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СтандартыSAE

SAE ARP246D

Действует
Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines (Stabilized: Sep 2018)
ОписаниеИзмененияСсылкиВерсии

Ссылочные документы

SAE ARP755D
Действует
Aircraft Propulsion System Performance Station Designation and Nomenclature
SAE ARP246C
Заменен
Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines

На этот документ ссылаются

SAE ARP1420C
Действует
Gas Turbine Engine Inlet Flow Distortion Guidelines (Stabilized: Apr 2017)
SAE ARP1420B
Заменен
Gas Turbine Engine Inlet Flow Distortion Guidelines
SAE ARP246C
Заменен
Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines
SAE ARP246A
Заменен
POSITION TERMS AND NUMBERING SYSTEM FOR AIRCRAFT GAS TURBINE ENGINES
SAE AIR1419D
Действует
Inlet Total-Pressure Distortion Considerations for Gas-Turbine Engines
SAE AIR1379B
Действует
Prestressing (Autofrettaging) of Hydraulic Tubing Lines (Stabilized: Feb 2019)
SAE AIR1379A
Заменен
Prestressing (Autofrettaging) of Hydraulic Tubing Lines
SAE AIR1419C
Заменен
Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
SAE AIR1419B
Заменен
Inlet Total-Pressure-Distortion Considerations for Gas-Turbine Engines
SAE AS755F
Действует
Aircraft Propulsion System Performance Station Designation
SAE ARP246
Заменен
NUMBERING POSITIONS FOR NOZZLES, BURNERS, ETC. FOR TURBO-JET AND TURBO-PROP ENGINES
SAE ARP1420A
Заменен
Gas Turbine Engine Inlet Flow Distortion Guidelines
SAE ARP246B
Заменен
ORIENTATION OF ENGINE AXIS, COORDINATE AND NUMBERING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES
SAE ARP1420
Заменен
GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES