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5-Hole Differential Pressure Airspeed Probe

5-Hole Differential Pressure Airspeed Probe
5-Hole Differential Pressure Airspeed Probe
5-Hole Differential Pressure Airspeed Probe
5-Hole Differential Pressure Airspeed Probe
5-Hole Differential Pressure Airspeed Probe
5-Hole Differential Pressure Airspeed Probe
5-Hole Differential Pressure Airspeed Probe
The five-hole differential pressure airspeed probe is a high-performance measurement device specially designed for low-altitude aircraft, which can provide flight altitude (Hp), speed (CAS&TAS), Angle of attack (AOA), sideshow (AOS), static pressure (Ps), dynamic pressure (Qc), total atmospheric temperature (TAT) and static temperature (OAT) data for aircraft.

High altitude, low altitude, a variety of application scenarios

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Technical data

Precision parameter

Working temperature(-35~+55)℃

Qc(0~245) hPa≤0.2%FS

Ps(200~1100) hPa≤0.2%FS

AOA±30°≤±0.5°

AOS±30°≤±0.5°

Certifications & Accreditations

CNAS Laboratory Accreditation Certificate
CNAS Laboratory Accreditation Certificate
CE Certification Certificate
CE Certification Certificate
Certification of Weaponry and Equipment Quality Management System
Certification of Weaponry and Equipment Quality Management System

Product Gallery

  • 5-Hole Differential Pressure Airspeed Probe
    5-Hole Differential Pressure Airspeed Probe
  • 5-Hole Differential Pressure Airspeed Probe
    5-Hole Differential Pressure Airspeed Probe
    5-Hole Differential Pressure Airspeed Probe
    5-Hole Differential Pressure Airspeed Probe
5-Hole Differential Pressure Airspeed Probe-Model A
5-Hole Differential Pressure Airspeed Probe-Model B

5-Hole Differential Pressure Airspeed Probe

Technical advantage

AI compensation algorithm for high and low temperatures:By compensating for the temperature of the pressure sensor, the influence of temperature changes on the sensor can be eliminated to the greatest extent, ensuring more accurate measurement of the airflow pressure.
Three-dimensional non-reciprocal linear interpolation algorithm with variable Mach number:The "knowledge base" formed through extensive data training and the "expert database" accumulated over many years of experiments can precisely calculate the airflow velocity at any airflow Angle, ensuring that the airflow Angle and velocity are calculated more accurately.
Calibration capability:The first private calibration wind tunnel laboratory in China recognized by CNAS, with three wind tunnels, namely T-01, T-02 and T-03, and the wind speed range is: (0.2-30)m/s; (0.1-0.9) Mach ;(0.1-2.0) Mach.

 

Highly integrated and multi-functional in one

 

It integrates multiple functional components such as the total pressure hole, static pressure hole, heater, drainage hole, temperature sensor, pressure sensor and atmospheric temperature sensor internally, achieving a high degree of multi-functional integration.
 

Intelligent warming, cold prevention and ice melting

The adaptive PID algorithm dynamically adjusts the heating power, matching the optimal temperature rise curve with the real-time space velocity and the ambient temperature to prevent the probe from freezing or overheating and deforming. It features a wide power supply of (9~30)VDC, with a maximum heating power of 280W. It adopts PWM pulse width modulation technology, which saves 30% energy compared to traditional resistance heating.
 
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FAQs at a glance

What are the steps for calibrating pneumatic probes?
In flow field measurement, the pneumatic probe is a commonly used instrument for measuring parameters such as velocity and pressure in the flow field. To ensure the accuracy and reliability of the measurement results, the pneumatic probe needs to undergo the important operation of pneumatic probe calibration before use.
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