Measurement acquisition device with a sliding attack section on a support
Patent Information
- Application Number
- FR2024004859
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2024-05-13
- Publication Date
- 2025-11-14
- Estimated Expiration
- 2044-05-13
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Abstract
Claims
slide being formed by the groove delimited by the trailing part and the support rail (2).
12. Measurement acquisition device (1) according to any one of claims 9 to 11, • the attacking part (3) has an external surface (31), • the trailing part (4) has a second external surface (41) which extends tangentially from the external surface (31).
13. Device (1) for acquiring measurements according to any one of claims 9 to 12, • the sliding link allows a translation of the attacking part (3) relative to the support (2) in a direction of translation, • in a transverse plane which is orthogonal to the direction of translation, the attacking part (3) and the trailing part (4) completely cover the support (2).
14. Assembly comprising: • A test bench for turbomachine (10), • a measurement acquisition device (1) according to any one of the preceding claims, the measurement acquisition device (1) being fixed to the test bench for turbomachine (10) such that the driving part (5) faces a flow of gas circulating in the test bench for turbomachine (10).
15. A method using a measurement acquisition device (1) according to any one of claims 1 to 13 or an assembly according to claim 14, the method comprising: • detaching the attacking part (3) from the support (2) by translating the attacking part (3) relative to the support (2) via the sliding link, • attaching another attacking part to the support (2) by translating the other attacking part relative to the support (2) via the sliding link, wherein the other attacking part is different from the attacking part (3). [Fig. 1]
Citation Information
Patent Citations
device FOR MEASURING AERODYNAMIC QUANTITIES INTENDED TO BE PLACED IN A FLOW STREAM OF A TURBOMACHINE
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Device for measuring aerodynamic quantities intended for being placed in a flow section of a turbine engine
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DEVICE FOR MEASURING PARAMETERS OF A PRESTRAINED AERODYNAMIC FLOW, TURBOMACHINE VEIN FOR SUCH A MEASURING DEVICE AND METHOD FOR ASSEMBLING SUCH A MEASURING DEVICE
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Device for measuring aerodynamic magnitudes intended to be placed in a flow passage of a turbine engine
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