AIRCRAFT ENGINE THRUST MEASUREMENT DEVICE Russian patent published in 2016 - IPC G01L5/13 

Abstract RU 2582492 C1

FIELD: test equipment.

SUBSTANCE: invention can be used for measuring of effective aircraft engine thrust. Device comprises meter of air flow velocity head, sensor of angle of attack, overload transducer, setter of size of matrices, three units of generation of matrices, subtractor matrices, matrix transposition unit, unit for treatment of matrix, three multiplier units of matrices, connected to each other in certain manner.

EFFECT: technical result consists in improvement of accuracy of measurements, simplified design.

1 cl, 1 dwg

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RU 2 582 492 C1

Authors

Zaets Viktor Fedorovich

Korsun Oleg Nikolaevich

Kulabukhov Vladimir Sergeevich

Tuktarev Nikolaj Alekseevich

Lysjuk Oleg Pavlovich

Poplavskij Boris Kirillovich

Dates

2016-04-27Published

2015-02-12Filed