Invention Publication
- Patent Title: COMPRESSOR FOR AN ENGINE
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Application No.: US18345319Application Date: 2023-06-30
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Publication No.: US20240003353A1Publication Date: 2024-01-04
- Inventor: Sergio Elorza Gomez , Werner Humhauser , Roland Matzgeller
- Applicant: MTU Aero Engines AG
- Applicant Address: DE München
- Assignee: MTU Aero Engines AG
- Current Assignee: MTU Aero Engines AG
- Current Assignee Address: DE München
- Priority: DE 2022116667.8 2022.07.04
- Main IPC: F04D19/02
- IPC: F04D19/02 ; F02C3/06
Abstract:
The invention relates to a compressor for an engine, wherein the compressor has compressor stages arranged in succession in a flow direction of the compressor and each compressor stage has a rotating blade cascade and a guide vane cascade arranged downstream of the rotating blade cascade and the rotating blade cascade and the guide vane cascade each have an aspect ratio.
Public/Granted literature
- US12123419B2 Compressor for an engine Public/Granted day:2024-10-22
Information query
