Refine Your Search

Date

Date

Topic

Topic

Metals Cetane Engine mechanical components Optics Diesel / compression ignition engines Assembling A-6C2 Seals Committee

Search Results

Viewing 1 to 20 of 93
123Next >Last >>
Sort by title
Standard

Storage of Aerospace Elastomeric Seals and Seal Assemblies Which Include an Elastomer Element Prior to Hardware Assembly
1998-11-01
HISTORICAL
ARP5316
This SAE Aerospace Recommended Practice (ARP) addresses the general requirements for data recording procedures, packaging, and storing of aerospace elastomeric seals and seal assemblies which include an elastomeric element prior to the seal being assembled into hardware components. The requirement for packaging is an integral part of the controlled storage procedure and provides a means of positive product identity from the time of manufacture to the time of assembly into a component.
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

Sealing Techniques for Missile Applications
2008-07-16
HISTORICAL
ARP1833A
The purpose of this standard is to provide the missile hydraulic and pneumatic component designer with information learned, tested and substantiated in correction of problems and failures experienced with seals that are subject to the unique requirements of missile static storage and subsequent dynamic operational conditions. Missile hydraulic and pneumatic component designers have been handicapped by the absence of concise design criteria for two difficult sealing conditions usually existing in missile applications as follows: Static pressure condition - Low pressure for long periods in a cyclic temperature environment (i.e., long term storage requirements). Dynamic pressure condition - High pressures suddenly applied in an extreme temperature environment (i.e., operational firing requirement).
123Next >Last >>
X