公开(公告)号：US20160252248A1

公开(公告)日：2016-09-01

申请号：US14568896

申请日：2014-12-12

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Jose E. Ruberte Sanchez ,  Timothy J. McAlice ,  Kevin L. Rugg

IPC: F23R3/00 ,  F02K1/82

CPC classification number: F23R3/002 ,  F02K1/822 ,  F23M5/04 ,  F23M2900/05004 ,  F23R3/007 ,  F23R3/60 ,  Y02T50/675

Abstract: One exemplary embodiment of this disclosure relates to a gas turbine engine. The engine includes a first attachment member including an opening, a second attachment member including a loop at least partially extending through the opening, and a pin between the first attachment member and the loop.

Abstract translation: 本公开的一个示例性实施例涉及燃气涡轮发动机。 发动机包括包括开口的第一附接构件，包括至少部分地延伸穿过开口的环的第二附接构件以及第一附接构件和环之间的销。

公开(公告)号：US20180080373A1

公开(公告)日：2018-03-22

申请号：US15268713

申请日：2016-09-19

Applicant: United Technologies Corporation

Inventor： Daniel Bernard Kupratis ,  Tania Bhatia Kashyap ,  Mark F. Zelesky ,  Arthur W. Utay ,  Gabriel L. Suciu ,  Thomas N. Slavens ,  Kevin L. Rugg ,  Brian Merry

IPC: F02C3/107 ,  F02C3/14

CPC classification number: F02C3/107 ,  F02C3/145 ,  F02C7/04 ,  F05D2240/40 ,  F05D2250/30

Abstract: A turbine engine includes a first compressor and a second compressor fluidly parallel to the first compressor. A reverse flow combustor is fluidly connected to the first compressor and the second compressor. A first turbine and a second turbine are fluidly connected in series, and fluidly connected to an output of the reverse flow combustor.

公开(公告)号：US09664389B2

公开(公告)日：2017-05-30

申请号：US14568896

申请日：2014-12-12

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Jose E. Ruberte Sanchez ,  Timothy J. McAlice ,  Kevin L. Rugg

IPC: F23R3/00 ,  F02K1/82 ,  F23M5/04 ,  F23R3/60

CPC classification number: F23R3/002 ,  F02K1/822 ,  F23M5/04 ,  F23M2900/05004 ,  F23R3/007 ,  F23R3/60 ,  Y02T50/675

Abstract: One exemplary embodiment of this disclosure relates to a gas turbine engine. The engine includes a first attachment member including an opening, a second attachment member including a loop at least partially extending through the opening, and a pin between the first attachment member and the loop.

公开(公告)号：US20160160658A1

公开(公告)日：2016-06-09

申请号：US14905345

申请日：2014-07-01

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Michael G. McCaffrey ,  Greg C. Ojard ,  Kevin L. Rugg

IPC: F01D5/28 ,  F01D5/14 ,  F04D29/38 ,  F01D9/04

CPC classification number: F01D5/282 ,  F01D5/147 ,  F01D9/041 ,  F04D29/388 ,  F05D2220/32 ,  F05D2230/20 ,  F05D2230/60 ,  F05D2300/501 ,  F05D2300/6012 ,  F05D2300/6033 ,  F05D2300/6034 ,  F05D2300/614 ,  Y02T50/672 ,  Y02T50/673

Abstract: An airfoil includes a core with a first Young's Modulus; and an outer section at least partially surrounding the core with a second Young's Modulus, wherein the first Young's Modulus is higher than the second Young's Modulus.

Abstract translation: 机翼包括具有第一杨氏模量的芯; 以及至少部分地围绕所述芯的第二杨氏模量的外部部分，其中所述第一杨氏模量高于所述第二杨氏模量。