Most Useful Plane Not Produced

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Most useful plane not produced. Factory spec Brewster Buffalo's with the actual correct, (no sub par substitute accepted) engine.
It was already in production. It was already in service. It was there and in numbers. If only more of them worked as advertised.
 
Not the engine, the company. Napier hasn't made anything useful outside of perhaps the Lion. Giving them the business was obviously an attempt at procurement diversification, but the engine was never going to be reliable. Is any museum or racer flying a Sabre today?Not a giant Sabre into a Merlin hole, but Merlins have been swapped into replace Fiat/DB and Allison inlines with little apparent difficulty.

Apparently, it was done, once. According to a chapter of the book, Hurricane (I read this thing about 60 yars ago, so don't press me for details) someone in a Hurri night fighter squadron had his bird loose an engine, and he replaced it with a unit from either a Tiffy or a Tempest; he had great success with it, until the buaurocraps caught up with it, and shut him down. Seems the firewalls on the Hawker fighters were zll the same....

:cool:
 
Apparently, it was done, once. According to a chapter of the book, Hurricane (I read this thing about 60 yars ago, so don't press me for details) someone in a Hurri night fighter squadron had his bird loose an engine, and he replaced it with a unit from either a Tiffy or a Tempest; he had great success with it, until the buaurocraps caught up with it, and shut him down. Seems the firewalls on the Hawker fighters were zll the same....

:cool:
Despite the radiator under the hurricane being designed for a 27L 1500hp engine, not a 36L 2000-2600hp engine.

Despite the sabre weighing a full 250kg more before all the oil that goes in it and it's attendant oil cooler.

Despite the sabre being 10" wider, with exhausts in a different location. How did they manage the aircraft skin around it?

What about prop? The sabre has a much to0 big prop on it for a Hurricane it would hit the ground on takeoff. So you fit a smaller hurricane prop and somehow the sabre (temperamental engine) performs properly with much less mechanical resistance at the crank.

Also a 2.6 ton 32' aircraft and a 4 ton 42' aircraft have the same firewall??

I have a strong suspicion this story is apocryphal.
 
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Oh, and B-29s over Nihon....

Major problem was lack if suitable strategic targets--Much of Japanese war production was in small shops, even private homes; the factories were mainly assembly centers, not like Western ones, where metal stock goes in a loading dockat one end, and finished aircraft roll out the other. Engine factories seem to have been similar to the Western model--when the one producing engines for the Ki-61 'Tony' was destroyed, they had to replace it with a radial, resulting in the Ki-100(?) 'Tony'
 
Oh, and B-29s over Nihon....

Major problem was lack if suitable strategic targets--Much of Japanese war production was in small shops, even private homes; the factories were mainly assembly centers, not like Western ones, where metal stock goes in a loading dockat one end, and finished aircraft roll out the other. Engine factories seem to have been similar to the Western model--when the one producing engines for the Ki-61 'Tony' was destroyed, they had to replace it with a radial, resulting in the Ki-100(?) 'Tony'
They did the ijaaf a favour there. The Ki100 can be argued to be the best Japanese fighter of the war.
 
Not sure where that info comes from, Japan had large industrial centers throughout the home islands.
Even late into the war, many of these arras were still producing war material even after being bombed, much like Germany was doing.
Yes, small workshops were all across the country in towns and villages manufacturing everything from rifle ammunition to aircraft components, but their industrial centers were still active, viable targets.
And typically, where there was an industrial center, an Army and/or Navy facility could be found.
 
I think they should have fit the P-38J's with the P-38K's prop -- it seems like it wouldn't be that hard to do. As for the P-61, I think a turbocharger should have been present from the outset -- there were plans to do so, but the twin-stage supercharger was chosen to increase endurance.
The P-38K's prop required a different gear ratio and different reduction gear casing; the prop centerline was a few inches higher which required a redesign of the engine cowling. That cowling redesign was what would have shut production down for a few weeks. Those few weeks of production loss is why the AAC nixed the P-38K.
 
From my perspective as an American, looking at American aircraft, I am struck by how many times they made the RIGHT call on aircraft production. After an iffy first year of not being ready for war, the USAAF and USN made good calls that resulted in good aircraft in all categories being produced in large quantities.
 
The P-38K's prop required a different gear ratio and different reduction gear casing
How hard is it to change the gear-ratio? I remember there was a test run with an F4U-1 with a 0.4 gear-ratio instead of 0.5.
the prop centerline was a few inches higher which required a redesign of the engine cowling.
Why would it matter if the centerline was a little higher or lower, or did it have to do with the shape of the spinner?

From my perspective as an American, looking at American aircraft, I am struck by how many times they made the RIGHT call on aircraft production.
And how quickly we managed to get things to work at exactly the right moment... honestly some of it surprises me.
 
How hard is it to change the gear-ratio? I remember there was a test run with an F4U-1 with a 0.4 gear-ratio instead of 0.5.

The R-2800 used an epicyclic (planetary) reduction gear system. Changing the gear ratio on that may have been as simple as changing the gears, or may have required redesign of the carriers.

The V-1710 used a spur reduction gear type (except on the earlier long-nose C series). The centre spacing of the gears could be the same if only small adjustments are required, but if one of the gears (the one driven by the crank) is the smallest it can be for the tooth profile, the spacing between the gear centres would need to be changed.

This would require a redesign of the reduction gear case - easier on the V-1710 than the Merlin, whose reduction gear case was partially in unit the crankcase casting.


Why would it matter if the centerline was a little higher or lower, or did it have to do with the shape of the spinner?

If the centreline was higher or lower the cowl shape would change, if the spinner was the same as the previous version. It may not have been possible to make a smaller spinner, since the spinner has to contain the workings of the propeller pitch mechanism.
 
How hard is it to change the gear-ratio? I remember there was a test run with an F4U-1 with a 0.4 gear-ratio instead of 0.5.

Well, it requires a new set of gears, which have to be designed and built. It can actually be quite hard. There may have been a lot of luck involved, a gear combination could have been thrown together from off-the-shelf components, but something that is being built for a one-off test is not the same as something that's going to be produced in thousands.

Why would it matter if the centerline was a little higher or lower, or did it have to do with the shape of the spinner?

One is there would be a step behind the propeller, so more drag. Steps can also generate a lot of noise, buffeting, possibly interfering with control surfaces causing fatigue damage airframe.

And how quickly we managed to get things to work at exactly the right moment... honestly some of it surprises me.
 
Despite the radiator under the hurricane being designed for a 27L 1500hp engine, not a 36L 2000-2600hp engine.

Despite the sabre weighing a full 250kg more before all the oil that goes in it and it's attendant oil cooler.

Despite the sabre being 10" wider, with exhausts in a different location. How did they manage the aircraft skin around it?

What about prop? The sabre has a much to0 big prop on it for a Hurricane it would hit the ground on takeoff. So you fit a smaller hurricane prop and somehow the sabre (temperamental engine) performs properly with much less mechanical resistance at the crank.

Also a 2.6 ton 32' aircraft and a 4 ton 42' aircraft have the same firewall??

I have a strong suspicion this story is apocryphal.

The Sabre is a 1070kg (corrected) engine, the Merlin 20 is a 600kg engine. You would need about 150(corrected) kg of ballast in the tail. There were proposals for a Vulture Engine Hurricane so its not entirely absurd.
 
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There were proposals for a Vulture Engine Hurricane so its not entirely absurd.

There were?

The Vulture was not as wide or tall as the Sabre, but it was 5 to 6 inches wider than the Merlin, a couple of inches taller, quite a bit longer (than the single stage Merlin used on the Hurricane) and was, like the Sabre, about 500kg heavier than the Merlin.

I know there were proposals for a Griffon powered Hurricane, which makes sense as the Griffon was designed to fit on aircraft powered by Merlins (ie the Spitfire).
 
It is very much possible that a Re.2005 prototype have gotten the DB 603A engine some time in 1943, akin to the Re.2006 or G.56; later was good for 425 mph IIRC.
The Re 2006 with a DB 603A engine was projected to reach 750 km/h at 7200m (466 mph at 23620 feet)! The first prototype was completed in February 1944 but for political reasons was not flown and was later dismantled.
 
From my perspective as an American, looking at American aircraft, I am struck by how many times they made the RIGHT call on aircraft production. After an iffy first year of not being ready for war, the USAAF and USN made good calls that resulted in good aircraft in all categories being produced in large quantities.
My only thought on 1941/42 is that it was a shame the Soviets didn't get the Cobra 6 months earlier to wring the bugs out of it. Then I'm sure the Americans could have made far better use of it out in the Pacific in 1942/43.
 

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