don4331
Senior Airman
When the gov't is trying to limit warplane size, its extremely difficult to order large engines... USA was fortunate that the commercial industry was wanting larger planes and with them larger engines. Large twin is more economical to operate than quad engined plane. If industry isn't designing airframes for 2,000hp/2000lb engines why would a engine business commit to developing them?
Aside: Even in '90s, I could get from Canary Wharf (London) to Guyancourt (Paris suburb) faster on tube/train(Chunnel), than my colleague could drive/fly (via Heathrow/de Gaulle - if he got flight via City/Orly, bets were off). It was hard for commercial aviation to compete in Europe during 30s.
R-2800 broke so many crankshafts during development that P&W questioned if high power 18 cylinder was even possible. And even when they got it running they had issues with gallons of oil getting whipped like toffee around the crankshaft limiting power. Does Germany have the resources both human and financial to tackle the problem.
The issue with starting too soon is your 87 octane with pre Rubbra supercharger on derated R/Buzzard/Griffon I needs the nameplate lifted off the engine and everything underneath replaced with clean sheet design for 100 octane with post Hooker supercharger on Griffon IV. Which is what happened with RR's "big block" V-12. Thankfully, for RR only prototype had be build because if they had committed to production tooling Griffon might never have seen light of day.
Vulture starts out with that wonderful idea - just connect 4 Kestrel blocks/cylinder heads on common crankcase. But when the initial testing of single row "X", demonstrates that the master/slave rod(s) need more bearing area, so Vulture needs its own block/cylinder heads, RR should have shutdown the project and re-evaluated if it was the right engine to be focusing on. Especially when Peregrine is on the chopping block, so all parts become unique to the X-24 engine (OK, there might be some parts common to Kestrel and RR was pumping out Kestrels for advanced trainers, etc).
Note: Germany's war is won/lost in the battle with Russia. Does committing to radial engines solve that problem?
Aside: Even in '90s, I could get from Canary Wharf (London) to Guyancourt (Paris suburb) faster on tube/train(Chunnel), than my colleague could drive/fly (via Heathrow/de Gaulle - if he got flight via City/Orly, bets were off). It was hard for commercial aviation to compete in Europe during 30s.
R-2800 broke so many crankshafts during development that P&W questioned if high power 18 cylinder was even possible. And even when they got it running they had issues with gallons of oil getting whipped like toffee around the crankshaft limiting power. Does Germany have the resources both human and financial to tackle the problem.
The issue with starting too soon is your 87 octane with pre Rubbra supercharger on derated R/Buzzard/Griffon I needs the nameplate lifted off the engine and everything underneath replaced with clean sheet design for 100 octane with post Hooker supercharger on Griffon IV. Which is what happened with RR's "big block" V-12. Thankfully, for RR only prototype had be build because if they had committed to production tooling Griffon might never have seen light of day.
Vulture starts out with that wonderful idea - just connect 4 Kestrel blocks/cylinder heads on common crankcase. But when the initial testing of single row "X", demonstrates that the master/slave rod(s) need more bearing area, so Vulture needs its own block/cylinder heads, RR should have shutdown the project and re-evaluated if it was the right engine to be focusing on. Especially when Peregrine is on the chopping block, so all parts become unique to the X-24 engine (OK, there might be some parts common to Kestrel and RR was pumping out Kestrels for advanced trainers, etc).
Note: Germany's war is won/lost in the battle with Russia. Does committing to radial engines solve that problem?