FIELD: measurement equipment.
SUBSTANCE: device includes two wedge-like bodies installed with their bases opposite to an incident flow, two recording devices of vortex formation frequencies after the bodies and a processing device, the output of which is the sensor output. Wedge-like bodies are located on one axis one above another; on upper and lower bases perpendicular to a common axis of the wedge-like bodies there installed are straightening vanes in the form of thin plates separating the vortex formation zones of the wedge-like bodies. On the upper surface of one, for example upper one, straightening vane there is a receiving opening that is connected through a pneumatic channel to the input of the pneumatic-electrical transducer (sensor) of absolute pressure, the output of which is connected to the input of the processing device. The processing device is made in the form of a computer realising both algorithms for determination of an aerodynamic angle and a true air speed and algorithms for determination of other altitude and speed parameters.
EFFECT: higher measurement accuracy.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
VORTEX SENSOR OF AERODYNAMIC ANGLE AND TRUE AIR SPEED | 2012 |
|
RU2506596C1 |
HELICOPTER AIR DATA SYSTEM | 2010 |
|
RU2427844C1 |
HELICOPTER AIR SIGNALS SYSTEM | 2018 |
|
RU2695964C1 |
LABEL SENSOR FOR AERODYNAMIC ANGLE AND TRUE AIR SPEED | 2014 |
|
RU2580208C1 |
SYSTEM TO MEASURE HELICOPTER FLIGHT LOW SPEEDS | 2009 |
|
RU2426995C1 |
LABEL SENSOR FOR AERODYNAMIC ANGLE AND TRUE AIR SPEED | 2014 |
|
RU2585126C1 |
KINEMATIC SENSOR OF AERODYNAMIC ANGLE AND TRUE AIR SPEED | 2019 |
|
RU2737518C1 |
THREE-AXIS AIRSPEED METER | 2020 |
|
RU2762539C1 |
METHOD FOR MEASUREMENT OF HELICOPTER AIR SIGNALS AND SYSTEM FOR ITS REALIZATION | 2005 |
|
RU2307357C1 |
METHOD FOR THREE-AXIS MEASUREMENT OF AIR SPEED | 2020 |
|
RU2765800C1 |
Authors
Dates
2015-07-20—Published
2014-04-21—Filed