The boeing company (20240343418). THERMAL CONTROL SYSTEMS FOR REDUCING ICE FORMATION simplified abstract
THERMAL CONTROL SYSTEMS FOR REDUCING ICE FORMATION
Organization Name
Inventor(s)
Steven J. Adam of Orange CA (US)
Erin Bangert Voltz of Madison AL (US)
THERMAL CONTROL SYSTEMS FOR REDUCING ICE FORMATION - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240343418 titled 'THERMAL CONTROL SYSTEMS FOR REDUCING ICE FORMATION
The present disclosure describes thermal control systems for reducing ice formation in space vehicles. One example includes a fluid loop system with a perfluoropolyether heat transfer fluid and an anti-icing fluid that is immiscible with the heat transfer fluid but miscible with water to prevent ice formation.
- Fluid loop system for thermal control
- Perfluoropolyether heat transfer fluid
- Anti-icing fluid immiscible with heat transfer fluid
- Anti-icing fluid miscible with water
- Prevents ice formation in space vehicles
Potential Applications: - Space exploration vehicles - Satellites - Aircraft - Wind turbines - HVAC systems
Problems Solved: - Ice formation on critical components - Maintaining optimal thermal conditions in extreme environments
Benefits: - Improved safety and efficiency in space missions - Extended lifespan of equipment - Reduced maintenance costs
Commercial Applications: Title: Innovative Thermal Control Systems for Aerospace Industry This technology can be used in spacecraft, satellites, and other aerospace applications to ensure optimal thermal conditions and prevent ice formation in critical components.
Questions about Thermal Control Systems: 1. How does the anti-icing fluid prevent ice formation in the system? The anti-icing fluid is immiscible with the heat transfer fluid but miscible with water, creating a mixture that remains liquid at low temperatures, preventing ice formation.
2. What are the potential cost savings associated with using this thermal control system? By preventing ice formation and maintaining optimal thermal conditions, this system can reduce maintenance costs and extend the lifespan of equipment, leading to significant cost savings in the long run.
Original Abstract Submitted
the present disclosure provides examples of thermal control systems for reducing ice formation. in one example, a space vehicle comprising a first component, a second component, and a thermal control system is provided. the thermal control system is configured for transferring thermal energy between the first component and the second component. the thermal control system comprises a fluid loop in thermal communication with the first component and the second component, a heat transfer fluid including a perfluoropolyether, an anti-icing fluid, wherein the anti-icing fluid is immiscible with the heat transfer fluid and is miscible with water to form a mixture that remains liquid at temperatures under use conditions in space, and a pump for circulating the heat transfer fluid and the anti-icing fluid within the fluid loop.
