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Angle of Attack (AOA) Systems

Angle of Attack (AOA) Systems

Angle of Attack (AOA) Systems

Product catalog summary
Introduction
Precise and reliable measurement of the Angle of Attack (AOA) from takeoff to landing is crucial for improving aircraft performance and ensuring a safe operating margin above stall speed. The AOA is the angle between the wing chordline and the airflow direction. Maximum lift is achieved at a high AOA, but if the angle becomes too large, a stall occurs due to disrupted airflow and insufficient lift.

Angle of Attack (AOA) Systems
AOA systems are essential for monitoring and displaying the AOA to pilots. These systems include various sensors and transmitters designed to provide accurate AOA readings under different conditions.

Model 0012 AOA Transmitter
This model is designed for wing mounting on various aircraft types. It features a pivoting swept-vane element and can be equipped with thermostatically-regulated heaters for all-weather service. It is suitable for aircraft ranging from turboprops to supersonic fighters.
  • Specifications: Operating range: +5°F to +149°F (-15°C to +65°C), Weight: 1.25 lb. (567 g), Output: Potentiometer, Heater Power: 425 watts.

Model 0861 AOA Transmitter
This transmitter offers high reliability and low maintenance. It features a patented swept tapered vane for minimal aerodynamic drag and improved low air-speed sensitivity. It is electrically de-iced and does not require thermostats.
  • Specifications: User-specified operating range, Weight: 3 lb. (1.4 kg), Output: Synchro or resolver, RVDT or potentiometer, Heater Power: 115 volts, 400 Hz, Certification: TSO-C54.

Model 0020 Electronic Signal Conditioning Module
This module provides regulated power to AOA transmitters and processes signals for controlling indicators and stall warning devices. It features modular electronics for easy servicing.
  • Specifications: Operating temperature: -65°F to +160°F (-54°C to +71°C), Weight: 3 lb. (1.4 g), Power: 10 watts max.

Model 0031 Approach Indexer
This device provides a heads-up display of AOA information during approach and landing. It uses color-coded symbols to indicate approach speed and operates from the same AOA signal as the indicator.
  • Specifications: Lighting: 5 VDC at 1.5 watts max, Case: Standard 2 in. (5.1 cm) flanged.

Model 0032 and 0030 AOA Indicators
These indicators provide pilots with accurate AOA displays for various aircraft configurations. They are essential for calibrating AOA systems and ensuring accurate stall margin displays.
  • Model 0032: Includes AOA computer and indexer for calibration and display.
  • Model 0030: Displays cruise, takeoff, approach, stall warning, and stall markings.

State-of-the-Art Testing Capabilities
UTC Aerospace Systems has advanced icing wind tunnels for testing air data products. These facilities meet stringent icing requirements and optimize design performance across various flight conditions.

Enhanced Anti-Icing Capability
Accurate AOA measurement in all conditions is vital for performance and safety. New sensor technology effectively manages moisture content, ensuring reliable AOA sensing throughout the flight envelope.
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Catalog excerpts

Angle of Attack (AOA) Systems-1

Angle of Attack (AOA) Systems Precise, reliable measurement and display of Angle of Attack (AOA) from takeoff to landing can substantially improve aircraft performance as well as assure a safe operating margin above stall speed. Angle of attack is defined as the angle formed between the wing chordline and the direction of air flowing past the wing. At any specific AOA, the airflow over some percentage of the wing surface will generate lift as well as some amount of drag. Maximum lift is usually obtained at a relatively high angle. Where ingenuity takes off™ Stall is defined as the condition which arises when the angle grows so large that the flow is completely disrupted and not enough lift is generated to overcome the weight of the aircraft. This AOA, the stall angle, is constant for a particular aircraft, although various wing designs stall at differing angles. The amount of useful lift and drag generated by any wing at some specific AOA will depend upon the influence of such variables as the wing geometry, density altitude, aircraft gross weight and velocity. However, the ratio of lift to drag coefficients at a given angle remains constant. Therefore, the theoretically ideal ratio of lift and drag coefficients for any flight maneuver will always be found at the same AOA under all speeds or load conditions.

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Angle of Attack (AOA) Systems-2

Angle of Attack (AOA) Sensors Model 0012 AOA Transmitter This precision flow angle sensor is specifically suited for wing mounting on a conventional single-engine or multi-engine aircraft where a suitable fuselage location cannot be found. It features a pivoting swept-vane element extended on a boom from the wing’s leading edge, where it’s free of prop wash or other flow disturbances. For all-weather service, Model 0012 transmitters can be furnished with thermostaticallyregulated, 28-volt heaters for the vane, boom and nose cone. These heaters meet or exceed military specifications for de-icing...

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Angle of Attack (AOA) Systems-3

Model 0020 Electronic Signal Conditioning Module This module, when used with either Model 0012 or Model 0861 AOA transmitters, supplies regulated power to transmitter potentiometers and internal circuitry which processes transmitter signals. Model 0020 can be specified to have outputs for controlling a number of indicators, indexes and stall warning devices. Model 0020 operates on 28 VDC power and features modular, plug-in electronics for easy servicing. Circuitry for flap position inputs and a press-to-test function are optional. Specifications Temperature Limits Operating -65°F to +160°F (-54°C...

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Angle of Attack (AOA) Systems-4

Enhanced Anti-Icing Capability Accurate Angle of Attack (AOA) measurement in all environmental conditions is important to maintain performance and safety. EASA updates to CS 25 now require AOA sensors to operate successfully in the newly defined ice crystal requirements, commonly referred to as Appendix P from CS 25 (similar to Appendix D from FAR 33). Patented AOA sensor technology has been developed to effectively manage all types of moisture content without impacting sensing capability. AOA can be sensed throughout the flight envelope with minimal added power. New fixed wing platforms and...

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