Invention Grant
US08529204B2 Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction
有权
燃气涡轮发动机具有刚性地沿轴向连接但在径向方向上柔性的鼻锥组件
- Patent Title: Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction
- Patent Title (中): 燃气涡轮发动机具有刚性地沿轴向连接但在径向方向上柔性的鼻锥组件
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Application No.: US12369809Application Date: 2009-02-12
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Publication No.: US08529204B2Publication Date: 2013-09-10
- Inventor: Adam MacGregor Bagnall
- Applicant: Adam MacGregor Bagnall
- Applicant Address: GB
- Assignee: Rolls-Royce PLC
- Current Assignee: Rolls-Royce PLC
- Current Assignee Address: GB
- Agency: McCormick, Paulding & Huber LLP
- Priority: GB0803366.4 20080226
- Main IPC: F01D25/00
- IPC: F01D25/00
Abstract:
A nose cone assembly for a gas turbine engine comprises a spinner and a plurality of circumferentially spaced mounting members for mounting the spinner on a fan hub of the gas turbine engine. Each of the mounting members is rigid in a generally axial direction and flexible in a generally radial direction.
Public/Granted literature
- US20090214354A1 NOSE CONE ASSEMBLY Public/Granted day:2009-08-27
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