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公开(公告)号:US11753951B2
公开(公告)日:2023-09-12
申请号:US17380397
申请日:2021-07-20
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Jason Husband , James Glaspey , Aaron John Pepin
CPC classification number: F01D5/3053 , F01D5/02 , F01D5/147 , F01D5/282 , F01D5/3038 , F01D11/008 , F05D2240/301 , F05D2240/80 , F05D2260/30 , F05D2260/31 , F05D2300/603 , F05D2300/702
Abstract: A rotor assembly for a gas turbine engine includes a rotatable hub that has a main body and an array of annular flanges that extend about an outer periphery of the main body to define an array of annular channels. An array of airfoils are circumferentially distributed about the outer periphery. Each one of the airfoils includes an airfoil section extending from a root section received in the annular channels. Retention pins extend through the root section of a respective one of the airfoils and through the array of annular flanges to mechanically attach each root section to the hub.
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公开(公告)号:US20210348515A1
公开(公告)日:2021-11-11
申请号:US17380397
申请日:2021-07-20
Applicant: RAYTHEON TECHNOLOGIES CORPORATION
Inventor: Jason Husband , James Glaspey , Aaron John Pepin
Abstract: A rotor assembly for a gas turbine engine includes a rotatable hub that has a main body and an array of annular flanges that extend about an outer periphery of the main body to define an array of annular channels. An array of airfoils are circumferentially distributed about the outer periphery. Each one of the airfoils includes an airfoil section extending from a root section received in the annular channels. Retention pins extend through the root section of a respective one of the airfoils and through the array of annular flanges to mechanically attach each root section to the hub.
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