LABEL SENSOR FOR AERODYNAMIC ANGLE AND AIR SPEED Russian patent published in 2012 - IPC G01P5/14 

Abstract RU 2445634 C2

FIELD: physics.

SUBSTANCE: device has an ion label generator, a system of receiving electrodes, a channel for detecting ion labels and a measuring circuit for generating output signals. The system of receiving electrodes is in form of circular metal plates lying equidistant on a circle with the centre at the point of generation of ion labels and are placed directly under the opening in the metal plate - "mask", which is mounted on a dielectric plate, where the receiving electrodes are connected to inputs of preamplifiers of the channel for detecting ion labels and are merged into autonomous modules, having a screening housing. Outputs of the preamplifiers are connected through analogue switches (commutator switches) and adders to inputs of differential amplifiers of the channel for detecting ion labels.

EFFECT: wider measuring range for the aerodynamic angle, ensuring high aerodynamic angle resolution without increasing the number of receiving electrodes and size of the system of receiving electrodes, possibility of simultaneous measurement of the value and the direction angle of the air velocity vector of aircraft without putting protruding aerometric receivers into the incoming air stream.

6 cl, 6 dwg

Similar patents RU2445634C2

Title Year Author Number
KINEMATIC SENSOR OF AERODYNAMIC ANGLE AND TRUE AIR SPEED 2019
  • Soldatkin Vladimir Mikhajlovich
  • Soldatkin Vyacheslav Vladimirovich
  • Nikitin Aleksandr Vladimirovich
  • Efremova Elena Sergeevna
  • Ariskin Evgenij Olegovich
RU2737518C1
LABEL SENSOR FOR AERODYNAMIC ANGLE AND TRUE AIR SPEED 2014
  • Soldatkin Vladimir Mikhajlovich
  • Ganeev Farid Akhatovich
  • Soldatkina Elena Sergeevna
  • Makarov Nikolaj Nikolaevich
  • Derevjankin Valerij Petrovich
  • Krylov Dmitrij Lvovich
RU2580208C1
LABEL SENSOR FOR AERODYNAMIC ANGLE AND TRUE AIR SPEED 2014
  • Soldatkin Vladimir Mikhajlovich
  • Ganeev Farid Akhatovich
  • Urazbakhtin Ildar Rasimovich
  • Makarov Nikolaj Nikolaevich
  • Derevyankin Valerij Petrovich
  • Krylov Dmitrij Lvovich
RU2585126C1
ONBOARD SYSTEM OF MEASURING PARAMETERS OF WIND VELOCITY VECTOR AT STATION, TAKEOFF AND LANDING HELICOPTER 2014
  • Soldatkin Vladimir Mikhajlovich
  • Soldatkin Vyacheslav Vladimirovich
  • Ganeev Farid Akhatovich
  • Ariskin Evgenij Olegovich
  • Makarov Nikolaj Nikolaevich
  • Derevyankin Valerij Petrovich
  • Kuznetsov Oleg Igorevich
  • Istomin Dmitrij Aleksandrovich
RU2587389C1
HELICOPTER AIR SIGNALS SYSTEM 2018
  • Soldatkin Vladimir Mikhajlovich
  • Soldatkin Vyacheslav Vladimirovich
  • Nikitin Aleksandr Vladimirovich
  • Soldatkin Ruslan Vyacheslavovich
RU2695964C1
MEASUREMENT SYSTEM OF AIRBORNE VEHICLE ALTITUDE AND SPEED PARAMETERS 2011
  • Porunov Aleksandr Azikovich
  • Galjautdinova Adelja Nailevna
  • Tjurina Marina Mikhajlovna
  • Soldatkin Vladimir Mikhajlovich
  • Porunov Nikolaj Aleksandrovich
RU2477862C1
DEVICE FOR MEASURING PARAMETERS OF AIR FLUX 1982
  • Ivanchuk A.S.
  • Bal'Tser S.K.
  • Kostikov N.V.
  • Kuralesin V.A.
  • Makukha O.A.
  • Sidorov I.N.
  • Soldatkin V.M.
  • Ferenets V.A.
SU1190731A1
DEVICE FOR MEASURING KINEMATIC PARAMETERS OF AIR FLUX 1982
  • Ivanchuk A.S.
  • Ganeev F.A.
  • Soldatkin V.M.
  • Ferenets V.A.
SU1048922A1
PICKUP OF AERODYNAMIC ANGLES 1981
  • Arzamastsev Ju.A.
  • Ganeev F.A.
  • Geras'Kin V.E.
  • Gusev V.V.
  • Kljuev G.I.
  • Nikol'Skij S.A.
  • Olin V.N.
  • Soldatkin V.M.
  • Ferenets V.A.
SU1080613A1
METHOD FOR MEASURING RATE OF FLOW OF GAS OR LIQUID AND DEVICE TO ITS REALIZATION 1994
  • Abrosimov A.A.
  • Ferenets A.V.
RU2084831C1

RU 2 445 634 C2

Authors

Ganeev Farid Akhatovich

Soldatkin Vladimir Mikhajlovich

Urazbakhtin Il'Dar Rasimovich

Makarov Nikolaj Nikolaevich

Kozhevnikov Viktor Ivanovich

Dates

2012-03-20Published

2010-05-05Filed