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Nonflammable Aircraft Hydraulic Systems Development Air Force Wright Aeronautical Labs., Wright-Patterson Air Fo
- Format:
- Conference/Event
- Author/Creator:
- Snyder, Jr., Snyder, Jr., author.
- Conference Name:
- SAE International Congress & Exposition (1982-02-22 : Detroit, Michigan, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1982
- Summary:
- To eliminate the hazards associated with hydraulic fluid fires resulting from aircraft accidents and component failures, the Air Force established a program to develop a nonflammable aircraft hydraulic system using a nonflammable fluid over the -45\mDC to 135\mDC (-65\mDF to 275\mDF) temperature range. The Air Force is developing a chlorotrifluoroethylene oligomeric based fluid, compatible elastomeric seals, and necessary hydraulic component/system redesign. The status of this program is discussed which includes a summary of the flammability tests, fluid and seal development and performance testing of candidate materials in hydraulic components/systems
- Notes:
- Vendor supplied data
- Publisher Number:
- 821566
- Access Restriction:
- Restricted for use by site license
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