Your Selections

TEAEG1A
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Publishers

Committees

Committee Codes

Periodic Surveillance Procedures for Horizontal Dynamic Balancing Machines

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP1340B
  • Current
Published 2018-07-02 by SAE International in United States

This Technical Report has been declared “CANCELLED” as of November 2017. By this action, this document will remain listed in the respective index, if applicable. Cancelled Technical Reports are available from SAE.

Balancing Machine Proving Rotors

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP4162B
  • Current
Published 2017-03-17 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) specifies a series of balancing machine proving rotors and related test weights as directly required for the evaluation of gas turbine rotor balancing machines.
Datasets icon
Annotation icon

Balancing Machines - Description and Evaluation Vertical, Two-Plane, Hard-Bearing Type for Gas Turbine Rotors

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP4050A
  • Current
Published 2017-02-07 by SAE International in United States
Characteristics of vertical hard-bearing balancing machines are described which make such machines suitable for gas turbine rotor balancing.
Datasets icon
Annotation icon

Balancing Machines - Description and Evaluation Vertical, Single-Plane, Hard-Bearing Type for Gas Turbine Rotors

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP5323A
  • Current
Published 2017-02-02 by SAE International in United States
Characteristics of vertical hard-bearing balancing machines are described which make such machines suitable for gas turbine rotor balancing.
Datasets icon
Annotation icon

Balancing Machines: Tooling Design Criteria

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP4163
  • Current
Published 2016-05-20 by SAE International in United States
This document establishes general design criteria, tolerances, and limits of application for tooling, fixtures and accessories for mounting and driving gas turbine engine rotors on horizontal and vertical balancing machines. For your own safety, while using balancing tooling, regard the safety instructions of the individual supplier.
Datasets icon
Annotation icon

Adapter Interface - Turbine Engine Blade Moment Weighing Scale

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP1134
  • Current
Published 2016-05-20 by SAE International in United States
To provide a standard interface adapter flange on any blade classification instrument capable of meeting the sensitivity requirements for the specific class.
Datasets icon
Annotation icon

Balancing Machines – Description and Evaluation Vertical, Single-Plane, Non-Rotating Type for Gas Turbine Rotors

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP6217
  • Current
Published 2015-02-10 by SAE International in United States
Characteristics of vertical non-rotating balancing machines are described which make such machines suitable for balancing rigid unbladed gas turbine rotors or rotors with fixed, integral blades.
Datasets icon
Annotation icon

Balancing Machines - Description and Evaluation Vertical, Single-Plane, Hard-Bearing Type for Gas Turbine Rotors

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP5323
  • Historical
Published 2014-01-16 by SAE International in United States
Characteristics of vertical hard-bearing balancing machines are described which make such machines suitable for gas turbine rotor balancing.
Datasets icon
Annotation icon

Balancing Machines - Description and Evaluation Vertical, Single-Plane, Soft-Bearing Type for Gas Turbine Rotors

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP588C
  • Current
Published 2012-12-17 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) specifies the requirements of balancing machines that make them suitable for the subject class of work. It was developed for soft-bearing balancing machines but may also be used for hard-bearing machines until ARP4050 is issued for that type of machine.
Datasets icon
Annotation icon

Balancing Machines - Description and Evaluation Horizontal, Two-Plane, Soft-Bearing Type for Gas Turbine Rotors

EG-1A Balancing Committee
  • Aerospace Standard
  • ARP587C
  • Current
Published 2012-12-17 by SAE International in United States
The specific performance requirements preceding each test in Section 9 have been written to define certain characteristics of the machine. Conformance with the tests constitutes what is considered minimum proof that the machine will meet these requirements. The test procedures will not prove conformance with all requirements over the full range of all variables, neither will they measure nor define the exact reasons for nonconformance in a given test. Failure of a machine to conform may be due to shortcomings in specific components or to more general reasons such as lack of ruggedness, improper leveling or anchoring to the floor, etc.
Datasets icon
Annotation icon