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公开(公告)号:US20150360289A1
公开(公告)日:2015-12-17
申请号:US14740668
申请日:2015-06-16
Applicant: United Technologies Corporation
Inventor: Joe J. Liou , Michael A. Klecka , Andrzej Ernest Kuczek , Tahany Ibrahim El-Wardany , Lee A. Hoffman , Daniel V. Viens
CPC classification number: B22F3/1055 , B21H7/00 , B22D23/06 , B22F3/18 , B22F2999/00 , B23P9/02 , B23P15/00 , B33Y10/00 , C21D7/04 , C21D2221/00 , Y02P10/295 , B22F2003/166
Abstract: An additive manufacturing method for forming a component is disclosed. The method includes the steps of forming a first layer of additive material on a substrate. The first layer of additive material is deep rolled. A second layer of additive material is then formed on the first layer of additive material.
Abstract translation: 公开了一种用于形成部件的添加剂制造方法。 该方法包括在衬底上形成第一层添加剂材料的步骤。 第一层添加剂材料是深轧的。 然后在第一层添加剂材料上形成第二层添加剂材料。
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公开(公告)号:US10415419B2
公开(公告)日:2019-09-17
申请号:US15406324
申请日:2017-01-13
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Fanping Sun , Zaffir A. Chaudhry , Lee A. Hoffman , Hailing Wu , Seung Bum Kim , Michael G. McCaffrey , Joel H. Wagner
Abstract: A system for modulating turbine blade tip clearance is provided. The system may comprise an actuation control system having at least one actuator configured to modulate turbine blade tip clearance between a turbine blade tip and a blade outer air seal (BOAS). Each actuator may be coupled to the BOAS. Each actuator may comprise a solid-state motion amplification device such as a flextensional actuator. The actuators may be configured to move the BOAS in a radial direction from a first position to a second position to control tip clearance.
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公开(公告)号:US20190010823A1
公开(公告)日:2019-01-10
申请号:US15406324
申请日:2017-01-13
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Fanping Sun , Zaffir A. Chaudhry , Lee A. Hoffman , Hailing Wu , Seung Bum Kim , Michael G. McCaffrey , Joel H. Wagner
CPC classification number: F01D11/22 , F01D11/18 , F05D2240/11 , F05D2300/505
Abstract: A system for modulating turbine blade tip clearance is provided. The system may comprise an actuation control system having at least one actuator configured to modulate turbine blade tip clearance between a turbine blade tip and a blade outer air seal (BOAS). Each actuator may be coupled to the BOAS. Each actuator may comprise a solid-state motion amplification device such as a flextensional actuator. The actuators may be configured to move the BOAS in a radial direction from a first position to a second position to control tip clearance.
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