Your Selections

TEAEG1E
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Publishers

Committees

Committee Codes

new

Design Considerations for Enclosed Turboshaft Engine Test Cells

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • AIR4989A
  • Current
Published 2018-11-21 by SAE International in United States
This SAE Aerospace Information Report (AIR) developed by a broad cross section of personnel from the aviation industry and government agencies is offered to provide state-of-the-art information for the use of individuals and organizations designing new or upgraded turboshaft engine test facilities.
Annotation icon
new

Design Considerations for Enclosed Turboprop Engine Test Cells

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • AIR5295A
  • Current
Published 2018-11-21 by SAE International in United States
This document is offered to provide state-of-the-art information about design factors that must be considered in the design of new or significantly modified engine test cells used to test propeller equipped turboprop engines in either QEC or bare engine configurations. The report does not address design considerations for test cells designed to test turboprop engines with dynamometer type load absorption devices because they are essentially tested as turboshaft engines. Design considerations for those test cells are presented in AIR4989, Reference 2.1.
Datasets icon
Annotation icon
new

Acoustical Considerations for Engine Test Cells

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • ARP5759
  • Current
Published 2018-11-21 by SAE International in United States
This document discusses, in broad and general terms, the subject of acoustical considerations in engine test cells. One of the primary purposes of an engine test cell is to control the noise emanating from the operating engine in order to reduce noise in the surrounding facility and community to acceptable levels. This is done by the design and installation of specialized acoustic elements and features, which need to be fully integrated into the overall test cell design. It should be further noted, that the requirements of acoustic control are critical to the proper operation of the engine, safety of plant equipment and personnel, and meeting local and legal noise requirements.
Datasets icon
Annotation icon

Gas Turbine Engine Test Facility Audit Process

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • ARP6196
  • Current
Published 2018-01-04 by SAE International in United States
This SAE Aerospace Recommended Practice provides recommendations for: the audit process in general; a list of specific areas of attention to be audited; maintaining the test facility in such a manner that it meets audit requirements.
Datasets icon
Annotation icon

Infrasound Phenomenon in Engine Test Cells

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • AIR5303
  • Current
Published 2018-01-04 by SAE International in United States
This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground level testing of large turbofan and turbojet engines, and particularly those who are interested in infrasound phenomena.
Annotation icon

Structural Design and Construction Considerations for Enclosed Turbofan/Turbojet Engine Test Cells

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • ARP5305A
  • Current
Published 2017-12-18 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) is written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in constructing new or adding to existing engine test cell facilities.
Annotation icon

Test Facility Shakedown and Commissioning

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • AIR6364
  • Current
Published 2017-11-29 by SAE International in United States
The paper discusses in general terms the activities required to be undertaken or demonstrated during the establishment of the facility such as: the assessment checks prior to forwarding to the end users site for embodiment into the facility system the establishment of the facility such as trial installations of hardware, functionality checking of lifting transportation and access systems, centerline pull checks, pressure testing of fuel and air start systems, flushing of wet systems and electrical continuity checking. the commissioning of the facility such as instrumentation calibrations, engine starts, engine running, assessment of command and control system, assessment of DAS system, aerodynamic and acoustic surveys. The paper will concentrate on the main engineering engine related aspects of the facility and will not necessarily contain information on the construction validation activities such as HVAC, electrical, facility fire system, waste water etc. Risk analysis may be performed during the design phase whose results could lead to pay particular attention to some specific equipment / functionalities during the commissioning phase. If identified, these risks should be translated to specific…
Datasets icon
Annotation icon

Installed Outdoor Engine Testing

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • AIR5301A
  • Current
Published 2017-11-29 by SAE International in United States
This SAE Aerospace Information Report (AIR) was written because of the growing interest in aircraft installed outdoor engine testing by the Federal Aviation Administration, airlines, charter/commercial operators, cargo carriers, engine manufacturers and overhaul and repair stations. This document was developed by a broad cross section of personnel from the aviation industry and government agencies and includes information obtained from a survey of a variety of operators of fixed and rotary wing aircraft and research of aircraft and engine maintenance manuals.
Datasets icon
Annotation icon

Trend Analysis for Maintaining Correlation of Gas Turbine Engine Test Cells

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • ARP5758A
  • Current
Published 2017-10-04 by SAE International in United States
This document describes a recommended practice and procedure for the trending of parameters to maintain the test cell correlation status. Trending is performed to monitor test cells for changes that can affect engine performance or the data acquired from engine tests.
Datasets icon
Annotation icon

Design, Calibration, and Test Methods for Turbine Engine Icing Test Facilities

EG-1E Gas Turbine Test Facilities and Equipment
  • Aerospace Standard
  • AIR6189
  • Current
Published 2017-09-15 by SAE International in United States
This SAE Aerospace Information Report (AIR) provides descriptions of test procedures and established practices for the application, use, and administration of the conduct of icing testing for all types of turbine engines in conventional supercooled liquid (14 CFR Part 25 Appendix C) environmental conditions in ground test facilities (sea-level and altitude) for icing certification purposes.
Datasets icon
Annotation icon