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公开(公告)号：US20160160648A1
公开(公告)日：2016-06-09
申请号：US14865132
申请日：2015-09-25
Applicant: United Technologies Corporation
Inventor： Scott D. Virkler , Daniel E. Kane
CPC classification number: F01D5/08 , F01D5/081 , F01D5/147 , F01D5/187 , F01D5/3007 , F01D5/3092 , F05D2220/32 , F05D2240/24 , F05D2240/30 , F05D2240/35 , F05D2260/202 , F05D2260/231 , F05D2260/941 , F05D2270/112 , Y02T50/672 , Y02T50/676
Abstract: A rotor assembly for a gas turbine engine includes a rotor disk. The rotor disk includes a heat barrier feature radially inward of a rotor blade and radially outward of a rotor disk.
Abstract translation: 用于燃气涡轮发动机的转子组件包括转子盘。 转子盘包括在转子叶片的径向向内并且在转子盘的径向外侧的热障特征。
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公开(公告)号：US20180347367A1
公开(公告)日：2018-12-06
申请号：US16001176
申请日：2018-06-06
Applicant: United Technologies Corporation
Inventor： Scott D. Virkler , Daniel E. Kane
CPC classification number: F01D5/08 , F01D5/081 , F01D5/147 , F01D5/187 , F01D5/3007 , F01D5/3092 , F05D2220/32 , F05D2240/24 , F05D2240/30 , F05D2240/35 , F05D2260/202 , F05D2260/231 , F05D2260/941 , F05D2270/112 , Y02T50/672 , Y02T50/676
Abstract: A rotor assembly for a gas turbine engine includes a rotor disk. The rotor disk includes a heat barrier feature radially inward of a rotor blade and radially outward of a rotor disk.
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公开(公告)号：US10107102B2
公开(公告)日：2018-10-23
申请号：US14865132
申请日：2015-09-25
Applicant: United Technologies Corporation
Inventor： Scott D. Virkler , Daniel E. Kane
Abstract: A rotor assembly for a gas turbine engine includes a rotor disk. The rotor disk includes a heat barrier feature radially inward of a rotor blade and radially outward of a rotor disk.
