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公开(公告)号:US20170292399A1
公开(公告)日:2017-10-12
申请号:US15096346
申请日:2016-04-12
Applicant: United Technologies Corporation
Inventor: Graham R. Philbrick , Patrick D. Couture , Jason Arnold
CPC classification number: F01D17/145 , B64D27/10 , F01D5/02 , F01D11/24 , F01D25/24 , F05D2220/323 , F05D2270/114 , F05D2270/20 , F05D2270/303 , F05D2270/304 , F05D2270/305 , F05D2270/309 , F05D2270/335 , F05D2270/44
Abstract: Aspects of the disclosure are directed to systems and methods for receiving operating state parameters associated with an operative state of an aircraft, determining a clearance value between a first structure of the engine and a second structure of the engine, where the clearance value is determined based on the operating state parameters and a passive clearance model that includes a specification of an uncertainty in the clearance value, determining that the clearance value deviates from a clearance target in an amount that is greater than a threshold, and engaging an active clearance control (ACC) mechanism based on the deviation.
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公开(公告)号:US20140079537A1
公开(公告)日:2014-03-20
申请号:US13622652
申请日:2012-09-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Jason Arnold
CPC classification number: F01D5/027 , F05D2260/30 , F16F15/322 , F16F15/34 , Y10T74/2132
Abstract: A ring has a ring body with a central portion surrounding an axis and extending to first and second opposing ends separated by a split. The central portion has a first axial thickness. At least one retaining feature is formed on the ring body, the at least one retaining feature having a second axial thickness greater than the first axial thickness. An assembly and a gas turbine engine are also disclosed.
Abstract translation: 环具有环体,其具有围绕轴线的中心部分并且延伸到由分开分开的第一和第二相对端部。 中心部分具有第一轴向厚度。 至少一个保持特征形成在环体上,所述至少一个保持特征具有大于第一轴向厚度的第二轴向厚度。 还公开了一种组件和燃气涡轮发动机。
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