公开(公告)号：WO2014175969A3

公开(公告)日：2015-01-08

申请号：PCT/US2014023949

申请日：2014-03-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WANG CHENG-ZHANG ,  GLAHN JORN A ,  CLOUD DAVID F ,  MUNSELL PETER M ,  CRAWLEY CLIFTON J JR ,  NEWMAN ROBERT ,  STEARNS MICHELLE DIANA

IPC: F01D25/24 ,  F01D25/12 ,  F02C7/12 ,  F04D29/52 ,  F04D29/58

CPC classification number: F01D25/24 ,  F01D9/041 ,  F01D9/065 ,  F01D25/162 ,  F02C7/18 ,  F05D2240/14 ,  F05D2260/14 ,  F05D2260/20 ,  F05D2260/2212 ,  F05D2260/97 ,  Y02T50/676

Abstract: A turbine engine includes a turbine section with a low pressure turbine and a turbine case disposed about an axis. A frame assembly defines an outer cavity and an inner cavity with the outer cavity including at least one opening configured and adapted to communicate cooling air to the turbine case. A transfer tube is disposed within the outer cavity and is configured and adapted to receive cooling air. The transfer tube includes a bend configured to impart circumferential velocity to the cooling air within the outer cavity.

Abstract translation: 涡轮发动机包括具有低压涡轮机的涡轮机部分和围绕轴线布置的涡轮机壳体。 框架组件限定外腔和内腔，其中外腔包括构造并适于将冷却空气与涡轮机壳连通的至少一个开口。 传送管设置在外腔内并且被配置和适于接收冷却空气。 传送管包括弯曲部，该弯曲部被配置为向外腔内的冷却空气赋予圆周速度。

公开(公告)号：FR2648865A1

公开(公告)日：1990-12-28

申请号：FR9007868

申请日：1990-06-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FRED M ,  CRAWLEY CLIFTON J JR

IPC: F01D11/24

Abstract: Flow of cooling air to a thermal clearance control system in a gas turbine engine is selectably scheduled between a normal power level versus clearance schedule and an increased efficiency cruising schedule. Selection of the cruising schedule is accompanied by a limitation on the rate of engine power increase during the period when the cruise schedule is selected.

公开(公告)号：FR2648865B1

公开(公告)日：1994-09-16

申请号：FR9007868

申请日：1990-06-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FRED M ,  CRAWLEY CLIFTON J JR

IPC: F01D11/24

Abstract: Flow of cooling air to a thermal clearance control system in a gas turbine engine is selectably scheduled between a normal power level versus clearance schedule and an increased efficiency cruising schedule. Selection of the cruising schedule is accompanied by a limitation on the rate of engine power increase during the period when the cruise schedule is selected.

公开(公告)号：FR2648867A1

公开(公告)日：1990-12-28

申请号：FR9007870

申请日：1990-06-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FRED M ,  CRAWLEY CLIFTON J JR ,  RAUSEO ANTHONY F ,  LAGUEUX KEN R

IPC: F01D11/24 ,  F02C7/28

公开(公告)号：FR2648867B1

公开(公告)日：1994-09-16

申请号：FR9007870

申请日：1990-06-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FRED M ,  CRAWLEY CLIFTON J JR ,  RAUSEO ANTHONY F ,  LAGUEUX KEN R

IPC: F01D11/24 ,  F02C7/28

公开(公告)号：FR2648864A1

公开(公告)日：1990-12-28

申请号：FR9007867

申请日：1990-06-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FRED M ,  CRAWLEY CLIFTON J JR

IPC: F01D11/24

Abstract: A method for enhancing the thermal response of the engine case and annular shroud during the transient response period following a step change in engine power provides for the temporary reduction or elimination of the flow of cooling air supplied to the engine case by the active clearance control system. An alternate method additionally substitutes a flow of relatively warm air to further increase the response of the case.

公开(公告)号：EP2971612A4

公开(公告)日：2017-01-04

申请号：EP14787748

申请日：2014-03-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： WANG CHENG-ZHANG ,  GLAHN JORN A ,  CLOUD DAVID F ,  MUNSELL PETER M ,  CRAWLEY CLIFTON J JR ,  NEWMAN ROBERT ,  STEARNS MICHELLE DIANA

IPC: F01D25/24 ,  F01D9/04 ,  F01D9/06 ,  F01D25/12 ,  F01D25/16 ,  F02C7/12 ,  F02C7/18 ,  F04D29/52 ,  F04D29/58

CPC classification number: F01D25/24 ,  F01D9/041 ,  F01D9/065 ,  F01D25/162 ,  F02C7/18 ,  F05D2240/14 ,  F05D2260/14 ,  F05D2260/20 ,  F05D2260/2212 ,  F05D2260/97 ,  Y02T50/676

Abstract: A turbine engine includes a turbine section with a low pressure turbine and a turbine case disposed about an axis. A frame assembly defines an outer cavity and an inner cavity with the outer cavity including at least one opening configured and adapted to communicate cooling air to the turbine case. A transfer tube is disposed within the outer cavity and is configured and adapted to receive cooling air. The transfer tube includes a bend configured to impart circumferential velocity to the cooling air within the outer cavity.