FIELD: instrument engineering. SUBSTANCE: aerometric parameters meter operates when pressure receiver, to be oriented, is disposed as inside, and outside vertex column. Mode of measurement is identified by means of evaluation using pressure receiver angular position control and commutation unit. Angles α and β are used to characterize position of the receiver. Set of angles may be obtained according to results of flight and aerodynamic experiments, when pressure receiver is disposed inside the transit of vertex column. EFFECT: improved reliability. 4 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
HELICOPTER AIR SIGNAL SYSTEM | 2011 |
|
RU2518871C2 |
METER OF AEROMETRIC PARAMETERS OF FLYING VEHICLE | 1987 |
|
SU1559894A1 |
MEASUREMENT SYSTEM OF AIRBORNE VEHICLE ALTITUDE AND SPEED PARAMETERS | 2011 |
|
RU2477862C1 |
METHOD FOR MEASUREMENT OF HELICOPTER AIR SIGNALS AND SYSTEM FOR ITS REALIZATION | 2005 |
|
RU2307357C1 |
HELICOPTER AIR DATA SYSTEM | 2010 |
|
RU2427844C1 |
SYSTEM TO MEASURE PARAMETERS OF ATMOSPHERE DYNAMICS IN SURFACE LAYER | 2013 |
|
RU2548299C2 |
SYSTEM TO MEASURE HELICOPTER FLIGHT LOW SPEEDS | 2009 |
|
RU2426995C1 |
AIRSPEED AND YAW METER OF AIRCRAFT | 1979 |
|
SU801712A1 |
ONBOARD SYSTEM FOR MEASURING PARAMETERS OF WIND VELOCITY VECTOR DURING PARKING, TAKEOFF AND LANDING OF HELICOPTER | 2014 |
|
RU2592705C2 |
HELICOPTER AIR SIGNAL SYSTEM | 2005 |
|
RU2307358C1 |
Authors
Dates
1994-06-30—Published
1987-03-25—Filed