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
Patent Text Reader

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

    EP3075953A1

  • Hybrid airfoil cooling

    EP3354851A1

  • Heat pipe for a turbine engine

    EP4095351A1