TURBINE BLADE COMPRISING A TWO-PHASE THERMAL CONTROL SYSTEM (HEAT PIPE)
FR3163106A1Pending Publication Date: 2025-12-12SAFRAN AERO BOOSTERS SA
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Patent Information
- Application Number
- FR2024005978
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2024-06-06
- Publication Date
- 2025-12-12
Abstract
BLADES COMPRISING A TWO-PHASE THERMAL CONTROL SYSTEM (HEAT PIPE) One aspect of the invention relates to a turbomachine blade (2), in particular a stator blade, the blade comprising: a leading edge (20), a trailing edge (21), an intrados surface and an extrados surface extending from the leading edge (20) to the trailing edge (21), the assembly constituting the body (23) of the blade, a tip (24) and a foot (22), the blade (2) comprising a hollow part extending from the tip (24) to the body (23), the hollow part comprising a capillary heat pipe (1) comprising a reservoir (130) and a circuit (140) extending from the tip (24) to the body (23), and a fluid in a liquid-vapor equilibrium state filling said reservoir (130) in the total absence of any other gas in said reservoir, The fluid is configured to circulate in the heat pipe (1) when temperature gradients form on the reservoir (130). Figure to be published with the abbreviation: Figure 2
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Citation Information
Patent Citations
Heat transfer system and method for turbine engine using heat pipes
EP1884625A2
Vapour cooling system for a gas turbine engine
EP1956214A2
Heat pipe temperature management system for a turbomachine
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Hybrid airfoil cooling
EP3354851A1
Heat pipe for a turbine engine
EP4095351A1