Liquid Controls Group; a Unit of IDEX Corporation Differential Pressure Sensor (ΔP)

Description
The differential pressure transducer monitors the differential pressure (pressure drop) between a point immediately upstream and a point immediately downstream of the full flow fuel monitor, water coalescer, or other device typically applied in aviation fueling systems. The maximum differential pressure is observed during the fuel delivery is electronically input into the LectroCount® LCR-ll® Electronic Register. The highest differential pressures reached during the delivery is printed on the delivery ticked to provide a record of the maximum pressure drop. The corresponding flow rate at which this maximum differential pressure is observed is printed immediately after the differential pressure reading.
Description
The differential pressure transducer monitors the differential pressure (pressure drop) between a point immediately upstream and a point immediately downstream of the full flow fuel monitor, water coalescer, or other device typically applied in aviation fueling systems. The maximum differential pressure is observed during the fuel delivery is electronically input into the LectroCount® LCR-ll® Electronic Register. The highest differential pressures reached during the delivery is printed on the delivery ticked to provide a record of the maximum pressure drop. The corresponding flow rate at which this maximum differential pressure is observed is printed immediately after the differential pressure reading.

Suppliers

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Product
Description
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Differential Pressure Sensor - (ΔP) - Liquid Controls Group; a Unit of IDEX Corporation
Lake Bluff, IL, USA
Differential Pressure Sensor
(ΔP)
Differential Pressure Sensor (ΔP)
The differential pressure transducer monitors the differential pressure (pressure drop) between a point immediately upstream and a point immediately downstream of the full flow fuel monitor, water coalescer, or other device typically applied in aviation fueling systems. The maximum differential pressure is observed during the fuel delivery is electronically input into the LectroCount® LCR-ll® Electronic Register. The highest differential pressures reached during the delivery is printed on the delivery ticked to provide a record of the maximum pressure drop. The corresponding flow rate at which this maximum differential pressure is observed is printed immediately after the differential pressure reading.

The differential pressure transducer monitors the differential pressure (pressure drop) between a point immediately upstream and a point immediately downstream of the full flow fuel monitor, water coalescer, or other device typically applied in aviation fueling systems. The maximum differential pressure is observed during the fuel delivery is electronically input into the LectroCount® LCR-ll® Electronic Register. The highest differential pressures reached during the delivery is printed on the delivery ticked to provide a record of the maximum pressure drop. The corresponding flow rate at which this maximum differential pressure is observed is printed immediately after the differential pressure reading.

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Technical Specifications

  Liquid Controls Group; a Unit of IDEX Corporation
Product Category Pressure Sensors
Product Number (ΔP)
Product Name Differential Pressure Sensor
Device Category Sensor or Transducer
Measurement Type Differential; Negative Pressure
Media Liquid; Gas; Class 2: Jet Fuel
Display Type Printed Ticket
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