-
公开(公告)号:US20160298472A1
公开(公告)日:2016-10-13
申请号:US14685118
申请日:2015-04-13
Applicant: United Technologies Corporation
Inventor: Anthony P. Cherolis , Alexander Broulidakis , Matthew A. Hough , Jonathan Lemoine , Christopher Treat
CPC classification number: F16L55/00 , F01D9/065 , F05D2240/58 , F05D2300/43 , F16L21/035
Abstract: Aspects of the disclosure are directed to a tube of an engine of an aircraft configured to transfer a fluid, a boss of the engine, and a shim coupled to at least one of the tube and the boss that is configured to maintain a gap between the tube and the boss when the engine is assembled.
Abstract translation: 本公开的方面针对被配置为传送流体,发动机的凸台和联接到管和凸起中的至少一个的垫片的飞行器的发动机的管,所述垫被配置为保持间隙 管和发动机组装时的老板。
-
公开(公告)号:US20160230598A1
公开(公告)日:2016-08-11
申请号:US14617506
申请日:2015-02-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Anthony P. Cherolis , Jeffrey J. Lienau , Robert Newman , John H. Mosley , Joshua Daniel Winn , Paul K. Sanchez
CPC classification number: F01D25/14 , F01D9/065 , F01D25/12 , F01D25/162 , F01D25/24 , F02C7/12 , F05D2220/32 , F05D2220/3213 , F05D2260/20 , F05D2260/31 , Y02T50/676
Abstract: A mid-turbine frame assembly includes an inner frame case which includes a first plurality of holes and a second plurality of holes. A plurality of tie rods is circumferentially spaced around the inner frame case and includes an inlet passage that is aligned with the first plurality of holes. A plurality of hollow airfoils is aligned with the second plurality of holes.
Abstract translation: 中间涡轮机框架组件包括内框架壳体,其包括第一多个孔和第二多个孔。 多个拉杆围绕内框架周向隔开并包括与第一多个孔对准的入口通道。 多个中空翼型件与第二多个孔对准。
-
公开(公告)号:US20160222827A1
公开(公告)日:2016-08-04
申请号:US14612469
申请日:2015-02-03
Applicant: United Technologies Corporation
Inventor: Joshua Daniel Winn , Alexander Broulidakis , Paul K. Sanchez , Anthony P. Cherolis , Joseph J. Sedor , Christopher Treat
CPC classification number: F01D25/28 , F01D5/02 , F01D9/065 , F01D25/12 , F01D25/162 , F01D25/26 , F02C7/12 , F05D2220/32 , F05D2220/3213 , F05D2240/24 , F05D2260/20 , F05D2260/31 , Y02T50/676
Abstract: A fastener assembly includes a first component that includes a bushing opening. A second component includes a fastener opening. A threaded bushing is at least partially located within the bushing opening. A fastener extends through the fastener opening and engages the bushing.
Abstract translation: 紧固件组件包括包括衬套开口的第一部件。 第二部件包括紧固件开口。 螺纹衬套至少部分地位于衬套开口内。 紧固件延伸穿过紧固件开口并接合衬套。
-
-