Pump Standards
Pump standards address the performance, test, and design requirements for pumps that are used in commercial vehicles and aircrafts. Additionally, pump standards serve as a set of guidelines and recommended practices related to the maintenance, configuration, and design of pumps. One major developer of pump standards is SAE International (SAE). SAE has developed a variety of pump standards that are applicable to hydraulic pumps and fuel injection pumps. SAE has several technical committees that have contributed to the development of these standards, including the Truck and Bus Aerodynamics and Fuel Economy Committee (fact sheet) and the A-6C6 Power Sources Committee (fact sheet).
SAE J 744-2021
Hydraulic Pump and Motor Mounting and Drive Dimensions
This SAE Standard applies to hydraulic pumps and motors used on off-road self-propelled work machines as described in SAE J1116.
SAE AS 5259/2A-2021
CRIMPING TOOL AND ACCESSORIES, HYDRAULIC PUMPS, 10000 PSI MINIMUM
SCOPE IS UNAVAILABLE.
SAE J 1341-2012 (SAE J1341-2012)
Test Method for Measuring Power Consumption of Hydraulic Pumps for Trucks and Buses
This document covers evaluation techniques for determining the power consumption characteristics of hydraulic pumps used on heavy-duty trucks and buses. The testing technique outlined in this SAE Recommended Practice was developed as part of an overall program for testing and evaluating fuel consumption of heavy-duty trucks and buses. The technique outlined in this document provides a description of the test to be run to determine power consumption of these engine driven components, the type of equipment and facilities which are generally required to perform these tests are discussed in SAE J 745. It is recommended that the specific operating conditions suggested throughout the test be carefully reviewed on the basis of actual data obtained on the specific vehicle operation.
SAE AIR 1922B-2017
Aerospace û System Integration Factors That Affect Hydraulic Pump Life
This SAE Aerospace Information Report presents the following factors that affect hydraulic pump life and performance: a. The need to supply hydraulic fluid at the correct pressure and quality to the pump inlet port b. Considerations for the pump output c. Factors to be considered for the pump case drain lines d. The mounting of the hydraulic pump e. Hydraulic fluid properties, including cleanliness
SAE AS 595D-2010 (SAE AS595D-2010)
Aerospace - Civil Type Variable Delivery, Pressure Compensate, Hydraulic Pump
This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance and qualification test offlat cut-off pressure compensated, variable delivery hydraulic pumps, used in civil aircraft hydraulic systems. It also provides parameters for a Procurement Specification to be used in conjuction with this AS for each pump. NOTE: Hydraulic pumps may incorporate features such as a clutch in the input dirve, which will not be covered ty this standard.
SAE AIR 560C-1999 (SAE AIR560C-1999)
Missile Hydraulic Pumps ( Reaffirmed: Jul 2007 )
Missile pumps are categorized by a moderate testing life and a relatively short operational service life. Generally, the pumps are operated at higher speeds, temperatures, and pressures than those used in manned aircraft systems, yet reliability must be extremely high, since there rarely is a redundant system aboard the missile. Due to the short but critical life and performance requirements, development, reliability and acceptance testing should be focused on eliminating infant mortality failures. Missile pumps must be compatible with very severe environmental conditions during the service life. In general, the temperature, vibration, shock, and acceleration encountered are more severe than those met in manned aircraft. This SAE Aerospace Information Report (AIR) will be confined to describing missile environments and pump usage that differ significantly from those normally encountered in manned aircraft. Since missile pumps are usually driven by a secondary power source, and since this AIR is intended for use by systems designers, as well as pump designers, a brief description of some of these sources and some potential problem areas associated with each are included for reference. A more detailed treatment of auxiliary power sources can be found in AIR744. Detailed test requirements are not included in this AIR since a wide variation exists between those operating conditions and environments that might be encountered on an air-to-air missile, hung beneath the wing of a fighter aircraft, and that of an ICBM (Intercontinental Ballistic Missile), launched from an environmentally controlled silo. Missile pumps frequently have their genesis in standard aircraft pumps, however, what distinguishes them from manned aircraft pumps is that they are usually operated outside of, or at the extreme of their long-life design parameters. Therefore, if a new design pump is being proposed for a missile application, environmental conditions referenced in this AIR should be considered, as opposed to long-life operation and environmental requirements of a manned aircraft, engine-driven pump.
SAE J 968-1-2015 (SAE J968-1-2015)
Diesel Injection Pump Testing - Part 1: Calibrating Nozzle and Holder Assemblies
This part of SAE J968 specifies two types of calibrating nozzle and holder assemblies intended for the testing and setting of diesel injection pumps on test benches. It applies to: a. A calibrating nozzle and holder assembly with a single hole orifice plate; b. A calibrating nozzle and holder assembly with a delay pintle type nozzle. The approximate range of the calibrating nozzle and holder assembly is up to: a. 300 mm 3 /stroke with the single hole orifice plate; b. 150 mm 3 /stroke with the delay pintle type nozzle. Setting and maintenance requirements are specified in ISO 4008/3.
SAE J 968-2-2015 (SAE J968-2-2015)
Diesel Injection Pump TestingΓÇöPart 2: Orifice Plate Flow Measurement
This part of SAE J968 specifies the flow measuring system, including the fixture, to be used for flow testing the single hole orifice plates used in an orifice plate type nozzle and holder assembly (described in SAE J968/1) which is intended for testing and setting diesel fuel injection pumps on test benches. The flow measuring system and fixture ensure accurate flow testing of the entire range of orifices from 0.4 to 0.8 mm diameter as specified in SAE J968/1. It is intended primarily for use by the manufacturers of single hole orifice plates.
SAE ARP 1797A-1999 (SAE ARP1797A-1999)
Aircraft and Aircraft Engine Fuel Pump Low Lubricity Fluid Endurance Test ( Reaffirmed: Dec 2007 )
This procedure is intended to apply to fuel pumps. This procedure will be defined in terms of recommended test fluid, test setup, test conditions, and test method. This procedure may be used for other fuel system components, by testing in conjunction with the pump, which normally supplies the component inlet flow, or a substitute test pump of similar capacity. This procedure may be used, with variations in test conditions and test fluid for performing pump evaluation tests. Tests at progressively increasing pump speeds and pressures will provide design limitation data. Alternate test periods on a test pump and another pump, of a design for which actual service durability is known, will provide useful comparison data.
SAE AS 19692B-2016 (SAE AS19692B-2016)
Aerospace ΓÇô Military Type Variable Delivery, Pressure Compensated Hydraulic Pump
This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance, and qualification testing of flat cut-off pressure compensated, variable delivery hydraulic pumps used in military aircraft hydraulic systems. It also provides parameters for a Procurement Specification to be used in conjunction with this AS. The hydraulic pumps defined by this AS are generally for use in aircraft hydraulic systems conforming to and as defined in AS5440 and MIL-H-8891, as applicable. NOTES: 1. Hydraulic pumps may incorporate features such as a clutch in the input drive, which will not be covered by this standard. 2. AS595 should be used for commercial aircraft hydraulic pumps. 3. This document should not be used for hydraulic pumps in Electro-Hydrostatic Actuator applications (EHAs).
SAE ARP 4028-1994 (SAE ARP4028-1994)
Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation ( Reaffirmed: Dec 2007 )
This procedure is intended to apply to all engine or airframe mounted fuel pumps and controls when required by the applicable specification. The procedure recommends a recirculation system similar to ARP492 to control the fuel properties affecting the fluid and its ability to 'release' fuel vapors and dissolved air and have these 're-entrained or dissolved' during the fluid recovery process back to the tank and the original starting conditions. This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft/engine fuel pumps for the purpose of: a. determining two phase ('slugging flow') inlet performance capability; b. determining the pump's resistance to deterioration during an endurance test with the operating conditions defined by the applicable specification which includes two phase ('slugging flow') operation; and c. determining the effects that contaminated fuel operation may have had on two phase ('slugging flow') inlet performance. The procedure recommended herein is intended to produce useful, reproducible, steady state results. This test is not intended to establish maximum starting altitude or rate of climb performance of the pump. This procedure defines recommended test setups, test procedures, and data requirements for testing engine or airframe mounted fuel pumps or controls with pumps for the purpose of determining 'slugging flow' inlet performance capability
SAE ARP 4024-1994 (SAE ARP4024-1994)
Aircraft/Engine Fuel Pump Net Positive Suction Pressure Performance Test and Evaluation ( Reaffirmed: Dec 2007 )
This procedure applies to engine or airframe-mounted fuel pumps. The procedure recommends single-pass operation to minimize changes in fuel properties affecting NPSP capability. An optional method using a recirculation system is also included and may be specified at the discretion of the equipment specification. This procedure defines the recommended test setup, test procedure, data acquisition, and data presentation.
SAE ARP 492C-1994 (SAE ARP492C-1994)
Aircraft Engine Fuel Pump Cavitation Endurance Test ( Reaffirmed: Dec 2007 )
This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft engine fuel pumps for the purpose of determining their resistance to deterioration, during steady state endurance test, while receiving MIL-T-5624 Grade JP-4 fuel as a homogenous mixture of gas and liquid expressed as a ratio of vapor volume to liquid volume (V/L). If any of the above conditions do not apply, refer to Section 2. The procedure recommended herein is based on experience gathered by a number of laboratories conducting component qualification tests to MIL-E-5009, currently MIL-E-5007. It is intended to produce a uniform reproducible steady state test condition for fuel pump cavitation testing as required by various military engine specifications. This test is not intended to establish altitude or climb rate, starting, or other transient performance of the article tested.
SAE AS 5994A-2013 (SAE AS5994A-2013)
Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery (Stabilized: Oct 2013)
This specification establishes the common requirements for variable delivery electric motor driven, hydraulic pump units, suitable for use in aircraft hydraulic systems.
SAE J 745-2019
Hydraulic Power Pump Test Procedure
This test code describes tests for determining characteristics of hydraulic positive displacement pumps used on off-road self-propelled work machines as referenced in SAE J1116.
ISO 4093:1999
Diesel engines -- Fuel injection pumps -- High-pressure pipes for testing
This International Standard specifies the functional requirements of a range of high-pressure pipes for use on benches for the testing and setting of fuel injection pumps intended for diesel engines. Only dimensions and requirements affecting the hydraulic characteristics of the pipes are specified. Other requirements, such as the type of end connections or shape of the pipes when bent, are not included as these depend on the connections provided on the pump outlets and injector inlets, and on the design features of individual pumps and test benches. This International Standard applies to a range of pipes to enable the pump engine manufacturer to choose a suitable type of pipe for pump deliveries up to 300 mm 3 /stroke/cylinder. The particular pipe to be used shall be identified by the pump manufacturer in the test schedule for each individual pump type and application.
ISO 6519:2015
Diesel engines - Fuel injection pumps - Tapers for shaft ends and hubs
ISO 6519:2015 specifies the dimensions of tapered shaft ends and hubs of fuel injection pumps and common-rail high pressure pumps for diesel (compression-ignition) engines. The specified shaft ends and hubs may be used with or without Woodruff keys. NOTE The specified shaft ends and hubs can also be used for other applications where no specific standards exist.
SAE J 1537-2021
Gasoline Low-Pressure Electric Fuel Pump Characterization
This SAE Recommended Practice defines the tests for three basic categories of pump characteristics. These are the basic functional performance tests, the pump limitation tests and the pump integrity tests. The basic functional tests included are three individual tests, with the first being for pump speed, current draw, and electrical resistance. The other two individual tests are for the deadhead pressure and the delivered fuel flow rate at the rated delivery pressure and voltage. The included tests for pump limitations are individual tests for hot fuel handling, cold magnet knockdown, load dump transient, electrical interference, and reverse flow leak. The testing for pump integrity includes individual tests for vibration, temperature cycling, internal fluid compatibility, and operational durability. These 12 individual tests provide a characterization of the particular pump. This document only addresses the in-tank-mounted, electric-motor-driven, low-pressure fuel pump itself, and does not address in-tank pump modules, as these modules may include other devices. The pumps that are to be tested are intended for the pumping of liquid fuels that are applicable to fuel-injected, spark-ignition engines.
SAE J 1549-2015 (SAE J1549-2015)
Diesel Fuel Injection Pump - Validation of Calibrating Nozzle Holder Assemblies
The fuel injection pump is intended to validate the accuracy of calibrating nozzle and holder assemblies for applications using 0.4 - 0.8 mm diameter orifice plates and to assist in identifying problems in fuel injection pump test stands.
SAE J 1668-2021
Diesel Engines - Fuel Injection Pump Testing
The correct setting and adjustment of fuel injection pumps requires standardized testing conditions. This SAE Standard summarizes the design and operating parameters for test benches so that, using certain information supplied by the pump manufacturer, the pump test schedule, and certain information supplied by the test bench manufacturer, it can be determined whether a particular test bench is suitable for driving a particular injection pump. This document is in most cases a summary of the ISO Standard 4008, Parts 1, 2, and 3 and is intended to provide its critical aspects. Standard ISO 4008 should be referred to for more details.
SAE J 1776-2014 (SAE J1776-2014)
Marine Vehicles - Hydraulic System Pumps and Motors - Design and Specification Guide
This SAE Recommended Practice provides guidance for defining the requirements for evaluating hydraulic pumps and motors and for preparing detailed specifications for these components. The user can follow this document to set forth the pump and motor environmental and performance considerations, establish service life and reliability goals, and define specific evaluation tests for marine vehicle applications.
SAE J 2025-2021
Method for Evaluating the Flow Properties of Pumpable Sealers
This SAE Recommended Practice sets forth a method for evaluating the flow properties of automotive sealers that have been dispensed via a high pressure automatic system.
SAE J 2311-2020
Automatic Transmission Hydraulic Pump Test Procedure
This SAE Recommended Practice provides a method to determine the performance characteristics of the hydraulic oil pumps used in automatic transmissions and automatic transaxles. This document outlines the specific tests that describe the performance characteristics of these pumps over a range of operating conditions and the means to present the test data. This document is not intended to assess pump durability.
SAE J 2317-2015 (SAE J2317-2015)
Tamper Resistance for Adjustable Parameters on Diesel Fuel Injection Pumps
This SAE Recommended Practice defines a guideline for the fuel injection pump designer to select appropriate fastener designs which are considered to be tamper-resistant. It applies to fuel injection pumps used on diesel engines.
SAE J 2747-2019
Hydraulic Pump Airborne Noise Bench Test
Communicate the process of accurately measuring sound power levels of positive displacement hydraulic pumps commonly used in ground vehicle steering systems. This recommended practice defines the pump mounting (pulley, belt tension, isolation), operating conditions, (fluids, speed, temperature, pressure), room accoustics, instrumentation, noise measurement technique and data acquisition setup to be used. Included are recommendations for test sample size, and format for data presentation/reporting.
ISO 7299-1:2007
Diesel engines - End-mounting flanges for pumps - Part 1: Fuel injection pumps
ISO 7299-1:2006 specifies dimensional requirements for nine types of end-mounting flanges for fuel injection pumps (rotary, distributor and in-line fuel injection pumps) for use in diesel (compression-ignition) engines.
SAE AS 47B-2013 (SAE AS47B-2013)
PUMP, FUEL, MOUNTING PAD AND DRIVE (Stabilized: Dec 2013)
Scope is unavailable.
SAE AS 838A-2013 (SAE AS838A-2013)
Aircraft Hydraulic Starter/Pumps (Stabilized: Oct 2013)
This specification established (1) the common requirements for hydraulic units capable of functioning as starters and as pumps suitable for use in aircraft and missiles and (2) the methods to be used for demonstrating compliance with these requirements.
