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公开(公告)号：WO2015102949A3
公开(公告)日：2015-09-11
申请号：PCT/US2014071503
申请日：2014-12-19
Applicant: UNITED TECHNOLOGIES CORP
Inventor： BLANEY KEN F , HAYFORD RICHARD K , JAROCHYM CHRISTOPHER M
IPC: F01D11/22
CPC classification number: F01D11/20 , F01D5/12 , F01D11/22 , F01D25/24 , F05D2240/11 , F05D2270/64 , F05D2270/65
Abstract: An example active clearance control system for a gas turbine engine includes an actuator, and a case wall portion defining an aperture configured to receive the actuator. The actuator is configured to move an air seal segment, and the actuator is insertable to an installed position within the aperture through a radially outer side of the case wall portion.
Abstract translation: 用于燃气涡轮发动机的示例主动间隙控制系统包括致动器和限定配置成接收致动器的孔的壳体壁部分。 致动器构造成移动气密段，并且致动器可通过壳体壁部分的径向外侧插入孔内的安装位置。
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2.发明申请
公开(公告)号：WO2015020708A3
公开(公告)日：2015-04-02
申请号：PCT/US2014037420
申请日：2014-05-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： BLANEY KEN F , JAROCHYM CHRISTOPHER M
CPC classification number: F01D11/20 , F01D5/02 , F01D5/12 , F01D11/22 , F01D25/246 , F04D27/002 , F04D29/164 , F04D29/324 , F05D2220/32 , F05D2240/11 , F05D2250/232 , F05D2260/56 , F05D2260/57 , F05D2270/64 , F05D2270/65
Abstract: An active clearance control system for a gas turbine engine includes an annular piston with a multiple of piston lift lugs. A method of active blade tip clearance control for a gas turbine engine includes translating axial movement of an annular piston to radial movement of a multiple of blade outer air seal segments.
Abstract translation: 用于燃气涡轮发动机的主动间隙控制系统包括具有多个活塞升程凸耳的环形活塞。 一种用于燃气涡轮发动机的主动叶片尖端间隙控制的方法包括将环形活塞的轴向运动转换成多个叶片外部气密部分的径向运动。
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3.发明公开
公开(公告)号：EP3019707A4
公开(公告)日：2016-08-10
申请号：EP14835039
申请日：2014-05-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： BLANEY KEN F , JAROCHYM CHRISTOPHER M
IPC: F01D11/22
CPC classification number: F01D11/20 , F01D5/02 , F01D5/12 , F01D11/22 , F01D25/246 , F04D27/002 , F04D29/164 , F04D29/324 , F05D2220/32 , F05D2240/11 , F05D2250/232 , F05D2260/56 , F05D2260/57 , F05D2270/64 , F05D2270/65
Abstract: An active clearance control system for a gas turbine engine includes an annular piston with a multiple of piston lift lugs. A method of active blade tip clearance control for a gas turbine engine includes translating axial movement of an annular piston to radial movement of a multiple of blade outer air seal segments.
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4.发明公开ACCESSIBLE RAPID RESPONSE CLEARANCE CONTROL SYSTEM 审中-公开ZUGÄNGLICHESSCHNELL REAGIERENDES ABSTANDSKONTROLLSYSTEM
公开(公告)号：EP3097274A4
公开(公告)日：2017-10-04
申请号：EP14876467
申请日：2014-12-19
Applicant: UNITED TECHNOLOGIES CORP
Inventor： BLANEY KEN F , HAYFORD RICHARD K , JAROCHYM CHRISTOPHER M
IPC: F01D11/22
CPC classification number: F01D11/20 , F01D5/12 , F01D11/22 , F01D25/24 , F05D2240/11 , F05D2270/64 , F05D2270/65
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