Invention Grant
- Patent Title: Hybrid rotor disk assembly for a gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机的混合转子盘组件
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Application No.: US13116199Application Date: 2011-05-26
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Publication No.: US08851853B2Publication Date: 2014-10-07
- Inventor: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
- Applicant: Ioannis Alvanos , Gabriel L. Suciu , Christopher M. Dye , Glenn Levasseur
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/32
- IPC: F01D5/32 ; F01D5/28 ; F01D5/30 ; F01D5/22
Abstract:
A rotor disk assembly for a gas turbine engine includes a rotor hub defined about an axis of rotation, the rotor hub includes a blade mount section with a first radial flange having a multiple of first apertures and a second radial flange with a multiple of second apertures.
Public/Granted literature
- US20120301306A1 HYBRID ROTOR DISK ASSEMBLY FOR A GAS TURBINE ENGINE Public/Granted day:2012-11-29
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