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It didn't say which came first...
Which design was proposed first, and what roles were the XH-3130/3730 designed for?
OkayShortround6 said:The H-3130 was run during 1938 as experimental engine X-86.
It was later rebuilt with bigger cylinders as the H-3730 and tested in 1940 as experimental engine X-97.
For some reason, I thought they were both US Navy engines.I don't know were the H-2600 falls in the time line. It was an army engine and the other two were navy engines.
I was thinking fighters, bombers, patrol planes, etc...wuzak said:What were they designed for? Aircraft that required engines.
So they could be mounted in a skinny or wide layout without issue?They were deiberately designed to be narrow and to be able to mounted with cylinders vertical or horizaontal, to suit single engine types (vertical) and multi-engine types (horizontal).
I was thinking fighters, bombers, patrol planes, etc...
So they could be mounted in a skinny or wide layout without issue?
True, but bombers tend to require bigger enginesYep. They are all aircraft that require engines.
I thought by around 1938 they gave up on the idea of the O-1230/1430 and decided to reconfigure it into the IV-1430.The idea was that the horizontal mounting would be enable the engine to be enclosed in the wing or, at least, present no more frontal area than the wing profile behind it for a nacelle mounted engine.
True, but bombers tend to require bigger engines
I thought by around 1938 they gave up on the idea of the O-1230/1430 and decided to reconfigure it into the IV-1430.
I'm curious why they asked Pratt & Whitney to develop this design
when they had the IV-1430 and O-1230 which could both be doubled up into the IV-2860 and H-2470?
Consider that...
- The USAAC asked Allison to produce the X-3420 (later V-3420) out of 2 x V-1710's
- The USN asked Lycoming to take the O-1230 and double it up into the H-2470
- The USAAC & USN could have teamed up to cosponsor the H-2470 as they did with the V-1710
Truewuzak said:Or more of them.
According to Wikipedia (yes I know that mostly invalidates what I'm going to write): "Continental built the first I-1430 engine in 1938 and successfully tested it in 1939"Not exactly sure when that was changed.
It might very well have been an unsolicited contender, but the Army seemed to fund it...Not sure that the USAAC asked them to design anything.
Which lead to the H-3130?I believe it was George Mead that had pushed for the development of the sleeve valve engines
The hyper-engine was the O-1430 which then became the XI-1430. The H-2470 was based on the Lycoming O-1230.I think you mean the O-1430, not the IV 1430.
According to Wikipedia...Not sure where the idea for the H-2470 came from
Was the V-1710 submitted first to the USAAC or vice-versa?At some stage the USN did start sponsoring the program, no doubt after Lycoming pitched the idea.
Does anybody have dimensions (other than displacement figures) for the X-1800/XH-2600, and H-2470 including...
as well as weight?
- Length
- Width
- Depth
- Bore & Stroke (if possible)
I have the displacement figures (far as I know) for both (XH-2600: 2597.7 in^3; H-2470: 2467.8 in^3).
I did, it didn't have a complete listing for dimensions.Did you try wiki as a starting point?
I got a "Permission Denied" on that site. Can you do a screen-cap?
I did, it didn't have a complete listing for dimensions.
I got a "Permission Denied" on that site. Can you do a screen-cap?