism for adjusting the height of the transport vehicle or loading dock, or a plurality of engagement members that are capable of aligning the loading dock and transport vehicle.
摘要翻译： 提供了一种用于货物处理的系统和方法。 该系统包括运输车辆，其包括能够容纳多个货物集装箱的货舱和用于联接到货舱的装载台。 该系统还包括沿着货舱的地板定位的至少一个轨道车和塔架。 预定数量的塔架可操作以升高和降低货舱内的货物集装箱。 本发明还提供一种用于运输货物集装箱的轨道车，以及用于将至少一个货物集装箱定位在运输车辆内的装置。 本发明还提供了一种用于对准装载台和运输车辆的系统，该系统包括用于调节运输车辆或装载码头的高度的机构，或者能够对准装载底座和运输车辆的多个接合构件。
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公开(公告)号：US20100074758A1
公开(公告)日：2010-03-25
申请号：US12237911
申请日：2008-09-25
CPC分类号： F01D5/147 , B64C11/00 , B64C27/18 , F01D5/145 , F01D5/18 , F03D1/0675 , F04D29/324 , F04D29/38 , F04D29/663 , Y02E10/721 , Y02T50/671 , Y02T50/673 , Y02T50/676
摘要： A rotor blade including a root attachable to a rotor hub. The blade includes a tip and one or more channels aligned within the blade generally between the root and the tip. Each channel has a sealed first end and a second end vented to outside the blade. The channel(s) are vented to one or more exterior surfaces of the blade through one or more apertures in the exterior surface(s).
摘要翻译： 一种转子叶片，其包括可附接到转子毂的根部。 叶片包括尖端以及通常在根部和尖端之间在叶片内对齐的一个或多个通道。 每个通道具有密封的第一端和通向叶片外部的第二端。 通道通过外表面中的一个或多个孔被排放到叶片的一个或多个外表面。
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9.发明授权公开(公告)号：US06497389B1
公开(公告)日：2002-12-24
申请号：US09945102
申请日：2001-08-31
申请人： Blaine K. Rawdon , Arthur V. Hawley
发明人： Blaine K. Rawdon , Arthur V. Hawley
IPC分类号： B64D2500
CPC分类号： B66F3/35 , B64D25/00 , B64D2201/00 , Y10S244/905
摘要： An airbag system for elevating the fuselage of an aircraft off a landing surface a sufficient degree to allow for emergency egress of passengers and crew through ventral emergency exit doors. An airbag assembly made up of a plurality of independent airbags is disposed within the aircraft. When activated, the airbag system deploys the airbags external of the aircraft that elevate the fuselage of the aircraft a sufficient degree to allow for utilizing the ventral emergency exit doors on the fuselage to enable evacuating the passengers and crew. An activation mechanism is connected to the inflation.devices associated with each of the airbags. The activation mechanism generates an electrical signal which activates the inflation devices, which in turn fill the airbags with a compressed fluid, thus expanding the airbags and lifting the fuselage. A crew member initiates the activation of the airbag system through one or more switches.
摘要翻译： 一种气囊系统，用于将飞机的机身从足够的角度提升到足够的程度，以允许乘客和船员通过腹侧紧急出口门的紧急出口。 由多个独立安全气囊组成的气囊组件设置在飞机内。 当活动时，气囊系统部署飞行器外部的安全气囊，以提升机身机身足够的程度，以便利用机身上的腹侧紧急出口门，以使乘客和机组人员能够撤离。 激活机构连接到与每个安全气囊相关联的通风装置。 激活机构产生电信号，其激活充气装置，充气装置又用压缩流体填充安全气囊，从而使安全气囊膨胀并提升机身。 机组人员通过一个或多个开关启动气囊系统的启动。
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公开(公告)号：US5542798A
公开(公告)日：1996-08-06
申请号：US322701
申请日：1994-10-13
CPC分类号： B60P7/0861 , B60P7/083 , Y10T24/2175
摘要： Restraining and tensioning apparatus (10) for a cargo tie-down belt (12) has a chassis (26) with a fluted spindle (98) onto which the belt is wound, ratchet gears (120,122), tensioning lever (28), and two pairs of locking pawls (136, 138, 148, 150), each locking pawl being engaged by an individual spring urging the pawl into contact with a ratchet gear.
摘要翻译： 用于货物捆扎带（12）的限制和张紧装置（10）具有底盘（26），带有带槽的主轴（98），所述带被卷绕在其上，棘轮（120,122），张紧杆（28）和 两对锁定爪（136,138,148,150），每个锁定爪由单独的弹簧接合，以推动棘爪与棘轮啮合。
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