Assembly consisting of at least one aircraft turbine engine and inertial measurement unit, and related methods
CN121359092APending Publication Date: 2026-01-16SAFRAN AIRCRAFT ENGINES SAS
Patent Information
- Application Number
- CN202480041010.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Priority Date
- 2023-06-22
- Filing Date
- 2024-06-10
- Publication Date
- 2026-01-16
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Figure CN121359092A_ABST
Abstract
The invention relates to an assembly comprising at least one turbine engine (2) for an aircraft, comprising a casing in which at least one rotating body is mounted to allow propulsion of the aircraft, in which an air flow flows from upstream to downstream in the turbine engine (2), at least one inertial measurement unit (3) mounted in the turbine engine (2), the inertial measurement unit (3) is configured to measure at least one turbine engine load applied to the turbine engine during flight of the aircraft, and at least one computer configured to determine at least one fault of the turbine engine (2) based on the turbine engine load.
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Citation Information
Patent Citations
System and method for measuring fatigue for mechanical components of an aircraft and aircraft maintenance method
EP2502047B1
Method and system for monitoring equipment
US20170092021A1