Shortround6
Lieutenant General
The Mercury, for British engines, showed the best increase in power form better fuel.Some engines - both liquid cooled and air cooled - benefitted more, some benefited less. The FS Mercury engines of late 1930s vintage went from being good for 800 HP at 9000 ft (and 840 HP at 14000 ft) on 87 oct fuel to 990 HP at 9000 ft on the early 100 oct fuel - an almost 25% increase.
Basically, only the Merlins were better in the % of extra power due to 100 oct fuel in that time, thatm in case of Mk.III gained about 35% at ~9000 ft (970 HP vs. 1300).
A lot of things are trade-offs and in the case of twin engine British bombers there may be a number of problems trying to operate at higher altitudes. The Pegasus was never allowed to use the higher levels of boost that the Mercury was. A bit higher yes, about 1 to 1.25lb of extra boost. The Pegasus XVIII was rated at 885hp at 15,500ft at 5lbs and 965hp at 13,000ft at 6.75lbs using 100/130. Now about 1/2 of the change is due to the 2500ft change in altitude.Availability of the high-altitude models of engines does not mean that the low- or mid- altitude models are not made.
On the bombers, there is a lot of place to fit and streamline the intercoolers. So better start working on these, including the suitable gearing of both S/Cs, so the, at least, Welligtons and Hampdens can cruise well at 20000 ft instead at 15000 ft, with bomber Ensign-lookalike and Halifax (with Hercules) following suit.
Adding several hundred pounds of extra supercharger and intercooler/duct to the the medium bombers is going cut into the performance no matter how streamline you make it. Are you willing to cut into fuel or bomb load to carry the bigger supercharging system? There is going to be some improvement in performance. The question is how much and at what cost.
In the Mercury yes, in the Pegasus it does not appear so. Actual problem may have been in the crankshaft? The longer stroke may have stressed the crankshaft more? Or they may have been a cooling problem. Adding an extra 1 in of fins at the bottom of the cylinder which is the coolest part of the cylinder may have meant the Pegasus had a problem with higher power. Taurus had cooling problems and the Hercules was never ending saga of trying to keep the cylinders and cylinder head cool. They did it but there were a number of cylinder and cylinder head redesigns to allow for more power. For the Hercules this was paralleled by the increase in allowable boost pressures.As noted by the users of the Mercury and the 100 oct fuel, there was a lot of stretch wrt. the engine strength.
In some of these engines it wasn't worth the trouble. If an engine is only using 100hp to drive the supercharger going from 60% efficient supercharger to a 70% efficient supercharger is not even going to give you 10hp at the crankshaft on a 1000hp class engine. Or 20hp for a high gear ratio version. Now a more efficient supercharger will heat the air less and allow for more power because you can use higher boost.Appeal of the more refined superchargers is that they use less engine power to provide the same boost at the chosen altitude, meaning there is more power left to the prop (with IHP remaining the same).
The Taurus was an altogether bad decision by Bristol but it shows how sometimes designers and companies can fall into some holes in thinking. A very expensive/heavy small diameter (but low drag) engine will find acceptance over cheaper/lighter but higher drag engines in the market place???? The the hoped for 3300rpm never paned out which hurt power when the production engines stayed at 3100rpm.Hence the suggestions to drop the Taurus in most of the what-if scenarios dealing with RAF for ww2.
It is not but Bristol with sleeve valves had problems with BMEP that poppet valve engines did not. Using boost pressure is a shortcut to judging either BMEP or other structural problems, not 100% reliable but an indicator.High boost is not the only metric of the engine quality.
Mercury was a good engine, however it was too small. The Pegasus had problems with the long stroke. For most of the 1930s it was OK but the high piston speed limited RPM.Marginal engines don't achieve 25% power increase when going from 87 to the early 100 octane fuel.
Compared to the R-1820 that used a 175mm stroke the Mercury used a 165mm stroke and the Pegasus used a 190mm stroke.
Perseus had a triple whammy. Too small (Mercury size cylinders), RPM limit very close to the Mercury. Early sleeve valves that didn't allow for high boost, perhaps not a problem with 87 octane fuel.
Wright redid the crankshaft/crankcase to go from 2200rpm to 2350 rpm and they did it again to go to 2500rpm and they did it yet again to go to 2600rpm. They also changed the cylinder barrels and the cylinder heads every time. There was never a "just change the supercharger" model change, maybe Wright just built crappy superchargers?
Bristol, like a lot (all) of Britain had shortage of engineers/draftsmen. They could not go in a lot of different directions as once. Just like manufacturing any major change in R&D may mean decrease somewhere else. They also spread themselves too thin in the late 30s.
There are things that are worthwhile to do even if they do not result in the best possible outcome. But some projects are not going to give a very good out come for investment.This becames the same speke as the long range Spitfire - if it is not the 100% equivalent of the P-51D, then it is not worth it. To what I disagree 100% with.
If your resources (investment ability) are limited perhaps 2-3 good investments are better than 1 excellent one. And 2-3 good ones may beat 5-6 marginal ones.