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SAE AIR 4151 : 2004

Current
Current

The latest, up-to-date edition.

INTRODUCTION TO STARTING SYSTEMS
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

13-04-2004

1 SCOPE
2 APPLICABLE DOCUMENTS
  2.1 SAE Publications
  2.2 USAF Publications
3 DISCUSSION
  3.1 Purpose
  3.2 Starting Energy Balance
  3.3 Start Performance
  3.4 Start System Uses
  3.5 Start System Types
  3.6 Ground Power Unit (GPU)
  3.7 Ground Support Equipment (GSE)
  3.8 Electric Battery Power Unit
  3.9 Auxiliary Power Unit (APU)
  3.10 Jet Fuel Starter (JFS)
  3.11 Start System Components
  3.12 Fluid Energy Storage
  3.13 Fuel Energy Storage
  3.14 Energy Extraction
  3.15 Cartridge Energy Sources
  3.16 Engine Starters
  3.17 Starter Air Valve
  3.18 Propulsion Engine Starter Control Systems
  3.19 Engine Starting Considerations
4 SUMMARY
5 FURTHER INFORMATION
FIGURES

This SAE Aerospace Information Report (AIR) covers basic aircraft engine start systems fundamentals.

Committee
AE-6
DocumentType
Standard
Pages
28
ProductNote
THIS STANDARD ALSO REFERS TO 841604, 841606, 841636, 924105, 942104,942106
PublisherName
SAE International
Status
Current
Supersedes

SAE ARP 906 : 2001 GLOSSARY, AIRCRAFT ENGINE STARTING AND AUXILIARY POWER SYSTEMS
SAE AS 1606 : 1992 GAS TURBINE STARTER (JET FUEL STARTER) SPECIFICATION
SAE AIR 1174 : 2001 INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS
SAE ARP 1961 : 2016 GEARBOX - AIRFRAME MOUNTED ACCESSORY
SAE AIR 944 : 1990 PNEUMATIC GROUND POWER SUPPLIES FOR STARTING AIRCRAFT
SAE AIR 4204 : 1991 COMMERCIAL AIRCRAFT AUXILIARY POWER UNIT INSTALLATIONS
SAE AIR 1466 : 1978 HYDRAULIC ENERGY LIMITED ENGINE STARTING SYSTEMS
SAE AIR 744 : 2015 AEROSPACE AUXILIARY POWER SOURCES
SAE AIR 713 : 1988 GUIDE FOR DETERMINING, PRESENTING, AND SUBSTANTIATING TURBINE ENGINE STARTING AND MOTORING CHARACTERISTICS

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