公开(公告)号：US20070120010A1

公开(公告)日：2007-05-31

申请号：US11502961

申请日：2006-08-11

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

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

IPC分类号： B64D27/12

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：US20050274485A1

公开(公告)日：2005-12-15

申请号：US10867417

申请日：2004-06-14

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

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

IPC分类号： B22C9/22

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机的元件上。 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 。