公开(公告)号：US07398945B2

公开(公告)日：2008-07-15

申请号：US11502961

申请日：2006-08-11

申请人： George L. Huggins ,  Brian J. Meyer ,  Lee J. Post ,  Gordon R. Crook ,  Scott N. Nelson ,  Stanley T. Kampf ,  Aaron R. Heitmann ,  Hafizullah Wardak ,  Daniel J. Allison ,  Joseph W. Camenzind

发明人： George L. Huggins ,  Brian J. Meyer ,  Lee J. Post ,  Gordon R. Crook ,  Scott N. Nelson ,  Stanley T. Kampf ,  Aaron R. Heitmann ,  Hafizullah Wardak ,  Daniel J. Allison ,  Joseph W. Camenzind

IPC分类号： B64D27/26

CPC分类号： B22C9/22 ,  B64D27/26 ,  B64D2027/264

摘要： A truss structure well suited for use as an engine strut on a commercial aircraft. The truss structure is cast as a single piece integrally formed component from a titanium alloy or another suitably lightweight, structurally strong material. The truss structure includes a plurality of integrally formed attachment structures which enable the truss structure to be secured to an element of an aircraft such as a wing. A plurality of attachment areas for an element such as an engine is also formed that allows the element (e.g. jet engine) to be secured to the truss structure. The truss structure includes a plurality of elongated rails and truss elements that are arranged to provide redundant load paths to ensure that a failure of any one truss element or elongated rail will not result in a failure of the overall truss structure to support whatever load is required.

摘要翻译： 桁架结构非常适合用作商用飞机上的发动机支柱。 桁架结构由钛合金或其他适当重量轻，结构坚固的材料铸造为单件整体成形件。 桁架结构包括多个整体形成的附接结构，其能够将桁架结构固定到诸如机翼的飞行器的元件上。 还形成用于诸如发动机的元件的多个附接区域，其允许元件（例如喷气发动机）固定到桁架结构。 桁架结构包括多个细长轨道和桁架元件，其布置成提供冗余的载荷路径，以确保任何一个桁架元件或细长导轨的故障不会导致整个桁架结构的故障，以支持所需的任何载荷 。

公开(公告)号：US08479460B1

公开(公告)日：2013-07-09

申请号：US12857188

申请日：2010-08-16

申请人： Brian J. Meyer

发明人： Brian J. Meyer

IPC分类号： E04F11/16

CPC分类号： E04D12/006 ,  E04B5/10 ,  E04B2001/2415 ,  E04B2001/2439 ,  E04B2001/2442 ,  E04B2001/2448 ,  E04B2001/2457 ,  E04B2001/2472

摘要： A deck system includes plural deck units fastened together and carried directly by the framing system of a building directly or indirectly by frame elements that are themselves carried by the framing system. To relieve lateral forces on the deck system that exceed a pre-engineered level, these frame elements include a slidable support and slidable brackets both with slotted holes that permit controlled and limited movement of the deck system in two mutually orthogonal directions with respect to the framing system of the building. In addition, the individual deck units may move horizontally with respect to the each other and the framing system. Each decking unit may be connected to an adjacent decking unit using a slotted hole formed in one of its two side laps.

摘要翻译： 甲板系统包括多个甲板单元，它们由建筑物的框架系统由建筑物的框架系统直接地或间接地紧固在一起并由框架元件直接承载，框架元件本身由框架系统承载。 为了减轻甲板系统上超过预设水平面的侧向力，这些框架元件包括可滑动的支撑件和可滑动的支架，其具有开槽孔，其允许甲板系统相对于框架在两个相互正交的方向上受控和有限地运动 建筑系统。 此外，单个甲板单元可以相对于彼此和框架系统水平移动。 每个装甲单元可以使用在其两个侧面圈之一中形成的开槽孔连接到相邻的甲板单元。

公开(公告)号：US07104306B2

公开(公告)日：2006-09-12

申请号：US10867417

申请日：2004-06-14

申请人： George L Huggins ,  Brian J Meyer ,  Lee J Post ,  Gordon R Crook ,  Scott N Nelson ,  Stanley T Kampf ,  Aaron R Heitmann ,  Hafizullah Wardak ,  Daniel J Allison ,  Joseph W Camenzind

发明人： George L Huggins ,  Brian J Meyer ,  Lee J Post ,  Gordon R Crook ,  Scott N Nelson ,  Stanley T Kampf ,  Aaron R Heitmann ,  Hafizullah Wardak ,  Daniel J Allison ,  Joseph W Camenzind

IPC分类号： B22D23/00

CPC分类号： B22C9/22 ,  B64D27/26 ,  B64D2027/264

摘要： A truss structure well suited for use as an engine strut on a commercial aircraft. The truss structure is cast as a single piece integrally formed component from a titanium alloy or another suitably lightweight, structurally strong material. The truss structure includes a plurality of integrally formed attachment structures which enable the truss structure to be secured to an element of an aircraft such as a wing. A plurality of attachment areas for an element such as an engine is also formed that allows the element (e.g. jet engine) to be secured to the truss structure. The truss structure includes a plurality of elongated rails and truss elements that are arranged to provide redundant load paths to ensure that a failure of any one truss element or elongated rail will not result in a failure of the overall truss structure to support whatever load is required.

摘要翻译： 桁架结构非常适合用作商用飞机上的发动机支柱。 桁架结构由钛合金或其他适当重量轻，结构坚固的材料铸造为单件整体成形件。 桁架结构包括多个整体形成的附接结构，其能够将桁架结构固定到诸如机翼的飞行器的元件上。 还形成用于诸如发动机的元件的多个附接区域，其允许元件（例如喷气发动机）固定到桁架结构。 桁架结构包括多个细长轨道和桁架元件，其布置成提供冗余的载荷路径，以确保任何一个桁架元件或细长导轨的故障不会导致整个桁架结构的故障，以支持所需的任何载荷 。