Refine Your Search

Topic

Search Results

Standard

Turbine Engine Starting System Design Requirements

1999-03-01
CURRENT
ARP949B
This SAE Aerospace Recommended Practice (ARP) defines and establishes a standard presentation of data for gas turbine propulsion engine starter characteristics in graphs and curves. The data presentation applies to both pneumatic and hydraulic energy source starting systems.
Standard

Safety Criteria for Pneumatic Starting Systems

1999-03-01
CURRENT
AIR1639A
This SAE Aerospace Information Report (AIR) presents safety criteria for pneumatic type engine starting system design and component hardware. Included are safety criteria in design of both starter control valves and starters as well as in design of airframe control systems. Safety topics concern starter valve operation and material application, airframe controls and instrumentation installations and starter rotor integrity and containment.
Standard

STARTER SYSTEM OPTIMIZATION START ANALYSIS, TURBINE ENGINE - ELECTRIC, BATTERY POWER

1987-08-01
CURRENT
AIR1602
This SAE Aerospace Information Report includes procedures for the analysis of a gas turbine engine start. It utilizes a standard form for the essential starting characteristics of the gas turbine engine and for the starting power capability of the aircraft battery. This report illustrates the format of the characteristic which is provided by the electric starter to transform the battery electric power (voltage and current) to the mechanical power (torque and speed) required to successfully start the engine. An aircraft engine start battery typically also serves as a backup source for emergency electrical energy. Guidelines are therefore provided for the determination of battery capacity to fulfill the emergency energy requirements of the aircraft.
Standard

RECIPROCATING ENGINE PNEUMATIC STARTERS

1994-02-01
CURRENT
AIR4152
The purpose of this SAE Aerospace Information Report (AIR) is to present a brief discussion of pneumatic starters for reciprocating engines. This AIR also provides a general analysis guide for preliminary sizing of pneumatic starter systems for reciprocating engines.
Standard

Pneumatic Ground Power Supplies for Starting Aircraft

2004-04-06
CURRENT
AIR944C
The material contained in this report has been simplified to facilitate its use. Specific manufacturers should be contacted for more detailed information. Many of the basic power supplies are available in numerous configurations and some provide shaft power or electrical power in addition to the pneumatic capability. Vehicles for the ground transportation of the power supplies are also varied to fit specific requirements.
Standard

PNEUMATIC GROUND POWER SUPPLIES FOR STARTING AIRCRAFT

1990-02-01
HISTORICAL
AIR944B
The material contained in this report has been simplified to facilitate its use. Specific manufacturers should be contacted for more detailed information. Many of the basic power supplies are available in numerous configurations and some provide shaft power or electrical power in addition to the pneumatic capability. Vehicles for the ground transportation of the power supplies are also varied to fit specific requirements.
Standard

PNEUMATIC GROUND POWER SUPPLIES FOR STARTING AIRCRAFT

1978-01-01
HISTORICAL
AIR944A
The material contained in this report has been simplified to facilitate its use. Specific manufacturers should be contacted for more detailed information. Many of the basic power supplies are available in numerous configurations and some provide shaft power or electrical power in addition to the pneumatic capability. Vehicles for the ground transportation of the power supplies are also varied to fit specific requirements. The state-of-the-art in small gas turbines has advanced to a point where they are competitive with the more conventional ground power supplies in practically all areas.
Standard

PERFORMANCE ACCEPTANCE TESTING OF AIR TURBINE STARTERS

1982-02-25
CURRENT
ARP715A
This Aerospace Recommended Practice describes two performance acceptance test methods to determine the performance acceptability of new production and overhauled air turbine starters. Before a new or overhauled starter is delivered to a customer, the starter is subjected to a performance acceptance test in accordance with an acceptance test procedure. The performance acceptance test is intended to ensure that the customer receives a starter that meets or exceeds minimum starter performance requirements.
Standard

INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS

1987-04-01
HISTORICAL
AIR1174A
This report lists military and industry specifications and standards which are used in aerospace engine starting and auxiliary power systems. Only those hardware standards which have been specifically designed for engine starting systems are listed. Revisions and amendments which are current for these specifications and standards are not listed.
Standard

INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS

1970-07-15
HISTORICAL
AIR1174
This report lists military and industry specifications and standards which are used in aerospace engine starting systems. Only those hardware standards which have been specifically designed for engine starting systems are listed. Revisions and amendments which are current for these specifications and standards are not listed.
Standard

Glossary, Aircraft Engine Starting and Auxiliary Power Systems

2001-04-01
CURRENT
ARP906B
The Aircraft Engine Starting and Auxiliary Power System Glossary presents definitions of terms commonly encountered and associated with aircraft engine starting and auxiliary power systems. Terms have been arranged alphabetically.
Standard

Gas Energy Limited Starting Systems

1999-04-01
CURRENT
AIR1467B
This SAE Aerospace Information Report (AIR) presents information on gas energy limited propulsion engine starting systems employed in commercial and military applications and remote industrial sites. The types of systems discussed utilize solid propellant cartridge gas, monopropellant hydrazine gas, bipropellant gas, compressed stored gas, and cryogenic stored nitrogen. Presented information conveys design features, performance capabilities and system limitations with methods of computing results.
X