FIELD: device for measurement of helicopter altitude-speed parameters.
SUBSTANCE: the system has a flow-through multichannel aerometric receiver, throttled static pressure chambers and whose 2n impact pressure pipes are commented to the inputs of n differential pneumoelectric converters, where n=2.3... , whose electric measuring circuits via series-connected multiplexer and analog-to-digital converter are connected to a microprocessor, whose output servers as the output of the system of the helicopter altitude-speed flight parameters. Differential thermo anemometric gas-flow transducers may be used as pneumoelectric converters.
EFFECT: simplified embodiment of the system.
2 cl, 3 dwg
| Title | Year | Author | Number |
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| METER OF AEROMETRIC PARAMETERS OF FLYING VEHICLE | 1987 |
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RU2477862C1 |
