Gernert et al., 1991 - Google Patents
Flexible heat pipe cold plates for aircraft thermal controlGernert et al., 1991
- Document ID
- 17274272609640829707
- Author
- Gernert N
- Sarraf D
- Steinberg M
- Publication year
- Publication venue
- SAE transactions
External Links
Snippet
This paper describes the development of flexible heat pipe cold plate (FHPCP) technology for aircraft thermal control. Four different FHPCP's were constructed for a variety of difficult aircraft cooling problems. This included an electronics package embedded in a moving …
- 238000001816 cooling 0 abstract description 17
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US7246940B2 (en) | Method and apparatus for managing the temperature of thermal components | |
| Zilio et al. | Active and passive cooling technologies for thermal management of avionics in helicopters: Loop heat pipes and mini-Vapor Cycle System | |
| CA2924101A1 (en) | Aviation bypass valve including a shape memory alloy material | |
| Gernert et al. | Flexible heat pipe cold plates for aircraft thermal control | |
| Mao et al. | Shape memory alloy actuator with active cooling device and deflectable winglet application | |
| CN109405382B (en) | Anti-impact vibration-reduction heat dissipation system suitable for satellite-borne gas bearing refrigerator | |
| Yao et al. | Study on heat pipe heat dissipation of high-power ultrasonic transducer | |
| Babin et al. | Experimental investigation of an ion-drag pump-assisted capillary loop | |
| Lebel et al. | An experimental apparatus and procedure for the simulation of thermal stresses in gas turbine combustion chamber panels made of ceramic matrix composites | |
| Arts et al. | LPT9310 COTS cooler for ECOSTRESS | |
| Belov et al. | Numerical and experimental study of loop heat pipe steady-state performance | |
| Der et al. | A low cost, flexible pulsating heat pipe technology | |
| JP6970202B2 (en) | Heat engine with dynamically controllable hydraulic outlet | |
| Bugby et al. | Advanced components and techniques for cryogenic integration | |
| Martinez | Experimental study of a low-frequency thermoacoustic device | |
| Lohse et al. | Inherently safe looped thermosyphon cooling system for aircraft applications using dielectric fluid H-Galden | |
| Swift et al. | The NICMOS turbo-Brayton cryocooler—two years in orbit | |
| Gernert et al. | A Thermal Analysis of an F/A-18 Wing Section for Actuator Thermal Management | |
| Mehoke et al. | Development Of The Miniature Spacecraft Energy Retention (MiSER) Thermal Control Panel | |
| Oriti et al. | Advanced Stirling Convertor Testing at NASA Glenn Research Center | |
| Oriti | Extended Operation of Stirling Convertors in a Thermal Vacuum Environment | |
| Tournier et al. | Modeling of the startup of a horizontal lithium heat pipe from a frozen state | |
| Tu et al. | Heat and mass transfer in a flat disc-shaped evaporator of a miniature loop heat pipe | |
| Manzoni et al. | DESIGN OF PULSATING HEAT PIPES A novel non-equilibrium lumped parameter model for transient gravity levels | |
| Swerdling et al. | Development of a thermal diode heat pipe for the advanced thermal control flight experiment/ATFE |