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Patent Agency Ranking
公开(公告)号：US10968763B2
公开(公告)日：2021-04-06
申请号：US16265664
申请日：2019-02-01
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Scott D. Virkler
Abstract: A method for assembling a seal arrangement may comprise applying an adhesive to a seal, applying a force to a shoe of the seal, and removing the force from the shoe, wherein the adhesive secures the shoe with respect to a static structure in response to the force being removed.
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公开(公告)号：US10364696B2
公开(公告)日：2019-07-30
申请号：US15151274
申请日：2016-05-10
Applicant: United Technologies Corporation
Inventor： Scott D. Virkler
Abstract: A clearance control assembly for providing clearance control between a blade outer air seal and an airfoil tip of a gas turbine engine includes an outer case, a first blade outer air seal carrier, a blade outer air seal, an actuator, a load-applying member, and a lever. The first blade outer air seal carrier is positioned radially inward of the outer case. The blade outer air seal is positioned radially inward of and mounted to the blade outer air seal carrier. The load-applying member is positioned to be acted upon by the actuator during operation of the actuator. The lever is connected to the case and is operably in contact with the load-applying member and the first blade outer air seal carrier.
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公开(公告)号：US20170328230A1
公开(公告)日：2017-11-16
申请号：US15151274
申请日：2016-05-10
Applicant: United Technologies Corporation
Inventor： Scott D. Virkler
CPC classification number: F01D11/22 , F01D21/003 , F01D25/24 , F04D27/001 , F04D29/164 , F04D29/526 , F05D2220/32 , F05D2240/30 , F05D2260/30 , F05D2260/56
Abstract: A clearance control assembly for providing clearance control between a blade outer air seal and an airfoil tip of a gas turbine engine includes an outer case, a first blade outer air seal carrier, a blade outer air seal, an actuator, a load-applying member, and a lever. The first blade outer air seal carrier is positioned radially inward of the outer case. The blade outer air seal is positioned radially inward of and mounted to the blade outer air seal carrier. The load-applying member is positioned to be acted upon by the actuator during operation of the actuator. The lever is connected to the case and is operably in contact with the load-applying member and the first blade outer air seal carrier.
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公开(公告)号：US09126294B2
公开(公告)日：2015-09-08
申请号：US14302139
申请日：2014-06-11
Applicant: United Technologies Corporation
Inventor： Scott D. Virkler , Matthew P. Ricker , Gordon Kinkade
CPC classification number: B23P19/04 , B25B27/20 , F01D5/066 , F01D25/285 , Y10T29/49824 , Y10T29/4987 , Y10T29/49947 , Y10T29/5363 , Y10T29/53657 , Y10T29/53983
Abstract: An apparatus includes a body, a driver, a plurality of shafts, and a plurality of arms. The body is configured for insertion into a component and the driver is adapted for movement relative to the body. The plurality of shafts extend through the body and are connected to the plurality of arms. The tool is configured such that contact by the driver against the shaft rotates the plurality of shafts to pivot the plurality of arms.
Abstract translation: 一种装置包括主体，驱动器，多个轴和多个臂。 主体被配置为插入到部件中，并且驱动器适于相对于主体移动。 多个轴延伸穿过主体并连接到多个臂。 该工具被构造成使得驾驶员抵靠轴的接触使多个轴旋转以枢转多个臂。
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公开(公告)号：US20140109548A1
公开(公告)日：2014-04-24
申请号：US13713257
申请日：2012-12-13
Applicant: United Technologies Corporation
Inventor： Scott D. Virkler
CPC classification number: F01D5/02 , F01D5/3007 , F05D2240/24 , Y10T29/49321
Abstract: A rotor disk for a gas turbine engine is disclosed and formed to enable operation at high rotational speeds in a high temperature environment. The rotor disk is formed to include a bore, a live rim diameter and an outer diameter related to each other according to defined relationships.
Abstract translation: 公开了一种用于燃气涡轮发动机的转子盘，用于在高温环境中以高转速进行操作。 根据规定的关系，转子盘形成为包括孔，活圈直径和彼此相关的外径。
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