公开(公告)号：US5722813A

公开(公告)日：1998-03-03

申请号：US739478

申请日：1996-10-28

申请人： Pei-Ching Li ,  Bruce D. Reynolds ,  Theodore Westerman

发明人： Pei-Ching Li ,  Bruce D. Reynolds ,  Theodore Westerman

IPC分类号： F04D29/08 ,  F04D29/44

CPC分类号： F04D29/083 ,  F04D29/444 ,  F05D2250/52

摘要： The present invention provides a self-sealing segmented deswirl molded from an organic matrix composite. Each deswirl segment is comprised of a length of outer shroud, an integral mounting flange extending radially outward from the shroud, and several integral deswirl vanes extending radially inward from the shroud. A means for sealing between segments is provided at the circumferential ends of the mounting flange. The sealing means includes an integral flexible sealing member extending from one end of the mounting flange, and a mating slot for sealingly receiving the sealing member at the other end of the mounting flange.

摘要翻译： 本发明提供了由有机基质复合材料模制的自密封分段脱模。 每个旋转部分由一长度的外护罩组成，一个从护罩径向向外延伸的整体式安装凸缘以及从护罩径向向内延伸的几个整体的旋转叶片。 在安装凸缘的周向端部设置有用于在段之间进行密封的装置。 密封装置包括从安装凸缘的一端延伸的整体的柔性密封构件和用于在安装凸缘的另一端处密封地接收密封构件的配合槽。

公开(公告)号：US5525035A

公开(公告)日：1996-06-11

申请号：US326092

申请日：1994-10-19

申请人： Avi Ben-Porat ,  George Milo ,  Walter Smith ,  Theodore Westerman

发明人： Avi Ben-Porat ,  George Milo ,  Walter Smith ,  Theodore Westerman

IPC分类号： B29C67/00 ,  B29C70/34 ,  B29D22/00 ,  F01D1/02

CPC分类号： D04C3/48 ,  B29C67/0014 ,  B29C70/345 ,  B29C70/462 ,  B29C70/48 ,  B29D22/00 ,  D04C1/06 ,  F01D9/02 ,  F02C7/04 ,  B29C70/86 ,  B29K2105/06 ,  B29L2024/00 ,  B29L2031/7504 ,  D10B2505/02 ,  F05D2220/32 ,  F05D2250/51 ,  F05D2300/603 ,  F05D2300/614 ,  Y10T29/49321

摘要： An integral structure comprised of inner and outer coaxial shells mutually supported so as to define an annular passageway between the shells. The integral structure may be an air inlet housing for a gas turbine engine and the inner shell may be a hub member having a generally cylindrical passage extending therethrough for rotatably receiving a drive shaft. The inner shell has an outer surface of revolution. A plurality of duct preforms each include an inner duct surface shaped to congruently mate with said outer surface of said inner member, an outer duct surface spaced from said inner duct surface, and first and second lateral walls having opposed lateral surfaces. The duct member preforms are mounted onto the outer surface of the inner member in side-by-side relationship such that the first and second lateral walls on adjacent pairs of duct member preforms are coextensive and engaged. A coaxial outer shell preform is spaced from the inner member. Resin on the duct member preforms and the outer shell preform is cured to form an integral structure comprised of the inner member and outer shell member and a plurality of circumferentially spaced strut members defined by the first and second lateral walls.

摘要翻译： 内部和外部同轴壳体的一体结构相互支撑，以便在壳体之间限定一个环形通道。 一体结构可以是用于燃气涡轮发动机的空气入口壳体，并且内壳可以是具有延伸穿过其中的大致圆柱形通道的轮毂构件，以可旋转地接收驱动轴。 内壳具有外表面的旋转。 多个管道预成型件各自包括成形为与所述内部构件的所述外表面一体配合的内部管道表面，与所述内部管道表面间隔开的外部管道表面，以及具有相对侧面的第一和第二侧壁。 管道构件预成型件以并排关系安装在内部构件的外表面上，使得相邻的管道构件预制件对上的第一和第二侧壁共同延伸并接合。 同轴外壳预制件与内部构件间隔开。 管道构件预制件和外壳预制件上的树脂被固化以形成由内构件和外壳构件组成的整体结构以及由第一和第二侧壁限定的多个周向间隔的支柱构件。

公开(公告)号：US5362344A

公开(公告)日：1994-11-08

申请号：US12581

申请日：1993-02-03

申请人： Avi Ben-Porat ,  George Milo ,  Walter Smith ,  Theodore Westerman

发明人： Avi Ben-Porat ,  George Milo ,  Walter Smith ,  Theodore Westerman

IPC分类号： B29C67/00 ,  B29C70/34 ,  B29D22/00 ,  B32B5/08 ,  B65H81/02 ,  F01D5/14

CPC分类号： D04C3/48 ,  B29C67/0014 ,  B29C70/345 ,  B29C70/462 ,  B29C70/48 ,  B29D22/00 ,  D04C1/06 ,  F01D9/02 ,  F02C7/04 ,  B29C70/86 ,  B29K2105/06 ,  B29L2024/00 ,  B29L2031/7504 ,  D10B2505/02 ,  F05D2220/32 ,  F05D2250/51 ,  F05D2300/603 ,  F05D2300/614 ,  Y10T29/49321

摘要： A method is disclosed of making an integral structure comprised of inner and outer coaxial shells mutually supported so as to define an annular passageway between the shells. The integral structure may be an air inlet housing for a gas turbine engine and the inner shell may be a hub member having a generally cylindrical passage extending therethrough for rotatably receiving a drive shaft. The inner shell is formed by braiding on a shaped mandrel a plurality of fibers such as fiberglass, boron, carbon, or the like, to form an inner shell preform having an outer surface of revolution. A plurality of duct preforms are similarly formed on a conical mandrel, then removed, and administered onto an outer peripheral surface of a duct mold so as to define a modified shape. The modified duct preforms are then positioned onto the outer surface of the inner shell preform in side-by-side relationship such that the first and second lateral surfaces on adjacent modified duct preforms are coextensive and engaged, the plurality of modified duct preforms completely circumscribing the inner shell preform. Then, a plurality of fibers are braided across the plurality of outer modified duct surfaces of the duct preforms to form an outer shell preform spaced from and coaxial with the inner shell preform. Thereafter, resin is applied to the structure to encapsulate the braided inner shell preform, the braided modified duct preforms, and the braided outer shell preform. The resin is then cured to thereby complete fabrication of the integral structure.

摘要翻译： 公开了一种制造整体结构的方法，所述整体结构包括相互支撑的内部和外部同轴壳体，以便在壳体之间限定环形通道。 一体结构可以是用于燃气涡轮发动机的空气入口壳体，并且内壳可以是具有延伸穿过其中的大致圆柱形通道的轮毂构件，以可旋转地接收驱动轴。 内壳通过在成形的心轴上编织多个纤维如玻璃纤维，硼，碳等形成，以形成具有外表面旋转的内壳预制件。 多个管道预成型件类似地形成在锥形心轴上，然后移除，并且施加到管道模具的外周表面上以限定修改形状。 经修改的管道预成型件然后以并排关系定位在内壳预制件的外表面上，使得相邻改进的管道预成型件上的第一和第二侧表面共同延伸并接合，多个经修改的管道预成型件完全限定 内壳预制件。 然后，多个纤维被编织在管道预成型件的多个外部修改的管道表面上，以形成与内壳预制件间隔开并与内壳预制件同轴的外壳预制件。 此后，将树脂施加到结构上以封装编织的内壳预制件，编织的经修改的管道预制件和编织的外壳预制件。 然后固化树脂，从而完成整体结构的制造。