GNOME

The Gnome engines used in the facility were manufactured by Rolls-Royce. The Gnome is a turboshaft propulsion unit. Three main variants of the engine have been produced - 1000, 1200 and 1400. The 1400 variant is used to power the Sea King helicopter.

The engine comprises a free power turbine and independent gas generator.

- Mass flow - 5.63kg/s
- Ten stage axial compressor with variable incidence inlet guide vanes (1st four stages)
- 8.3:1 compression ratio
- Straight through annular combustion chamber with sixteen fuel injectors
- Fuel type - Kerosene - JP-4
- Exhaust temperature up to 685 ºC
- Fuel consumption - approx. 5 litres/min at max continuous rating
- Dry weight without gearbox 125kg
- Electric start - two HT ignitors

Gnome Turbojet rig (TJ1)

To provide a means for simulating typical thrust engine environments, two of the GETL engine rigs use a Gnome with the power turbine removed.

The 3rd stage nozzle guide vanes which support the rear bearing have been cut back to reduce swirl and an additional vane set has been provided to reduce swirl still further.

The gas generator can then be run as a turbojet engine generating some 3kN of thrust.

The turbojet rigs provide from small scale up to full scale testing of nozzles depending upon the application (0.16m diameter).

Gnome Turboshaft rig (TS1)

TS1 is a very compact rig which uses the Gnome engine in its conventional format - i.e. with the power turbine. The engine is loaded using the compressor from another Gnome engine. These are linked using a gearbox taken from a Westland Wessex helicopter, and is therefore small, lightweight and contains its own oil delivery and cooling system. However the operation is limited to 19,500rpm compressor speed.

The Gnome compressor is mounted underneath the engine, which makes this rig very transportable.

Gnome Turboshaft rigs (TS2, TS3, TS4)

S&C has designed three other engine rigs which use the Gnome in shaft format and loaded by a Gnome compressor, similar to TS1, but in these rigs the gearbox has been designed to allow the engine to be fully loaded to 1235SHP. This generates a large amount of compressed air which can be delivered to other rigs. The engine and compressor are mounted side by side and there is an ancillary oil cooling system.

TS3 is a variant which has been containerised to allow safe operation outside the test facilities.

The turboshaft rigs can supply a compressed air flow of max 4kg/s at 220ºC, with an NPR up to 5.0.

ADOUR

The Adour engine is manufactured by jointly by Rolls-Royce and Turbomeca and variants of the engine are used in the BAE Systems Hawk, SEPECAT Jaguar and Mitsubishi F-1 and T-2 aircraft. In S&C's facility at Kemble, the Mk.104 (Jaguar) engines are used and these are run in the dry mode as a thrusting engine.

Key features of the 104 engine:

- Bypass ratio 0.75-0.8
- Two shaft
- Five stage axial compressor
- Two stage turbine
- Mass flow approximately 40kg/s
- Thrust 23.5kN (sea level static - dry)
- Exhaust temperature up to 750 ºC
- NPR up to 2.0 (sea level static)
- Air start

TS5 (T55-Viper)

Larger mass flows of compressed air can be generated using S&C's TS5 turboshaft rig, which comprises a T55 (Chinook) engine which is loaded using the compressor from a Viper 535 (from the BAC 167 Strikemaster). The shaft speeds of these two engine types are well matched, meaning they can be directly coupled without the use of a gearbox.

Key features of the TS5 turboshaft:

- Mass flow of compressed air approximately 15kg/s (max 18 kg/s)
- Exhaust temperature up to 700 ºC
- NPR up to 2.0 (sea level static)
- Hydraulic start

Microturbo starter (SAPHIR)

The smallest of S & C's engine rigs, the SAPHIR is a very useful jet engine for low-cost scaled testing with manageable flows. The rig is based on the Microturbo SAPHIR, a small gas turbine compressor unit used to supply air for starting engines in many aircraft including the Jaguar and the Hawk.

Key features of the SAPHIR:

- Mass flow of compressed air approximately 0.4kg/s at 45 PSI
- Air delivery 50 BHP
- Electric start