专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20080139100A1 ADJUSTABLE CABIN NOZZLE 有权
标题翻译：可调节的客舱喷嘴
公开(公告)号：US20080139100A1
公开(公告)日：2008-06-12
申请号：US11609474
申请日：2006-12-12
申请人： Raymond H. Horstman , Scott W. Bohm , Kenneth J. Walter , Steven L. Williams , Kirk D. Skaggs , John M. Brown , Chao-Hsin Lin
发明人： Raymond H. Horstman , Scott W. Bohm , Kenneth J. Walter , Steven L. Williams , Kirk D. Skaggs , John M. Brown , Chao-Hsin Lin
IPC分类号： B64D13/00
CPC分类号： B64D13/00 , B64D2013/0625
摘要： An aircraft air distribution system includes a base and first and second arrays of nozzle air transfer ports in the base. An adjustable flow plate is positioned over the nozzle air transfer ports. A compressible member is located between the base and the adjustable flow plate and between the first and second arrays. First and second air ejector regions are located, respectively, on the sides of the compressible member between the base and the adjustable flow plate to connect to the first and second arrays, and direct air from the first and second arrays from the sides of the base. Fasteners moveably connect the adjustable flow plate to the base and are adjustable to change a size of different sections of the first and second air ejector regions to change an amount of airflow originating from the different sections of these regions.
摘要翻译：飞机空气分配系统包括基座和基座中的第一和第二喷嘴空气传送孔阵列。可调节的流动板位于喷嘴空气传输端口上方。可压缩构件位于基座和可调节流动板之间以及第一和第二阵列之间。第一和第二空气喷射器区域分别位于基座和可调节流动板之间的可压缩构件的侧面上，以连接到第一和第二阵列，并且从基座的侧面引导来自第一和第二阵列的空气。紧固件可移动地将可调节流动板连接到基座并且可调节以改变第一和第二空气喷射器区域的不同部分的尺寸，以改变源自这些区域的不同部分的气流量。

2. 发明授权

US07287701B2 Handheld coordinate reference system 有权
标题翻译：手持座标参考系
公开(公告)号：US07287701B2
公开(公告)日：2007-10-30
申请号：US11059779
申请日：2005-02-17
申请人： Gary E. Miller , William O. Price , Kirk D. Skaggs
发明人： Gary E. Miller , William O. Price , Kirk D. Skaggs
IPC分类号： G06K7/10
CPC分类号： G01S17/89 , G01S17/023
摘要： A method and apparatus for determining a spatial position of interest in an assembly is disclosed. In one embodiment, the method comprises the steps of determining a reference position of reference unit; moving the reference unit from the reference position to the first spatial position; inertially measuring a displacement of the reference unit while the reference unit is unilluminated by an illuminator; and determining the first position from the reference position, illuminator energy reflected from the reference unit, and the inertially measured displacement of the reference unit.
摘要翻译：公开了一种用于确定组件中感兴趣的空间位置的方法和装置。在一个实施例中，该方法包括以下步骤：确定参考单元的参考位置; 将参考单元从参考位置移动到第一空间位置; 在参考单元被照明器未照亮的同时惯性地测量参考单元的位移; 以及从参考位置确定第一位置，从参考单元反射的照明器能量以及参考单元的惯性测量位移。

3. 发明授权

US6024555A Tooling having compliant forming surface for forming resin composites 失效
标题翻译：具有用于形成树脂复合材料的柔性成形表面的模具
公开(公告)号：US6024555A
公开(公告)日：2000-02-15
申请号：US956331
申请日：1997-10-23
申请人： Harold M. Goodridge , Kirk D. Skaggs
发明人： Harold M. Goodridge , Kirk D. Skaggs
IPC分类号： B29C33/30 , B29C33/40 , B29C33/42 , B29C43/36 , B29C70/44 , B29C70/42
CPC分类号： B29C43/021 , B29C33/303 , B29C33/405 , B29C43/12 , B29C43/3642 , B29C70/44 , B29C2043/3644 , B29C2043/3657 , B29C33/42 , B29K2105/0854 , B29L2031/003 , Y10S425/044
摘要： A tooling concept uses a compliant forming surface for forming composite parts. The tooling concept utilizes a rigid support substructure that has a thin compliant forming surface. In the preferred embodiment of the invention, the tooling concept is used to form a composite sine wave spar. A preferred embodiment of the tooling concept includes upper and lower tool inserts and side tool inserts. The upper tool insert has a compliant forming surface that is located in between a rigid support substructure and the composite material used to form the composite part. Composite prepreg is laid up over a sine wave contour on the upper and lower tool inserts to form upper and lower U-shaped composite workpieces. The upper and lower tool inserts and workpieces are then brought together to form a sine wave I-beam. Radius fillers are then applied to the intersections between the upper and lower composite workpieces and cap strips are placed over the flanges of the joined composite workpieces. Side tools and end tools are then placed around the joined upper and lower tool inserts. The resulting assembly is covered with a breather cloth, baked in a vacuum bag and cured in an autoclave. During curing, the autoclave applies a hydrostatic pressure on the upper tool insert and thus compliant forming surface. The compliant forming surface in turn applies a consolidation and forming pressure to the composite workpiece within the tools. During curing, the compliant forming surface deforms slightly to account for thickness variations in the composite workpiece in order to produce a better quality formed composite part.
摘要翻译：工具概念使用柔性成形表面来形成复合部件。工具概念使用具有薄柔顺成形表面的刚性支撑子结构。在本发明的优选实施例中，工具概念用于形成复合正弦波形梁。工具概念的优选实施例包括上部和下部工具插入件和侧面工具插入件。上部工具插入件具有柔顺的成形表面，其位于刚性支撑子结构和用于形成复合部件的复合材料之间。复合预浸料在上下工具刀片上放置在正弦波轮廓上，形成上下U型复合工件。然后将上下工具插入件和工件组合在一起以形成正弦波I型梁。然后将半径填料施加到上复合工件和下复合工件之间的相交处，并将盖带放置在连接的复合工件的凸缘上。然后将侧面工具和端部工具放置在连接的上部和下部工具插入件周围。所得组件用通气布覆盖，在真空袋中烘烤并在高压釜中固化。在固化期间，高压釜在上部工具插入件上施加静水压力，从而在柔性成形表面上施加静水压力。柔性成形表面又对工具内的复合工件施加固结和成形压力。在固化期间，柔性成形表面略微变形以考虑复合材料工件中的厚度变化，以便产生更好质量的成形复合材料部件。

4. 发明授权

US08016650B2 Adjustable cabin nozzle 有权
标题翻译：可调节客舱喷嘴
公开(公告)号：US08016650B2
公开(公告)日：2011-09-13
申请号：US11609474
申请日：2006-12-12
申请人： Raymond H. Horstman , Scott W. Bohm , Kenneth J. Walter , Steven L. Williams , Kirk D. Skaggs , John M. Brown , Chao-Hsin Lin
发明人： Raymond H. Horstman , Scott W. Bohm , Kenneth J. Walter , Steven L. Williams , Kirk D. Skaggs , John M. Brown , Chao-Hsin Lin
IPC分类号： F24F9/00
CPC分类号： B64D13/00 , B64D2013/0625
摘要： An aircraft air distribution system includes a base and first and second arrays of nozzle air transfer ports in the base. An adjustable flow plate is positioned over the nozzle air transfer ports. A compressible member is located between the base and the adjustable flow plate and between the first and second arrays. First and second air ejector regions are located, respectively, on the sides of the compressible member between the base and the adjustable flow plate to connect to the first and second arrays, and direct air from the first and second arrays from the sides of the base. Fasteners moveably connect the adjustable flow plate to the base and are adjustable to change a size of different sections of the first and second air ejector regions to change an amount of airflow originating from the different sections of these regions.
摘要翻译：飞机空气分配系统包括基座和基座中的第一和第二喷嘴空气传送孔阵列。可调节的流动板位于喷嘴空气传输端口上方。可压缩构件位于基座和可调节流动板之间以及第一和第二阵列之间。第一和第二空气喷射器区域分别位于基座和可调节流动板之间的可压缩构件的侧面上，以连接到第一和第二阵列，并且从基座的侧面引导来自第一和第二阵列的空气。紧固件可移动地将可调节流动板连接到基座并且可调节以改变第一和第二空气喷射器区域的不同部分的尺寸，以改变源自这些区域的不同部分的气流量。

5. 发明授权

US5714179A Rigid tooling with compliant forming surface for forming parts from composite materials 失效
标题翻译：刚性工具具有柔性成型表面，用于从复合材料形成零件
公开(公告)号：US5714179A
公开(公告)日：1998-02-03
申请号：US544969
申请日：1995-10-30
申请人： Harold M. Goodridge , Kirk D. Skaggs
发明人： Harold M. Goodridge , Kirk D. Skaggs
IPC分类号： B29C33/30 , B29C33/40 , B29C33/42 , B29C43/36 , B29C70/44 , B29C70/42
CPC分类号： B29C43/021 , B29C33/303 , B29C33/405 , B29C43/12 , B29C43/3642 , B29C70/44 , B29C2043/3644 , B29C2043/3657 , B29C33/42 , B29K2105/0854 , B29L2031/003 , Y10S425/044
摘要： A tooling concept having a compliant forming surface for forming composite parts. The tooling concept utilizes a rigid support substructure that has a thin compliant forming surface. In the preferred embodiment of the invention, the tooling concept is used to form a composite sine wave spar. A preferred embodiment of the tooling concept includes upper and lower tool inserts and side tool inserts. The upper tool insert has a compliant forming surface that is located in between a rigid support substructure and the composite material used to form the composite part. Composite prepreg is laid up over a sine wave contour on the upper and lower tool inserts to form upper and lower U-shaped composite workpieces. The upper and lower tool inserts and workpieces are then brought together to form a sine wave I-beam. Radius fillers are then applied to the intersections between the upper and lower composite workpieces and cap strips are placed over the flanges of the joined composite workpieces. Side tools and end tools are then placed around the joined upper and lower tool inserts. The resulting assembly is covered with a breather cloth, baked in a vacuum bag and cured in an autoclave. During curing, the autoclave applies a hydrostatic pressure on the upper tool insert and thus compliant forming surface. The compliant forming surface in turn applies a consolidation and forming pressure to the composite workpiece within the tools. During curing, the compliant forming surface deforms slightly to account for thickness variations in the composite workpiece in order to produce a better quality formed composite part.
摘要翻译：具有用于形成复合部件的柔顺成形表面的加工概念。工具概念使用具有薄柔顺成形表面的刚性支撑子结构。在本发明的优选实施例中，工具概念用于形成复合正弦波形梁。工具概念的优选实施例包括上部和下部工具插入件和侧面工具插入件。上部工具插入件具有柔顺的成形表面，其位于刚性支撑子结构和用于形成复合部件的复合材料之间。复合预浸料在上下工具刀片上放置在正弦波轮廓上，形成上下U型复合工件。然后将上下工具插入件和工件组合在一起以形成正弦波I型梁。然后将半径填料施加到上复合工件和下复合工件之间的相交处，并将盖带放置在连接的复合工件的凸缘上。然后将侧面工具和端部工具放置在连接的上部和下部工具插入件周围。所得组件用通气布覆盖，在真空袋中烘烤并在高压釜中固化。在固化期间，高压釜在上部工具插入件上施加静水压力，从而在柔性成形表面上施加静水压力。柔性成形表面又对工具内的复合工件施加固结和成形压力。在固化期间，柔性成形表面略微变形以考虑复合材料工件中的厚度变化，以便产生更好质量的成形复合材料部件。

6. 发明授权

US06254812B1 Method of making a composite part using a compliant forming surface 失效
标题翻译：使用柔顺成形表面制造复合部件的方法
公开(公告)号：US06254812B1
公开(公告)日：2001-07-03
申请号：US09165857
申请日：1998-10-02
申请人： Harold M. Goodridge , Kirk D. Skaggs
发明人： Harold M. Goodridge , Kirk D. Skaggs
IPC分类号： B29C7044
CPC分类号： B29C43/021 , B29C33/303 , B29C33/405 , B29C33/42 , B29C43/12 , B29C43/3642 , B29C70/44 , B29C2043/3644 , B29C2043/3657 , B29K2105/0854 , B29L2031/003 , Y10S425/044
摘要： A tooling concept uses a compliant forming surface for forming composite parts. The tooling concept utilizes a rigid support substructure that has a thin compliant forming surface. In the preferred embodiment of the invention, the tooling concept is used to form a composite sine wave spar. A preferred embodiment of the tooling concept includes upper and lower tool inserts and side tool inserts. The upper tool insert has a compliant forming surface that is located in between a rigid support substructure and the composite material used to form the composite part. Composite prepreg is laid up over a sine wave contour on the upper and lower tool inserts to form upper and lower U-shaped composite workpieces. The upper and lower tool inserts and workpieces are then brought together to form a sine wave I-beam. Radius fillers are then applied to the intersections between the upper and lower composite workpieces and cap strips are placed over the flanges of the joined composite workpieces. Side tools and end tools are then placed around the joined upper and lower tool inserts. The resulting assembly is covered with a breather cloth, baked in a vacuum bag and cured in an autoclave. During curing, the autoclave applies a hydrostatic pressure on the upper tool insert and thus compliant forming surface. The compliant forming surface in turn applies a consolidation and forming pressure to the composite workpiece within the tools. During curing, the compliant forming surface deforms slightly to account for thickness variations in the composite workpiece in order to produce a better quality formed composite part.
摘要翻译：工具概念使用柔性成形表面来形成复合部件。工具概念使用具有薄柔顺成形表面的刚性支撑子结构。在本发明的优选实施例中，工具概念用于形成复合正弦波形梁。工具概念的优选实施例包括上部和下部工具插入件和侧面工具插入件。上部工具插入件具有柔顺的成形表面，其位于刚性支撑子结构和用于形成复合部件的复合材料之间。复合预浸料在上下工具刀片上放置在正弦波轮廓上，形成上下U型复合工件。然后将上下工具插入件和工件组合在一起以形成正弦波I型梁。然后将半径填料施加到上复合工件和下复合工件之间的相交处，并将盖带放置在连接的复合工件的凸缘上。然后将侧面工具和端部工具放置在连接的上部和下部工具插入件周围。所得组件用通气布覆盖，在真空袋中烘烤并在高压釜中固化。在固化期间，高压釜在上部工具插入件上施加静水压力，从而在柔性成形表面上施加静水压力。柔性成形表面又对工具内的复合工件施加固结和成形压力。在固化期间，柔性成形表面略微变形以考虑复合材料工件中的厚度变化，以便产生更好质量的成形复合材料部件。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式