FIELD: aeronautical engineering; flying laboratories for testing and development of gas-turbine engines of flying vehicles.
SUBSTANCE: proposed laboratory includes aircraft with shoulder wing, three standard engines and power plant under test; power plant includes pylon, cowled experimental engine with air intake. Laboratory is provided with streamlined adapter module which is provided with several attachment units for securing the experimental engines on external surface. Adapter module is mounted between pylon and cowled experimental engine.
EFFECT: reduction of time, labor consumption.
4 dwg
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Authors
Dates
2004-08-10—Published
2003-05-05—Filed