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Overview

Honeywell Harsh Application Aerospace Proximity Sensor, HAPS Series, Inline cylindrical flanged form factor, 2,50 mm/3,50 range, 3-wire open collector output normally closed, EN2997Y10803MN termination, no hardware.
Honeywell’s patented Harsh Application Aerospace Proximity Sensors (HAPS Series) are configurable, non-contact, hermetically sealed devices designed to sense the presence or absence of a target in harsh-duty aircraft applications. The HAPS Series provides on/off output, and can be configured with an optional health monitoring output to the host system. The technology Honeywell uses in the HAPS Series is considered an improvement on traditional ECKO (Eddy Current Killed Oscillator) topology that previously had been the standard in aerospace applications.
1PCFD3BCNN-000 Aerospace Proximity Sensors - Honeywell


Technical Specifications

Form Factor Inline, cylindrical flanged
Range Ga/Gd 2,50 mm/3,50 mm [0.098 in/0.138 in]
Electrical Output Type 3-wire, open collector output, normally closed
Termination EN2997Y10803MN
Pigtail Length not applicable
Hardware None
Weight 60 g to 150 g
Sensing Distance 4 mm max.
Sensing Face Inconel®
Outer Body Material Stainless steel
Sensor Head Diameter 13,5 mm [0.53 in]
MTBF 500,000 flight hours
Supply Voltage 12 Vdc to 28 Vdc
Supply Current <10 mA
Operating Temperature -55 °C to 115 °C [-67 °F to 239 °F]
Target Response Time 5 ms
Dielectric Strength 500 Vdc/500 Vac for 1 minute
Insulation Resistance 200 mOhm min. at 50 Vdc
Target Material 17-4 PH stainless steel heat treated to condition H1025
Target Dimension Rectangular target of 25 mm x 18 mm x 3 mm

Technical Specifications

Form Factor Inline, cylindrical flanged
Range Ga/Gd 2,50 mm/3,50 mm [0.098 in/0.138 in]
Electrical Output Type 3-wire, open collector output, normally closed
Termination EN2997Y10803MN
Pigtail Length not applicable
Hardware None
Weight 60 g to 150 g
Sensing Distance 4 mm max.
Sensing Face Inconel®
Outer Body Material Stainless steel
Sensor Head Diameter 13,5 mm [0.53 in]
MTBF 500,000 flight hours
Supply Voltage 12 Vdc to 28 Vdc
Supply Current <10 mA
Operating Temperature -55 °C to 115 °C [-67 °F to 239 °F]
Target Response Time 5 ms
Dielectric Strength 500 Vdc/500 Vac for 1 minute
Insulation Resistance 200 mOhm min. at 50 Vdc
Target Material 17-4 PH stainless steel heat treated to condition H1025
Target Dimension Rectangular target of 25 mm x 18 mm x 3 mm

Documents

TITLE DOCUMENT TYPE LANGUAGE SIZE
GAPS & HAPS Series Aerospace Proximity Sensors Datasheet English 3MB
GAPS & HAPS Series Proximity Sensors Installation Instructions English 569KB
Position Sensors Range Guide Product Range Guide English 2MB
GAPS & HAPS Series Proximity Sensors for Aerospace Applications Application Note English 1MB
Aerospace and Defense Product Range Guide Product Range Guide English 18MB
GAPS & HAPS Comparative Infographic Application Note English 4MB
1PCFD3BCNN-000 CAD Drawing CAD Model -- 255KB
White Paper: Do You Know When Your Proximity Sensor Is Sick? White Paper English 600KB

Product Features

  • Industry-leading indirect lightning and dielectric ruggedness: Meets the increased requirements of today’s composite aircraft and most challenging applications including landing gear, thrust reversers, and flight controls
  • Superior vibration ruggedness: Capable of withstanding extremely high vibration applications
  • Environmentally rugged: Fully hermetic packages provide long-term reliability in very harsh environments by eliminating the potential for contamination of the sensor from the application environment. In addition, Honeywell has developed an innovative method to hermetically seal wire-lead (pigtail) configurations
  • Integral Health Monitoring Capability: Optional third output state to indicate the health of the sensor (whether it is healthy or failed). Reduces maintenance time, reduces delayed flights, and lowers overall maintenance cost across the life of the aircraft
  • Non-contact design: Utilizes non-contact technology to sense the presence or absence of a target regardless of the dirty, harsh environment in which it is placed, eliminating mechanical failure mechanisms, reducing wear, minimizing downtime, increasing durability, and increasing reliability

Applications

  • Harsh aircraft applications, including:
  • Thrust reverser actuation system (TRAS) (stowed or deployed status)
  • Valves
  • Engines
  • Actuators
  • Nacelle
  • Canopies

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