Metallic Seals For Extreme Temperature Pressure Applications Republic Aviation Corporation

Format:

Conference/Event

Author/Creator:

Lee, John, author.

Conference Name:

National Aeronautic Meeting

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1962

Summary:

This paper concerns the design, development and evaluation of metallic seals to meet the extreme conditions of temperature and pressure experienced in fluid power systems of advanced aerospace vehicles.The basic principles and design problems that characterize the use of metallic seals are discussed. Single and two-stage rod seals for 4000 psi, -65 F to +1000 F, hydraulic system applications using mineral oil and polyphenyl ether fluids are described. The performance evaluation of metallic and graphite piston rings are included. The selection of rod-gland material combinations and surface coatings are discussed. Static seal configurations for use at 4000 psi and temperatures up to 1000 F are also described

Notes:

Vendor supplied data

Publisher Number:

620422

Access Restriction:

Restricted for use by site license