公开(公告)号：WO2015099869A3

公开(公告)日：2015-09-24

申请号：PCT/US2014061333

申请日：2014-10-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TEIXEIRA JOHN D ,  GROVER ERIC A ,  SURACE RAYMOND

IPC: F01D9/02 ,  F01D17/16

CPC classification number: F01D17/162 ,  F01D5/143 ,  F05D2250/241 ,  F05D2250/711 ,  F05D2250/712 ,  Y02T50/673

Abstract: A gas turbine engine component includes an outer diameter endwall, an inner diameter endwall spaced radially inward of the outer diameter endwall, and at least one body supported between the outer and inner endwalls for rotation about an axis. The body includes an outer diameter surface spaced from the outer diameter endwall by a first gap and an inner diameter surface spaced from the inner diameter endwall by a second gap. The outer and inner diameter surfaces and the outer and inner diameter endwalls are configured such that the first and second gaps remain generally constant in size as the body rotates about the axis.

Abstract translation: 燃气涡轮发动机部件包括外径端壁，在外径端壁径向向内间隔开的内径端壁以及支撑在外端壁和内端壁之间用于围绕轴线旋转的至少一个主体。 所述主体包括外径表面，所述外径表面与所述外径端壁间隔开第一间隙和与所述内径端壁间隔第二间隙的内径表面。 外径和内径表面以及外径和内径端壁被构造成使得当主体围绕轴线旋转时第一和第二间隙的尺寸通常保持恒定。

公开(公告)号：WO2015108606A3

公开(公告)日：2015-10-08

申请号：PCT/US2014063647

申请日：2014-11-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TEIXEIRA JOHN D ,  SLAVENS THOMAS N ,  SURACE RAYMOND

IPC: F01D25/12 ,  F01D5/18 ,  F01D9/02

CPC classification number: F01D17/162 ,  F01D5/186 ,  F01D9/041 ,  F01D9/065 ,  F01D25/12 ,  F04D29/056 ,  F04D29/563 ,  F04D29/582 ,  F05D2220/32 ,  F05D2240/50 ,  F05D2260/20

Abstract: A gas turbine engine with an adjustable vane includes a platform with a hole and an aperture. A vane is supported for rotation relative to the platform by a trunion that is received in the hole. The vane has an opening that is laterally spaced from the trunion and is in alignment with the aperture. The vane includes an airfoil with a cooling passage in fluid communication with the opening.

Abstract translation: 具有可调叶片的燃气涡轮发动机包括具有孔和孔的平台。 一个叶片被支撑，以便通过接收在孔中的密封圈相对于平台旋转。 叶片有一个开口，与开口横向隔开并与开口对齐。 叶片包括具有与开口流体连通的冷却通道的翼型件。

公开(公告)号：EP3071796A4

公开(公告)日：2016-12-07

申请号：EP14875854

申请日：2014-10-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TEIXEIRA JOHN D ,  GROVER ERIC A ,  SURACE RAYMOND

IPC: F01D5/14 ,  F01D17/16

CPC classification number: F01D17/162 ,  F01D5/143 ,  F05D2250/241 ,  F05D2250/711 ,  F05D2250/712 ,  Y02T50/673

公开(公告)号：EP3090146A4

公开(公告)日：2017-10-18

申请号：EP14878556

申请日：2014-11-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： TEIXEIRA JOHN D ,  SLAVENS THOMAS N ,  SURACE RAYMOND

IPC: F01D25/12 ,  F01D5/18 ,  F01D9/02 ,  F01D9/04 ,  F01D9/06 ,  F01D17/16

CPC classification number: F01D17/162 ,  F01D5/186 ,  F01D9/041 ,  F01D9/065 ,  F01D25/12 ,  F04D29/056 ,  F04D29/563 ,  F04D29/582 ,  F05D2220/32 ,  F05D2240/50 ,  F05D2260/20

Abstract: A gas turbine engine with an adjustable vane includes a platform with a hole and an aperture. A vane is supported for rotation relative to the platform by a trunion that is received in the hole. The vane has an opening that is laterally spaced from the trunion and is in alignment with the aperture. The vane includes an airfoil with a cooling passage in fluid communication with the opening.

公开(公告)号：EP3068977A4

公开(公告)日：2016-12-28

申请号：EP14862100

申请日：2014-11-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SLAVENS THOMAS N ,  GROVER ERIC A ,  TEIXEIRA JOHN D

IPC: F01D9/02 ,  F01D5/02 ,  F01D5/12 ,  F01D5/14 ,  F01D9/04 ,  F01D9/06 ,  F01D17/14 ,  F01D17/16 ,  F01D25/12 ,  F02C3/04 ,  F02C7/18

CPC classification number: F01D25/12 ,  F01D5/02 ,  F01D5/12 ,  F01D5/141 ,  F01D9/04 ,  F01D9/041 ,  F01D9/065 ,  F01D17/14 ,  F01D17/16 ,  F01D17/162 ,  F02C3/04 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2260/20

Abstract: A turbine stator vane assembly for a gas turbine engine is disclosed and includes an airfoil rotatable about an axis transverse to an engine longitudinal axis. The airfoil includes outer walls defining an inner chamber between a pressure side and a suction side of the airfoil. At least one spindle supports rotation of the airfoil and includes a feed opening for communicating cooling air into the inner chamber. An inlet defines a passage between the feed opening and the inner chamber and includes a protrusion of the outer wall on at least one of the pressure side and suction side of the airfoil.

Abstract translation: 公开了一种用于燃气涡轮发动机的涡轮机定子叶片组件，并且包括可围绕横向于发动机纵向轴线的轴线旋转的翼型件。 机翼包括限定在翼型的压力侧和吸力侧之间的内室的外壁。 至少一个主轴支撑翼型件的旋转并且包括用于将冷却空气连通到内部腔室中的进给口。 入口限定在进料口和内室之间的通道，并且在翼型的压力侧和吸力侧中的至少一个上包括外壁的突出部。