Refine Your Search

Date

Date

Topic

Topic

A-6C2 Seals Committee Planning / scheduling Electrohydraulics Defense industry Military aircraft Bodies and Structures Splines Standard

Search Results

Viewing 1 to 20 of 56
123Next >Last >>
Sort by title
Standard

Static Axial O-Ring Seal Applications Without Anti-Extrusion Devices for Engine and Engine Control Systems
2021-08-26
HISTORICAL
ARP1234D
This document establishes standard gland design criteria and dimensions for static axial O-ring seal applications without anti-extrusion devices specifically for engines and engine control systems operating at a maximum pressure of 1500 psi (10345 kPa). NOTE: The criteria herein are similar, but not identical, to those in AS4716 and the legacy standard MIL-G-5514.
Standard

Static Axial O-Ring Seal Applications Without Anti-Extrusion Devices for Engine and Engine Control Systems
2020-11-09
HISTORICAL
ARP1234C
This document establishes standard gland design criteria and dimensions for static axial O-ring seal applications without anti-extrusion devices specifically for engines and engine control systems operating at a maximum pressure of 1500 psi (10345 kPa). NOTE: The criteria herein are similar, but not identical, to those in AS4716 and the legacy standard MIL-G-5514.
Standard

Selection of Scrapers for Fluid Power Applications
2023-06-16
WIP
AIR7142
This SAE Aerospace Information Report (AIR) provides information on the selection of scrapers when combined with rod (ID) seals in fluid power applications, such as linear actuators and landing gear shock struts
Standard

Selection of Metallic Spring Energized Seals for Aerospace
2022-04-20
WIP
AIR6079A
The purpose of this report is to provide design, application and maintenance engineers with basic information on the use of metallic Spring Energized sealing devices when used as piston (OD) and rod (ID) seals in aircraft fluid power components such as actuators, valves, and swivel glands. The Spring Energized seal is defined and the basic types in current use are described. Guidelines for selecting the type of Spring Energized seal for a given design requirement are covered in terms of friction, leakage, service life, installation characteristics, and interchangeability. Spring Energized seals can also be made in various forms and types, including face seals (internal and external pressure sealing types), and rotary variants too. These further types will not be discussed in this document, but many of the same principles apply for them as well.
Standard

Retainers (Backup Rings), Hydraulic and Pneumatic, Polytetrafluoroethylene Resin, Single Turn, Scarf-Cut, For Use in AS4716 Glands
2020-08-25
HISTORICAL
AS5781B
This SAE Aerospace Standard (AS) specifies scarf-cut polytetrafluoroethylene (PTFE) retainers (backup rings) for use in glands in accordance with AS4716. They are usually used in hydraulic and pneumatic system components as anti-extrusion devices in conjunction with O-rings and other seals for static and dynamic applications. NOTE: This specification includes material tests but does not include hydraulic or pneumatic performance tests.
Standard

Recommendations for Installation of Seals in Standard Glands
2016-02-16
CURRENT
ARP5555
This SAE Aerospace Recommended Practice (ARP) contains guidance regarding hardware design and installation procedures for seals in hydraulic components that utilize standard seal glands in accordance with AS4716, AS4832, AS4088, AS4052, AS5857, and AS6235.
Standard

Reciprocating Sealing Surface Finishes in Fluid Power Systems
2022-05-13
WIP
ARP6010
This document provides recommendations for obtaining a finish and texture for reciprocating sealing surfaces in fluid power systems to improve dynamic seal performance. Recommendations on how to specify and measure the surface finish are also provided.
Standard

ROD SCRAPER GLAND DESIGN STANDARD
1994-05-01
HISTORICAL
AS4088A
Gland details are described for rod diameters from 1/4 to 15-1/2 inches, inclusive, corresponding to AS 568 O-Ring Dash No. sizes -108/-111, -206/-222, -325/-349 and -425/-460.
123Next >Last >>
X