تقرير
Development and Experimental Evaluation of Passive Fuel Cell Thermal Control
| العنوان: | Development and Experimental Evaluation of Passive Fuel Cell Thermal Control |
|---|---|
| المؤلفون: | Colozza, Anthony J, Jakupca, Ian J, Castle, Charles H, Burke, Kenneth A |
| بيانات النشر: | United States: NASA Center for Aerospace Information (CASI), 2014. |
| سنة النشر: | 2014 |
| مصطلحات موضوعية: | Energy Production And Conversion, Fluid Mechanics And Thermodynamics |
| الوصف: | To provide uniform cooling for a fuel cell stack, a cooling plate concept was evaluated. This concept utilized thin cooling plates to extract heat from the interior of a fuel cell stack and move this heat to a cooling manifold where it can be transferred to an external cooling fluid. The advantages of this cooling approach include a reduced number of ancillary components and the ability to directly utilize an external cooling fluid loop for cooling the fuel cell stack. A number of different types of cooling plates and manifolds were developed. The cooling plates consisted of two main types; a plate based on thermopyrolytic graphite (TPG) and a planar (or flat plate) heat pipe. The plates, along with solid metal control samples, were tested for both thermal and electrical conductivity. To transfer heat from the cooling plates to the cooling fluid, a number of manifold designs utilizing various materials were devised, constructed, and tested. A key aspect of the manifold was that it had to be electrically nonconductive so it would not short out the fuel cell stack during operation. Different manifold and cooling plate configurations were tested in a vacuum chamber to minimize convective heat losses. Cooling plates were placed in the grooves within the manifolds and heated with surface-mounted electric pad heaters. The plate temperature and its thermal distribution were recorded for all tested combinations of manifold cooling flow rates and heater power loads. This testing simulated the performance of the cooling plates and manifold within an operational fuel cell stack. Different types of control valves and control schemes were tested and evaluated based on their ability to maintain a constant temperature of the cooling plates. The control valves regulated the cooling fluid flow through the manifold, thereby controlling the heat flow to the cooling fluid. Through this work, a cooling plate and manifold system was developed that could maintain the cooling plates within a minimal temperature band with negligible thermal gradients over power profiles that would be experienced within an operating fuel cell stack. |
| نوع الوثيقة: | Report |
| اللغة: | English |
| URL الوصول: | https://ntrs.nasa.gov/citations/20150002327 |
| ملاحظات: | NNC12BA01B WBS 152964.04.01.01.04.03 |
| رقم الأكسشن: | edsnas.20150002327 |
| قاعدة البيانات: | NASA Technical Reports |
| الوصف غير متاح. |