Difference between revisions of "Rolls-Royce Engines: Pegasus"
| Line 13: | Line 13: | ||
The engine is mounted in the centre of the Harrier and as such it is necessary to remove the wing to change the power-plant having already sat the fuselage on trestles; the whole change took a minimum of eight hours. | The engine is mounted in the centre of the Harrier and as such it is necessary to remove the wing to change the power-plant having already sat the fuselage on trestles; the whole change took a minimum of eight hours. | ||
[[Bristol Aero-Engines]] began work on the BE.53 Pegasus in 1958. The engine was designed in tandem with the prototype of the Hawker Siddeley Harrier, the Hawker P.1127, which first flew in 1960. It was developed from the [[Bristol Orpheus|Bristol Orpheus]], overseen by [[Stanley Hooker]]. The low pressure stages came from the Bristol Olympus engine. | |||
Production and development of the Pegasus was continued by Rolls-Royce when it acquired Bristol in 1966. a related engine design, the 39,500 lbf (with reheat) Bristol Siddeley BS100 for a supersonic VTOl fighter (Hawker Siddeley P.1154) was not developed to production as the aircraft project was cancelled. | Production and development of the Pegasus was continued by Rolls-Royce when it acquired Bristol in 1966. a related engine design, the 39,500 lbf (with reheat) Bristol Siddeley BS100 for a supersonic VTOl fighter (Hawker Siddeley P.1154) was not developed to production as the aircraft project was cancelled. | ||
Revision as of 17:37, 18 November 2019
Note: This is a sub-section of Rolls-Royce
The Rolls Royce Pegasus is a turbofan engine originally designed by the Bristol Engine Co and now manufactured by Rolls-Royce.
The Pegasus engine powers all versions of the Hawker Siddeley Harrier multi-role military aircraft. Rolls-Royce licenced Pratt & Whitney to build the Pegasus for US built versions. The Pratt & Whitney version is designated F402, and although manufactured by Pratt & Whitney uses "RR" as the manufacturer code. The Pegasus has also been the planned engine for a number of aircraft projects, among which were the prototypes of the German Dornier Do 31 VSTOL military transport project.
The Pegasus vectored-thrust turbofan is a two-shaft design featuring three low pressure (LP) and eight high pressure (HP) compressor stages driven by two LP and two HP turbine stages respectively. Unusually the LP and HP spools rotate in opposite directions to greatly reduce the gyroscopic effects which would otherwise hamper low speed handling. The engine employs a simple thrust vectoring system that uses four swivelling nozzles, giving the Harrier thrust both for lift and forward propulsion, allowing for STOVL flight. The front two nozzles are fed with air from the LP compressor, the rear with hot (650 degrees C) jet exhaust. It was critical that the nozzles rotate together. This was achieved by using a pair of air motors fed from the HP (high pressure) compressor, in a fail-over configuration, pairs of nozzles connected with chains.
The Pegasus was also the first turbofan engine to have the initial compressor fan, the zeroth stage, ahead of the front bearing. This eliminated radial struts and the icing hazard they represent. Also inlet guide vanes were not used in contrast to contemporary practise; it was found that they were not beneficial as was thought.
To date, more than 1,200 engines have been produced and almost two million operating hours have been logged with the Harriers of the Royal Air Force, Royal Navy, U.S. Marine Corps and the navies of India, Italy, Spain and Thailand.
The engine is mounted in the centre of the Harrier and as such it is necessary to remove the wing to change the power-plant having already sat the fuselage on trestles; the whole change took a minimum of eight hours.
Bristol Aero-Engines began work on the BE.53 Pegasus in 1958. The engine was designed in tandem with the prototype of the Hawker Siddeley Harrier, the Hawker P.1127, which first flew in 1960. It was developed from the Bristol Orpheus, overseen by Stanley Hooker. The low pressure stages came from the Bristol Olympus engine.
Production and development of the Pegasus was continued by Rolls-Royce when it acquired Bristol in 1966. a related engine design, the 39,500 lbf (with reheat) Bristol Siddeley BS100 for a supersonic VTOl fighter (Hawker Siddeley P.1154) was not developed to production as the aircraft project was cancelled.
Variants
- Pegasus 2: Otherwise known as the BE53-3, used in the P.1127, 11,500 lbf
- Pegasus 5: Or BS.53-5 (Bristol-Siddeley 53-3). Used for the H-S Kestrel evaluation aircraft. 15,000 lbf
- Pegasus 10: For first Harriers, 20,500 lbf, entering service in 1971.
- Pegasus 11: The Pegasus 11 powered the first generation Harriers, the RAF's Hawker Siddeley Harrier GR.3, the USMC AV-8A and later the Royal Navy's Sea Harrier. The Pegasus 11 produced 21,000 lbf (93.4 kN) and entered service in 1974.
- Pegasus 11-21/Mk.105/Mk.106: The 11-21 was developed for the second generation Harriers, the USMC AV-8B and the RAF Harrier IIs. The original model provided an extra 450 lbf (2 kN). The RAF Harriers entered service with the 11-21 Mk.105 which generates 21,500 lbf (96 kN). The Mk.106 development was produced for the Sea Harrier FA2 upgrade and generates 21,750 lbf (97 kN).
- Pegasus 11-61/Mk.107: The 11-61 is the latest and most powerful version of the Pegasus, providing 23,800 lbf (106 kN). This equates to up to 15 percent more thrust at high ambient temperatures, allowing upgraded Harriers to return to an aircraft carrier without having to dump any unused weapons which along with the reduced maintenance reduces total cost of engine use. This latest Pegasus has also enabled a highly effective radar equipped version of the AV-8 Harrier II to be introduced. This version, the Harrier II+, combines the proven advantages of day and night STOVL operations with an advanced radar system and beyond-visual-range missiles. The RAF is in the process of upgrading its GR7 fleet to GR9 standard. Part of this process is the upgrade of the Mk.105 engines to Mk.107 standard. These aircraft will be known as GR7As and GR9As.
See Also
Sources of Information
- [1] Wikipedia