Variable Attitude Test Stand

Metadata Updated: March 8, 2017

The Variable Attitude Test Stand designed and built for testing of the V-22 tilt rotor aircraft propulsion system, is used to evaluate the effect of aircraft flight attitudes on the bearings and lubrication system of a propulsion system. The test stand can subject an operating engine to a wide range of fixed or continuously varying pitch and roll attitudes. This is one of the few test facilities in the world where full size rotors or propellers can be evaluated with the associated gearboxes and other airframe unique systems. In addition to propeller engines, turbojet/fan engines can be tested on this facility. This facility has been used for development and for FAA certification testing.Test stand capabilities:Pitch 105 degrees nose up and 60 degrees nose downRole +/- 60 degreesThrust loads up to 50,000 poundsEngine is mounted 30 feet above ground level

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Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

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Metadata Created Date March 8, 2017
Metadata Updated Date March 8, 2017

Metadata Source

Harvested from Federal Laboratory Consortium Data.json

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Resource Type Dataset
Metadata Created Date March 8, 2017
Metadata Updated Date March 8, 2017
Publisher Federal Laboratory Consortium
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Flcbusinessurl https://flcbusiness.federallabs.org/#/laboratory/3042
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