Precooled jet engine

A precooled jet engine is a concept for high speed jet engines that features a cryogenic fuel-cooled heat exchanger immediately after the air intake to precool the air entering the engine. After gaining heat and vapourising in the heat exchanger system, the fuel (e.g. H2) burns in the combustor. Precooled jet engines have never flown but are predicted to have much higher thrust and efficiency at speeds up to Mach 5.5. Precooled jet engines were described by Robert P. Carmichael in 1955.[1]

Pre-cooled engines avoid needing an air condenser because, unlike Liquid air cycle engines (LACE), pre-cooled engines cool the air without liquefying it.

A pre-cooled engine could be in the power-plant for a space launcher vehicle or for a very long range, very high speed aircraft.

Advantages of precoolers

One main advantage of pre-cooling is that, for a given overall pressure ratio, there is a significant reduction in compressor delivery temperature (T3), which delays the onset of the T3 limit as flight speed increases. Consequently, sea-level conditions (corrected flow) can be maintained after the pre-cooler over a very wide range of flight speeds, thus maximizing net thrust even at high speeds.

History and status of precoolers

Precoolers have never flown.

Similar systems

Precoolers were first proposed as part of the research in America on Project Suntan- a liquid hydrogen fuelled aircraft. Robert P. Carmichael in 1955 devised several engine cycles that could be used with hydrogen fuel, and this was one.[2]

Interest in precooled engines saw a brief emergence in the UK in 1982, when Alan Bond (formerly of the Blue Streak missile project) created a LACE-like design he called SATAN. The primary difference of these systems is that the air is only cooled, rather than liquified, and thus the gases are not actually separated, apparently giving significantly greater overall performance, due to a reduction in the amount of hydrogen used for cooling.

At the same time, John Scott and Bob Parkinson at British Aerospace had started some preliminary work on reusable launch systems. The two teams met and created HOTOL, which would use the BAe designed airframe with a Rolls Royce version of Bond's engine, known as the RB545. In 1986 the project was given an official go-ahead to the tune of 2 million pounds for research, but the program was later killed in 1989 when the project encountered problems and the government ended funding.

The principal designers continued development on their own, but the RB545 had been classified top secret and could not be used. Instead Bond developed another version that is more advanced, known as SABRE (ostensibly for Synergic Air BReathing Engine) which is meant for their Skylon design. Funding has not been terribly forthcoming (surprising, considering the design's potential to power an SSTO craft) and development continues at a relatively low level; papers and laboratory work are ongoing. A study of an aircraft powered by a SABRE class engine is underway under LAPCAT, partially funded by the EU looking towards hypersonic intercontinental travel (Brussels to Sydney in 2–4 hours non stop).[3]

See also

References

  1. ↑ NASA history Other Interests in Hydrogen
  2. ↑ NASA history Other Interests in Hydrogen
  3. ↑ Rob Coppinger (15 June 2006). "EU €7m hypersonic research plan considers UK-designed Mach 5 aircraft to fly Brussels to Sydney in 2h". Flight International. Retrieved 2009-07-03.
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