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| | #61 |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,861
| Oh yea! I disposed of many uniforms because of that stuff!
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| | #62 |
| Senior Member Join Date: Nov 2005
Posts: 167
| It's interesting to look at what they were getting out of the late two-stage blower V-1710's. A rare engine, only used in the P-51H, some P-82 Twin Mustangs, and the P-63. I don't have the figures in front of me, but they were quite a bit more powerful. There was also a V-3420, 24 cylinder double-V Allison, developed for a B-29 version (B-39?). I think it was real close to 3000 h.p.. What about the Junkers Jumo? |
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| | #63 | |
| Senior Member Join Date: Jul 2005 Location: Japan
Posts: 505
| Quote:
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| | #64 |
| Senior Member Join Date: Nov 2005
Posts: 167
| My mistake, it was the P-51J that had the 2 stage Allison. I think only 2 were built, and they had about 2,300 h.p.. The idea was that because Packard was going to have to start paying royalties to Rolls-Royce to continue Merlin production after the war's end, thought was given to going back to the Allison on the P-51. |
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| | #65 | |
| Senior Member Join Date: Jul 2005 Location: Japan
Posts: 505
| Quote:
From Joe Baughers excellent website; "The last prototype in the lightweight NA-105 series was the XP-51J, which was similar to the F and G models except that it reintroduced the Allison V-1710 engine to bring the Mustang full circle. The Allison engine was, however, the V-1710-119 version with a two stage, gear-driven supercharger, rated at 1500 hp for takeoff and 1720 hp with water injection at 20,700 feet. Unlike earlier Allisons, this engine had an updraft carburetor. The nose geometry was substantially modified, and all air inlets in the nose were completely eliminated. Instead, the carburetor air was taken in through a ram inlet at the front of the radiator duct and piped to the engine. A dorsal fin was fitted. Two XP-51J prototypes were ordered, with serial numbers being 44-76027 and 44-76028. 44-76027 made its first flight on April 23, 1945, piloted by Joe Barton. The XP-51J weighed 6030 pounds empty and 7550 pounds normal loaded. It was anticipated that a maximum speed of 491 mph could be achieved at an altitude of 27,400 feet, but this was never achieved during tests because the new Allison had not yet been cleared for full power operations. XP-51J Ser No 44-76027 was, in fact, loaned to Allison so that they could use it to iron out the bugs in their engine. The other XP-51J prototype, Ser No 44-76028, was never actually flown, but was scavenged for spare parts to keep the other example flying. The end of the war in the Pacific brought all further work on the XP-51J to an end. " | |
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| | #66 |
| Senior Member Join Date: Nov 2005
Posts: 167
| I have one source that lists the V-1710-119 as having 2,300 h.p., but other sources say 1720 h.p., as you pointed out. Maybe the higher figure was a proposed output, or a WER, but I now think the 1720 figure may indeed be more accurate. |
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| | #67 | |
| Banned Join Date: Jan 2005
Posts: 795
| Quote:
Eagle http://www.enginehistory.org/eagle_22.htm H24 sleeve valve 2238ci 5.4" x 5.125" (b x s) 3500hp@3500rpm 2 stage, 2 speed intercooled, aftercooled(1/bank) supercharging Was to be used in the Wyvern. Pennine X24 sleeve valve aircooled 2685ci 5.4" x 5.0" (b x s) 3000hp potential Crecy V-12 90* sleeve valve 2 stroke 1593ci 5.1" x 6.5" (b x s) 37" (104" Hg) boost with ADI > 3.6hp/ci Oh yes forgot, the BMW801 was putting out 2200hp+ with the F model. | |
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| | #68 |
| Senior Member Join Date: Aug 2005
Posts: 580
| Cylinder-for-cylinder, the VW Beetle boxer engine seems a lot better than the DB iverted vee's. Who else thinks a 12 cylinder version would've been good?
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| | #69 |
| Senior Member | As in a 12-cylinder boxer? Well they are very flat and low, which would have given it a low frontal area and lower center of gravity...It would have been interesting. |
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| | #70 |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,861
| Jabiru makes an 8 cylinder opposed, Kloeckner-Humboldt-Deutz made a 16 cylinder opposed diesel engine during WW2. Franklin and Continental also made 8 cylinder opposed engines, Frankin did do a 12... http://www.jabiru.net.au/engines/8cylinder/
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| | #71 | |
| Senior Member Join Date: Dec 2004 Location: Boise, Idaho
Posts: 1,175
| Quote:
The F-30 series 111/113 engines were given a 1,725hp @ 64" service rating by field order for WEP service. The G6R-143 model used in the P-82s was rated @ 2,250hp at 3,200rpm. The prototype engine for the P-63Q was rated @ 2,900hp but was not put into service for several reasons. wmaxt | |
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| | #72 | |
| Banned Join Date: Jan 2005
Posts: 795
| Quote:
Jumo 2xx series, 6 cylinders, 12 pistons http://www.geocities.com/hjunkers/ju_jumo205_a1.htm used in the Dornier Do 18, Dornier Do 24, Dornier Do 26, Blohm & Voss BV138 http://www.geocities.com/hjunkers/ | |
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| | #73 |
| Banned Join Date: Jul 2003
Posts: 110
| I believe the only H-block engines were the Napier Sabre and the Rolls-Royce Eagle 22. The Eagle was basiclly two flat 12 engines, one on top of the other, running a common crank. It produced 3,550 HP from 2,817 cubic inches, or 2,647 kW from 46.2 liters. Bore was 5.40 inches, stroke was 5.125 inches (13.72 cm x 13.02 cm). |
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