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#31
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#32
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"John R Weiss" wrote in message news:B7Ztb.171248$9E1.880881@attbi_s52... "Tarver Engineering" wrote... At least on single-engine birds; some twins may have had counter-rotating props, but I don't think they operated from carrier decks all that much. What, like a P-3? Not single-engine, not a twin, no counter-rotating props, and never operated from a carrier... Never? LOL |
#33
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Keith Willshaw wrote:
"Cub Driver" wrote in message news Why would they? Their aircraft engines rotated in the same direction as the American's, thus generating the same port-biased torque. No, British aircraft engines turned the other way. Still do, I believe. They famously emasculated the Lightning by burdening it with two left-turning engines. The problem with the version of the P-38 supplied to the RAF was the inferior supercharger supplied on the export version not the fact that it had 2 engines turning the same way. The supercharger supplied (actually just a low pressure blower) was what was specified by the British, and what was a standard feature on the Allison. The Allison was intended to use a separate turbosupercharger for high altitude work, but the British didn't feel that high altitude performance was necessary at the time they wrote the specification. In addition, turbosuperchargers were not a high-volume production item, so including them might have delayed deliver. By the time the aircraft were delivered, however, the RAF had learned through experience that high altitude performance was indeed important. The poor handling of the aircraft, however, was indeed due to the fitting of same-direction rotating engine and propeller combinations, which was done to minimize the logistics tail, by using an engine which was already in use by the RAF (in export P-40s, IIRC). This engine also developed less horsepower, even at sea level, than did the V-1710F series engine used in all P-38s since the XP. A final possible reason for the British refusing to accept the Lightning (and especially the follow-on Lightning II, with turbosupercharging and counter-rotating V-1710F engines) was due to the method under which they were ordered. The original order for these aircraft was prior to lend-lease coming into being, and the British would have had to pay cash for them, unlike other aircraft ordered later. Given the changed requirements making the Lightning I less useful than expected, and the availability of other aircraft under lend-lease, buying the aircraft probably didn't seem a very economical way to spend their treasure. The Lightning II, if not for the cash requirement, probably would have been very useful to the British. Mike |
#35
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"Tarver Engineering" wrote...
What, like a P-3? Not single-engine, not a twin, no counter-rotating props, and never operated from a carrier... Never? LOL The P-3 Orion? Never. |
#36
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"John R Weiss" wrote in message news:l7aub.170253$mZ5.1193885@attbi_s54... "Tarver Engineering" wrote... What, like a P-3? Not single-engine, not a twin, no counter-rotating props, and never operated from a carrier... Never? LOL The P-3 Orion? Never. OK then. |
#37
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ANDREW ROBERT BREEN wrote:
snip eddies from the island could be shed outboard instead of across the flight deck, and the side chosen for the island was determined by the turning characteristics of rotary-engined biplanes. Once the island was on the starboard side, the longer life of ships than aeroplanes ensured it stayed there.. OP jumping in to say thanks to all participants for the input. Coincidentally, I've been engaged in an email discussion about rotary engines, with a friend, albeit naval aircraft have not - yet - come into play, there. Too bad I wasn't capable of adding two and two (rotary torque-turning and my carrier question) and getting four, myself. Again, I appreciate the responses. -- Thomas Winston Ping |
#38
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"Keith Willshaw" wrote in
: "Cub Driver" wrote in message news They famously emasculated the Lightning by burdening it with two left-turning engines. The problem with the version of the P-38 supplied to the RAF was the inferior supercharger supplied on the export version not the fact that it had 2 engines turning the same way. While this is true, the previos Dan was correct. The P-38 had significant tail flutter problems with "inword" rotateing engines. This was fixed on American P-38's by having the engines rotate "outword" in opposite directions, however the British version had two engines which in addition to lacking the General Electric B-5 turbosuperchargers also rotated in the same direction. This lead to one of the engines generating the same effect that had been a problem with the P-38 prototypes. |
#39
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"Tarver Engineering" wrote in
: "John R Weiss" wrote in message news:B7Ztb.171248$9E1.880881@attbi_s52... "Tarver Engineering" wrote... At least on single-engine birds; some twins may have had counter-rotating props, but I don't think they operated from carrier decks all that much. What, like a P-3? Not single-engine, not a twin, no counter-rotating props, and never operated from a carrier... Never? LOL I assume you have some sort of evidence that a 140,000lb airplane that needs 4,000+ft of runway was somehow able to operate off of a carrier, right? |
#40
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The problem with the version of the P-38 supplied to the RAF was the inferior supercharger supplied on the export version not the fact that it had 2 engines turning the same way. How would you like to have to turn a fighter to the left to avoid a Japanese fighter when you have two 1200-hp Allisons pouring on the torque to the right? This was an all-but-impossible task. I think your grasp of the subject leaves something to be desired, Keith. British engines did turn anti-clockwise as seen from the cockpit; the export Lightning was all but useless as a result of two engines turning the same way; and carrier islands to starboard had little or nothing to do with engine rotation. all the best -- Dan Ford email: (put CUB in subject line) see the Warbird's Forum at www.warbirdforum.com and the Piper Cub Forum at www.pipercubforum.com |
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