Invention Grant
- Patent Title: Modular multistage compressor system for gas turbine engines
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Application No.: US17390836Application Date: 2021-07-30
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Publication No.: US11655757B2Publication Date: 2023-05-23
- Inventor: Benjamin M. Iwrey
- Applicant: Rolls-Royce North American Technologies Inc.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee: Rolls-Royce North American Technologies Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: Barnes & Thornburg LLP
- Main IPC: F02C3/06
- IPC: F02C3/06
Abstract:
A method of assembling a gas turbine engine is disclosed herein. The method comprises providing a set of standard axial compressor stages. Each axial compressor stage included in the set of standard axial compressor stages includes a rotor having a plurality of blades configured to rotate about an axis and a stator having a plurality of stator vanes.
Public/Granted literature
- US20230032126A1 MODULAR MULTISTAGE COMPRESSOR SYSTEM FOR GAS TURBINE ENGINES Public/Granted day:2023-02-02
Information query
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