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PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
- Aerospace Standard
Published May 01, 1998 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification and a detail pump specification establish the requirements for variable flow hydraulic pumps, for use in aircraft hydraulic systems conforming to and as defined in MIL-H-5440 and MIL-H-8891, as applicable. The general requirements for type I and type II hydraulic systems pumps are specified in MIL-H-8775 and for type III system pumps in MIL-H-8890.
|Aerospace Standard||Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump|
|Aerospace Standard||Standard Impulse Machine Equipment and Operation|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|TABLE I||Rated discharge pressure|
|TABLE II||Temperature relationship|
|Unnamed Dataset 5|
|TABLE III||Metallic coatings|
|Unnamed Dataset 7|
|TABLE IV||Qualification tests|
|TABLE V||Endurance test conditions|
|TABLE VI||Test specimen|
|Unnamed Dataset 11|
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.
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