17934194. NON-CONTACT THERMAL RADIATION SHIELD INTERFACE simplified abstract (International Business Machines Corporation)
Contents
- 1 NON-CONTACT THERMAL RADIATION SHIELD INTERFACE
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 NON-CONTACT THERMAL RADIATION SHIELD INTERFACE - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Original Abstract Submitted
NON-CONTACT THERMAL RADIATION SHIELD INTERFACE
Organization Name
International Business Machines Corporation
Inventor(s)
Nicholas A. Masluk of Putnam Valley NY (US)
NON-CONTACT THERMAL RADIATION SHIELD INTERFACE - A simplified explanation of the abstract
This abstract first appeared for US patent application 17934194 titled 'NON-CONTACT THERMAL RADIATION SHIELD INTERFACE
Simplified Explanation
The thermal radiation shield interface for cryogenic systems described in the patent application consists of two elements with flanges at their distal, free ends that are positioned in an interleaved arrangement to cover an opening between them, shielding it from radiation leakage.
- The interface includes a first element with flanges at its distal end.
- A second element also has flanges at its distal end.
- The flanges of both elements are positioned in an interleaved arrangement to cover an opening between them.
Potential Applications
The technology can be applied in:
- Cryogenic systems
- Spacecraft
- Aerospace industry
Problems Solved
This innovation addresses:
- Radiation leakage in cryogenic systems
- Heat transfer issues in spacecraft
- Efficiency of thermal management in aerospace applications
Benefits
The benefits of this technology include:
- Improved thermal insulation
- Enhanced system performance
- Reduced energy consumption
Potential Commercial Applications
This technology could be used in:
- Cryogenic storage facilities
- Satellite systems
- Thermal control systems in aircraft
Possible Prior Art
One possible prior art could be:
- Existing thermal insulation techniques in cryogenic systems
Unanswered Questions
How does this technology compare to traditional thermal insulation methods in terms of cost-effectiveness?
This article does not provide a direct comparison between the new technology and traditional methods in terms of cost-effectiveness. Further research or analysis would be needed to determine the cost-effectiveness of this innovation compared to existing solutions.
What are the environmental impacts of implementing this technology in aerospace applications?
The article does not address the environmental impacts of using this technology in aerospace applications. A study on the environmental footprint of the new technology compared to current practices would be necessary to assess its environmental implications.
Original Abstract Submitted
A thermal radiation shield interface for cryogenic systems includes a first element with a distal, free end. Flanges project from the distal, free end of the first element. A second element also includes a distal, free end. Flanges project from the distal, free end of the second element. The flanges of the first element and the flanges of the second element are positioned in an interleaved arrangement to cover an opening between the first element and the second element shielding the opening from radiation leakage.
