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Anemometer

A precision meteorological instrument that measures wind speed and direction, providing critical data for air traffic control, weather reporting, and aerodrome operations. Available in cup, propeller, and ultrasonic variants with varying accuracy and maintenance requirements.

Anemometer

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Overview

What Is It?

An Anemometer is a meteorological instrument used to measure wind speed and, in many configurations, wind direction. At airfields, anemometers are essential for providing real-time wind data to pilots, air traffic controllers, and weather forecasters. The data is used to determine runway selection, approach and departure procedures, and to issue weather warnings. Modern anemometers use electronic sensors (cups, propellers, or ultrasonic transducers) that convert wind motion into electrical signals that are processed and displayed in knots, metres per second, or kilometres per hour.

Purpose

Purpose & Function

Wind data exists because the direction and strength of the wind is one of the most operationally consequential variables at any airport — it determines which runway is safest to use, whether a crosswind exceeds an aircraft's certified limits, and whether departures or arrivals should be delayed until conditions ease. Without accurate, continuously updated wind measurement, both controllers assigning runways and pilots planning an approach or takeoff would be working from stale or estimated information in a situation where wind can shift meaningfully within minutes.

Because a tailwind or excessive crosswind component can compromise an aircraft's ability to land or take off within available runway length, or make directional control difficult during the roll, the anemometer's data directly underpins some of the most fundamental safety decisions made at an airport, from runway selection down to individual go-around calls.

Application

Where Is It Used?

Installed at airfields as part of the meteorological observation system. Typically located near the runway midpoint or at the touchdown zone, mounted on a mast or tower at a height of 10 metres above ground level (as recommended by ICAO and WMO). Used for aerodrome weather reporting, ATC wind information, and as input to automated systems such as RVR and weather displays. Also used at heliports, offshore platforms, and remote airstrips where wind data is critical for safe operations.

Placement

Installation & Location

Mounted on a dedicated meteorological mast, or a cross-arm on a shared wind mast, sited so the sensor sits in open, unobstructed air. WMO and ICAO siting guidance calls for clearance from buildings, trees, and other masts of roughly ten times the height of the obstruction, to avoid turbulence and shadowing effects on the readings. Standard exposure height is 10 m above ground level (or above surrounding terrain on undulating ground), though a lower height is sometimes used near the runway touchdown zone where local practice or approach surface constraints apply. The mast is set on a concrete foundation with a lightning air terminal and dedicated earthing, since a structure of this height is itself a lightning risk in open terrain. Signal and power cabling run underground in duct back to the meteorological equipment shelter, and the sensor head is aligned to true (or magnetic) north during commissioning, since direction accuracy depends entirely on this reference being set correctly.

Function

How Does It Work?

A cup anemometer uses three or four hemispherical cups mounted on a vertical shaft; wind causes the cups to rotate, and the rotational speed is proportional to wind speed. A vane (wind vane) is typically co-located to measure wind direction. Propeller anemometers use a horizontal-axis propeller that aligns with the wind. Ultrasonic anemometers use sound waves to measure wind speed and direction with no moving parts, offering higher reliability and lower maintenance. The instrument outputs electrical signals (analogue voltage, current, or digital data) that are processed by a display unit or fed into the airfield weather system.

Architecture

System Architecture & Control Logic

Unlike the airfield ground lighting fixtures elsewhere in this library, the anemometer has no relationship to the constant current series circuit — it is a data source, not a load, and sits instead within the airfield's automated weather observation system. The sensor head's raw output (analogue voltage/current for cup and propeller types, or a digital serial stream for ultrasonic types) is passed to a signal conditioning unit or transducer at the mast base, then on to a data logger or data collection platform (DCP) that samples, timestamps, and averages the readings (typically as a 2-minute or 10-minute running mean, per ICAO/WMO reporting convention). The DCP reports over a wired or fibre link to the central AWOS/ASOS processor, which merges it with other sensor inputs to generate the wind entries in METAR/TAF products, the live wind readout on the controller's display, and ATIS broadcasts. Because each anemometer is individually addressed on this data network rather than sharing a current loop, a fault — a stuck cup, an iced vane, a stale or out-of-range reading, or a heater failure on de-iced models — is reported against that specific sensor ID, not as an ambiguous loop-wide fault requiring further sectionalised testing. Where multiple anemometers are deployed along a single runway (e.g., touchdown, midpoint, and stop-end for a long or CAT II/III runway), the AWOS processor reports each position's wind separately so controllers can identify localised wind shear or gust differences between the ends.

Measurement Logic

Three Ways to Sense Wind

Cup Rotation Speed RPM ∝ wind speed Propeller Wind Aligns horizontal axis to wind Spin Rate Proportional to speed Ultrasonic Sound pulses, both directions No moving parts Time-of-Flight Diff. Speed + direction Electrical Signal Output To airfield weather system
Mechanical / signal path
Return sound pulse
Construction

Physical Construction

Anemometers are built around a weatherproof sensor head mounted on a mast or boom, with cup, propeller, or ultrasonic transducer elements fabricated from corrosion-resistant materials such as anodised aluminium, stainless steel, or UV-stabilised composite to withstand continuous outdoor exposure and, in cup or propeller types, high-speed rotation over years of service. The sensor head bearings are sealed, low-friction units, often with heating elements built into the housing or shaft to prevent icing that would otherwise stall the moving parts or bias readings in freezing conditions. The electronics enclosure, whether integral to the sensor head or mounted separately at the mast base, is potted or gasket-sealed to an IP65/IP67 rating and connects via shielded, weather-rated cable to the signal conditioning and output interface. The mounting mast itself is typically a rigid, corrosion-resistant pole set at the standard 10 m reference height, with the sensor head aligned clear of nearby obstructions and turbulence sources so wind measurements remain representative of the open-air flow. Cable glands, connectors, and junction boxes are all rated for continuous outdoor service and lightning-prone siting.

Specification

Technical Parameters

ParameterTypical Value
Measurement Range (Speed)0.2 – 75 m/s (0.4 – 167 mph)
Measurement Range (Direction)0 – 360° (with vane or ultrasonic)
Accuracy (Speed)±2% or ±0.2 m/s (whichever is greater)
Accuracy (Direction)±2° – ±5° depending on type
Startup Threshold0.2 – 0.5 m/s (cup type)
Mounting Height10 m above ground (ICAO / WMO standard)
Output Signal4–20 mA, 0–10V, RS-232, RS-485, SDI-12, or NMEA
Protection ClassIP65 / IP67 (weatherproof)
Operating Temperature-40°C to +70°C
Power Supply

Electrical Requirements

RequirementTypical Value
Power Supply12V/24V DC or 230V AC via AWOS/ASOS power unit; solar/battery for remote sites
Power Consumption< 5W typical (higher when heating element is active)
Heating Element (De-icing)Optional 20–50W element on the cup/vane or ultrasonic transducers to prevent ice-related error
Signal CablingShielded twisted-pair or RS-485/SDI-12 data cable, run separately from AC power
Cable RoutingScreened multicore, direct-burial or conduit-routed from mast base to met data logger
Lightning/Surge ProtectionSurge arrestor at the mast base and sensor bonded to the mast lightning-protection system
Earthing/GroundingMast structure and sensor body bonded to site earth grid
Data IntegrationInterfaced to the AWOS/ASOS data logger or airfield meteorological system
Compliance

Applicable Standards

ICAO Annex 3

Meteorological service requirements for international air navigation

WMO No. 8 (Guide to Instruments)

Wind measurement instrument specifications and installation

FAA AC 150/5220-16

Airport weather observation systems (AWOS) requirements

ISO 17713

Meteorological wind measurement standards

Prerequisites

Installation Requirements

Mast Foundation & Earthing
Civil

Set the mast on a concrete foundation with a lightning air terminal and dedicated earthing, since a structure of this height is itself a lightning risk in open terrain.

Mounting Height & Siting Clearance
Civil

Position the sensor at the standard 10 m reference height with clearance from buildings, trees, and other masts of roughly ten times the obstruction height to avoid turbulence and shadowing.

Cable Route to Equipment Shelter
Electrical

Run signal and power cabling underground in duct back to the meteorological equipment shelter, keeping the run separate from unrelated high-voltage circuits.

True North Alignment
Mechanical

Align the sensor head to true (or magnetic) north during installation, since direction accuracy depends entirely on this reference being set correctly.

Heater Circuit Wiring
Electrical

On de-iced models, terminate the heater supply on its own protected circuit so anti-icing function can be verified and maintained independently of the signal path.

Rotor/Vane Assembly Fitting
Mechanical

Fit the cup, propeller, or vane assembly to the sealed bearing so it rotates freely with minimal starting torque and no binding across its full range.

Data Interface Configuration
Electrical

Configure the sensor's output protocol and network address so its readings are individually identifiable to the AWOS/ASOS processor.

Pre-Energisation Sign-off
Documentation

Record mast position, cable route, and north-reference alignment as-built before the sensor is accepted for commissioning.

Verification

Testing & Commissioning

Insulation Resistance & Continuity Test
Pre-Energisation

Megger-test power cabling and verify signal cable continuity before the sensor is energised, ruling out faults introduced during installation.

Power-Up & Self-Test
Energisation

Energise the sensor and confirm it passes its internal self-diagnostic routine, with cup, propeller, or ultrasonic transducer electronics all reporting healthy.

Mechanical Free-Rotation Check
Functional Test

For cup and propeller types, confirm the rotor spins freely with minimal starting torque and the vane moves without binding across its full range.

Wind Speed Calibration Verification
Functional Test

Verify wind speed output against a portable calibrator or reference anemometer across the operating range before the sensor is accepted.

Wind Direction Alignment (True North Referencing)
Functional Test

Confirm the sensor's zero-direction reference is correctly aligned to true north using a survey-grade compass or sighting method.

Heater Function Test
Functional Test

Where fitted, verify the anti-icing heater activates correctly to confirm it will keep moving parts and transducers free of ice buildup.

Output & Communications Verification
Final Acceptance

Confirm wind speed and direction data reports correctly to the AWOS or ATC display via the sensor's communication interface before handover.

Documentation & As-Built Sign-off
Final Acceptance

Record calibration, alignment, and communications test results alongside as-built position in the commissioning dossier for handover.

Upkeep

Inspection & Maintenance

Calibration Check
Annual

Test speed and direction readings against a certified reference standard to confirm the sensor still meets the ±2% accuracy requirement for aviation use.

Bearing & Starting Threshold Test
Annual

On cup or propeller types, check bearing friction and starting threshold, replacing bearings on a 2-3 year cycle before wear degrades low-wind accuracy.

Visual Inspection
Quarterly

Check cups, propeller, or ultrasonic transducers for physical damage, corrosion, or debris that could bias readings or increase mechanical drag.

Heater Function Test (if fitted)
Pre-winter

Verify de-icing heaters activate and clear ice or snow buildup correctly before winter operations begin, since icing can stall moving parts or block ultrasonic paths.

Lightning Protection & Grounding Check
Annual

Inspect surge protection, lightning arrestors, and grounding connections on the mast, since elevated installations are especially exposed to strikes and induced surges.

Mast & Mounting Inspection
Annual

Check the 10m mast, guy wires, and mounting hardware for corrosion or looseness that could introduce vibration or tilt affecting measurement accuracy.

Cable & Signal Output Test
Annual

Verify the output signal (4-20mA, RS-232/485, SDI-12, or NMEA) is clean and free of noise or intermittent dropouts along the full cable run.

Field Notes

Common Field Issues

Bearing Wear and Friction

Mechanical anemometers (cup and propeller types) rely on bearings that wear over time, increasing starting threshold and reducing accuracy. Regular calibration and bearing replacement (typically every 2–3 years) is essential to maintain performance.

Icing and Snow Accumulation

In cold climates, ice can form on the cups or propeller, affecting measurements. Heated anemometers are available for these conditions. Regular visual inspection and de-icing procedures are recommended during winter operations.

Lightning and Surge Damage

Anemometers mounted on tall masts are vulnerable to lightning strikes and induced surges. Proper surge protection, grounding, and lightning arrestors are critical to protect the instrument and the data acquisition system.

Calibration Drift

Electronic sensors can drift over time, affecting accuracy. Regular calibration against a reference standard (at least annually) is required to ensure the anemometer meets the ±2% accuracy specification for aviation use.

Diagnostics

Troubleshooting Guide

No Output / Signal Loss
Likely Cause
Broken or corroded cable/connector between the sensor head and the data acquisition unit, or a failed power supply to the transducer.
Diagnostic Steps
Check power at the sensor head; test cable continuity and connector integrity end to end; confirm the data acquisition system is polling the correct port/address.
Corrective Action
Repair or replace the damaged cable/connector, restore power to the sensor, and confirm live readings are reaching the AWOS/ALCMS display.
Reading Stuck at Zero or High Starting Threshold
Likely Cause
Worn bearings on a cup or propeller anemometer are increasing friction and preventing rotation at low wind speeds.
Diagnostic Steps
Manually spin the rotor and check for roughness or drag; compare starting threshold against the manufacturer's specification; inspect bearings for wear or contamination.
Corrective Action
Replace worn bearings (typically every 2–3 years) and re-calibrate the sensor to confirm it meets the starting threshold specification.
Erratic or Noisy Readings
Likely Cause
Electrical interference on the signal cable, a loose connector, or a partially failed transducer producing unstable output.
Diagnostic Steps
Inspect and re-seat all connectors; check cable routing for proximity to noise sources; compare output against a reference anemometer under the same conditions.
Corrective Action
Re-terminate loose connections, reroute or shield the signal cable if interference is confirmed, and replace the transducer if it fails the reference comparison.
Iced-Over Sensor or Frozen Rotor
Likely Cause
Ice or snow accumulation on the cups/propeller in cold conditions, or a failed heating element on a heated anemometer.
Diagnostic Steps
Visually inspect for ice buildup; on heated units, verify heater power draw and surface temperature at the sensor.
Corrective Action
De-ice the sensor per procedure, and repair or replace a failed heating element ahead of the next cold-weather period.
Reading Drift Versus Reference Standard
Likely Cause
Gradual electronic or mechanical drift has pushed the sensor outside the ±2% accuracy specification required for aviation use.
Diagnostic Steps
Run a calibration check against a certified reference standard; review calibration history for a trend indicating progressive drift.
Corrective Action
Recalibrate the sensor to bring it back within specification, or replace the transducer if it cannot be brought back into tolerance.
Instrument Damaged After a Storm
Likely Cause
A lightning strike or induced surge on the mast has damaged the sensor electronics or the data acquisition interface.
Diagnostic Steps
Inspect the sensor, mast grounding, and surge arrestors for visible damage; test the data acquisition interface for a blown input stage.
Corrective Action
Replace the damaged sensor or interface card, verify grounding and surge protection are intact, and confirm lightning arrestors are rated correctly before re-energising.
Reliability

Failure Modes & Root Causes

Bearing Wear or Seizure
Medium Severity
Root Cause
Progressive wear of the cup/propeller bearings from continuous rotation, or contamination and dried-out lubrication after prolonged exposure.
Effect
Increased starting threshold or complete loss of rotation, causing under-reading or a stuck-at-zero wind speed reading.
Detection Method
Manual spin test for roughness or drag, and comparison of the starting threshold against the manufacturer's specification during scheduled calibration.
Transducer / Electronic Module Failure
High Severity
Root Cause
Component aging in the signal-conditioning electronics, a partial internal short, or thermal stress inside the sensor head.
Effect
Erratic, noisy, or unstable output even though the rotor or vane is moving freely.
Detection Method
Comparison of output against a reference anemometer under matching conditions, and inspection for unstable readings unrelated to actual wind behaviour.
Cable / Connector Damage
High Severity
Root Cause
Corrosion at the connector interface, cable jacket abrasion from mast movement, or a broken conductor from repeated flexing.
Effect
Total signal loss or intermittent dropout at the data acquisition unit despite the sensor head itself being functional.
Detection Method
Cable continuity testing end to end, connector inspection for corrosion, and confirmation that power is present at the sensor head.
Heating Element Failure
Medium Severity
Root Cause
Element burnout, a blown fuse in the heater circuit, or a failed thermostat/control circuit on heated anemometer variants.
Effect
Ice or snow accumulates on the cups or propeller in cold conditions, causing under-reading or a frozen, non-rotating sensor.
Detection Method
Heater power-draw verification and surface temperature check at the sensor during cold-weather inspection.
Lightning / Surge Damage
High Severity
Root Cause
A direct or induced lightning strike on the mast overwhelming the sensor's surge protection and grounding path.
Effect
Sudden, complete loss of output or physical damage to the sensor electronics and data acquisition interface after a storm.
Detection Method
Post-storm inspection of the sensor, mast grounding, and surge arrestors, plus a bench test of the data acquisition interface for a blown input stage.
Calibration Drift
Low Severity
Root Cause
Gradual electronic or mechanical drift in the transducer over months to years of continuous operation.
Effect
Readings fall outside the ±2% accuracy specification required for aviation use, even though the sensor otherwise operates normally.
Detection Method
Scheduled calibration checks against a certified reference standard, with calibration history reviewed for a progressive trend.
Precautions

Safety & Operational Notes

Electrical Isolation Before Servicing
Electrical Safety

De-energise the sensor supply and, separately, the de-icing heater circuit at the AWOS/ASOS power unit before opening the housing or disconnecting cable, and verify zero energy at the sensor since the heater circuit is independently fed.

Rotor / Propeller Pinch Hazard
Mechanical

Cup wheels and propellers can spin freely in ambient wind even with the sensor powered down; secure or restrain the rotor before hands-on work and keep fingers clear of the rotating assembly.

Hot Heating Element
Personnel Safety

Allow the de-icing heater on the cup/vane or ultrasonic transducers to cool before handling after active operation, particularly in winter conditions where the element may have been running continuously.

Storm and Lightning Exposure
Electrical Safety

Avoid mast-top work during an electrical storm or high wind; confirm the mast grounding and surge arrestors are intact before returning the sensor to service after any lightning activity.

Airside Work Coordination
Operational

Work on masts within the aerodrome's obstacle-limitation surfaces or movement area requires ATC/airside coordination and a NOTAM where wind data will be unavailable, with vehicle access following the aerodrome's safety management procedures.

Calibration Reference Integrity
Operational

Handle the certified reference wind source carefully during calibration checks and keep its own calibration traceable, since a drifted reference can mask real sensor drift rather than reveal it.

Restore to Compliant State
Compliance

Confirm the sensor is reporting within its ±2% accuracy specification and the heater circuit is functioning before closing out maintenance, and cancel the associated NOTAM only once wind data is confirmed reliable.

Field Insight

Engineering & Expert Notes

Bearing Icing Shows Up as a Reading, Not an Alarm
Calibration

Light icing on cup or propeller bearings tends to under-report wind speed rather than stop the instrument outright, which is a more dangerous failure mode than a clear fault; verify heater operation ahead of icing season instead of waiting for a functional test in mild weather.

Bearing Wear Degrades Low-Speed Response First
Maintenance

A cup anemometer nearing the end of its bearing life typically shows an increased starting threshold, under-reporting light winds while still tracking strong winds reasonably well; trend low-speed readings specifically rather than judging condition from high-wind accuracy alone.

Siting Can Degrade Without Any Fault at the Instrument
Siting

New structures, vegetation growth, or even seasonal foliage near the mast can disturb airflow enough to bias readings while the anemometer itself remains perfectly calibrated; review the surrounding exposure at each major inspection, not just the instrument.

Ultrasonic Transducers Are Vulnerable to Small Obstructions
Troubleshooting

Insects, spider webs, or debris bridging an ultrasonic transducer path cause intermittent dropouts or erratic readings that can look like an electronic fault; a visual check of the transducer faces should be a distinct step from any electrical diagnostic.

Cross-Check Against a Second Source, Not Just Self-Test
Verification

An anemometer's internal self-diagnostic can pass while the sensor has drifted slightly out of calibration; compare readings against a redundant anemometer or nearby wind sensor periodically to catch a slow drift that a self-test alone would miss.

Direction Vane Alignment Errors Are Easy to Overlook
Installation

On combined speed/direction units, a vane or reference mark that's a few degrees off true north introduces a systematic direction bias that doesn't show up as a fault anywhere in diagnostics; verify north alignment specifically after any remount or mast work.

Quick Answers

Frequently Asked Questions

Short answers about the anemometer: what it is, how it works, specifications, standards, maintenance and common faults.

Q1What is an anemometer at an airfield?

An anemometer is a meteorological instrument that measures wind speed and, in many configurations, wind direction. At airfields it supplies real-time wind data to pilots, air traffic controllers and forecasters for runway selection, approach and departure procedures and weather warnings.

Q2What types of anemometer are used?

The three main types are cup, propeller and ultrasonic. A cup anemometer uses rotating hemispherical cups whose speed is proportional to wind speed, with a co-located vane for direction. A propeller type uses a horizontal-axis propeller that aligns with the wind. An ultrasonic type uses sound waves with no moving parts, offering higher reliability and lower maintenance.

Q3Why does wind measurement matter at an airport?

Wind determines which runway is safest, whether a crosswind exceeds an aircraft's certified limits, and whether departures or arrivals should be delayed. A tailwind or excessive crosswind can compromise landing or take-off performance or directional control, so accurate, continuously updated data underpins basic safety decisions.

Q4Where should an anemometer be installed?

Typically near the runway midpoint or touchdown zone, on a dedicated mast at 10 m above ground level per ICAO and WMO guidance. Siting guidance calls for clearance from buildings, trees and other masts of roughly ten times the obstruction height. The mast needs a lightning air terminal and dedicated earthing, and the sensor head is aligned to north during commissioning.

Q5How accurate is an anemometer?

Typical measurement range is 0.2 m/s to 75 m/s with speed accuracy of ±2% or ±0.2 m/s, whichever is greater. Direction accuracy is typically ±2° to ±5° depending on type, and cup types have a startup threshold of about 0.2 m/s to 0.5 m/s.

Q6How is an anemometer connected and powered?

Outputs include 4-20 mA, 0-10 V, RS-232, RS-485, SDI-12 or NMEA. Power is typically 12 V or 24 V DC, or 230 V AC via the AWOS/ASOS power unit, with solar or battery for remote sites. Consumption is typically under 5 W, higher when an optional 20 W to 50 W de-icing heater is active.

Q7How does anemometer data reach controllers and pilots?

The sensor output goes through a signal conditioning unit at the mast base to a data logger or data collection platform, which typically averages readings as a 2-minute or 10-minute running mean. The AWOS/ASOS processor then feeds METAR/TAF products, the controller's wind display and ATIS broadcasts. The anemometer is not part of the constant current series circuit.

Q8Which standards apply to anemometers?

The main references are ICAO Annex 3, WMO Guide to Instruments No. 8, FAA AC 150/5220-16 (AWOS) and ISO 17713. Always verify the current edition and your aerodrome's approved requirements.

Q9How often should an anemometer be inspected and calibrated?

Typical intervals are quarterly for visual inspection, annual for calibration, bearing and starting threshold tests, lightning protection and grounding, mast and mounting, and cable and signal output checks, plus a heater function test before winter where fitted. Your airport's approved maintenance programme takes precedence.

Q10What are the common problems with anemometers?

Common problems are bearing wear and friction, icing and snow accumulation, lightning and surge damage, and calibration drift. Symptoms include no output, a reading stuck at zero or a high starting threshold, erratic readings, or a frozen rotor.

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