This content is not included in your SAE MOBILUS subscription, or you are not logged in.
SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE
- Aerospace Standard
Published April 01, 1995 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Information Report (AIR) is to present to hydraulic system designers the salient factors that affect hydraulic piston pump life and performance.
It is noted that this document differs in scope from ARP819. ARP819 is a composite checklist of the many variables that affect the pump selection for a particular application.
|Aerospace Standard||Aerospace – System Integration Factors That Affect Hydraulic Pump Life|
|Aerospace Standard||Aerospace - Application Guide for Hydraulic Power Transfer Units|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|TABLE 1||Suggested In-Service Fluid Limits (Reference AIR810)|
A6C4 is responsible for the development of standards, processes, and practices related to Fluid Power Sources (Pumps, Motors, Accumulators), and the integration of these components for Commercial and Military air vehicles. The panel provides a forum for government engineers, prime contractors, and suppliers to exchange technical information, regulatory updates, recent technology developments, issues related to system development and in service operation and lessons learned.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.