Flowmeter Fuel Flow Transmitter

Technical Information

Catalogue No: C0780
Category: Fuel Systems
Object Type: Sensor/Transducer
Object Name: Flowmeter Fuel Flow Transmitter
Part No: 7501 26000
Serial No: 039/63X
Manufacturer: Elliott Bros
Division: Unknown
Platform(s):
Year of Manufacture: 1963
Dimensions:
Width (mm):
132 
Height (mm):
168 
Depth (mm):
118 
Weight (g):
2,063 
Location: Archive Object Store
Inscription(s):

Elliott
Transmitter Flowmeter
Type No. 7801.26000
Serial No. 039/63X
Ref. No. 6A/8249
────────────────
Mod No.
ES01
ES02
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HOUSING STAMPED WITH:
SC2022
3D479Z

Notes:

The rotor in this unit is large, more like a paddlewheel than the in-line rotor in the later units. This unit has an ‘X’ in the Serial Number which suggests that it was a prototype or an experimental design.

In the mid 60’s the Aircraft Engine Instruments Division of Elliotts specialised in the control and management of fuel propulsion systems and its many products included Fuel Flow Transmitters.
The Transmitter is a transducer that measures the rate of fuel flowing through it and converts this to an electrical signal to drive a remote meter. It was developed from the well-proven variable orifice type units that the Division had manufactured for a wide range of civil and military aircraft. A similar unit, Type 7801-11000, was designed for direct engine mounting to the Rolls-Royce Spey on the Trident. It had an accuracy of ± 1.0% of actual flow rate over the cruise band. These units have an ‘X’ in the Serial Number which suggests that they were prototypes or experimental designs.

The Fuel flow business was important to Elliotts and it was in 1964 that the new Fuel Flow laboratory was opened at Rochester. It offered a unique service in Europe. It was designed to test fuel flow equipment for the new generation of supersonic aircraft where fuel temperature of 150°C or higher would be encountered, and units would be required to operate at rigid standards of accuracy under extreme conditions of temperature (up to 200°C ambient) and in areas of extreme vibration.
The Laboratory can achieve gravimetric calibration accuracy within an error band of ±0.1% of flow
rate under the following conditions:
1. Flow rates from 50 to 120,000 lb/hr.
2. Fuel temperatures from -55°C to +180°C.
3. Ambient temperatures from -60°C to +200°C.
There is also a Vibrator capable of producing a maximum thrust of 500 pounds with frequencies of up to 3,000 c.p.s. for resonance searches.

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