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#11
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(Skyking) writes:
FACT: Most multi engine airplanes lose 70% performance when they lose an engine. FACT: All single-engine airplanes lose 100% performance when they lose an engine. Here are some more facts for any poor sod who wanders in to r.a.h expecting to see useful information... A typical light twin typically holds altitude quite sufficiently on a single engine. http://www.aopa.org/members/files/pi.../prof0305.html (AOPA members only) A feathering prop is not required for adequate single engine performance in a very light plane. The Leza AirCam is said to be able to take off on one engine. (I'd provide a reference but their Web site is useless.) A typically-loaded (for me) light twin can take off, circle the pattern and land with one engine at idle (similar to windmilling) and the gear hanging out. There's a sweet-looking very light multi-engine plane for sale right now. http://www.aircam3.com/ I want one. --kyler |
#12
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"Kyler Laird" wrote in message ... A typical light twin typically holds altitude quite sufficiently on a single engine. We weren't talking about typical light twins, we were talking about ultralights. A feathering prop is not required for adequate single engine performance in a very light plane. The Leza AirCam is said to be able to take off on one engine. (I'd provide a reference but their Web site is useless.) The aircam is hardly typical. The thing has exceptional power, 200 HP in a 1000 lb aircraft and the engines are mounted as close to the centerline as they could get. |
#13
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"Kyler Laird" wrote in message ... ] A typical light twin typically holds altitude quite sufficiently on a single engine. http://www.aopa.org/members/files/pi.../prof0305.html (AOPA members only) For those who can't read that, it's a Barry Schiff articled talking about flying a Seminole with a SE service ceiling of a bit over 4000'. Of course he is talking about a feathered and otherwise cleaned up twin, and his conclusion is NOT that you hold altitude sufficiently, but that the rate of descent is manageable. |
#14
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#15
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"Neal Fulco" wrote in message
om... Bill, I have often thought about this also. Featherable props are expensive and it would be good to get around them. For a pusher installation, has anyone considered trying to develop the type of prop that Europeans use on some of their powered sailplanes, that being a folding prop. When the engine becomes " dead " the prop would fold back into the slipstream and lose it's drag. Neal, in my mispent youth I spent part of my time building contest-type model airplanes. The rubber-band types (typically 4 oz of rubber in a 4 oz airframe) used folding prop blades even in the usual tractor arrangement. Think about it, folding props up front are entirely practical! There may be _other_ reasons you might not want a folding prop. Very good reasons. |
#16
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#17
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BllFs6 wrote: Anybody ever looked at explosive bolts for ditching a draggy prop? Look for a guy with the nickname "Gus". Dave 'it just blew' Hyde Well..... that ref eludes me....but im often clueless...... Bllll ps...how do you know you blew a seal? your lips taste like sardines...... |
#18
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"Gig Giacona" wrote in message ... "jic" wrote in message news:Y4JIb.106419$ss5.61293@clgrps13... Why are there no multi engine ultralight trainers? I have about twenty hours behind a 912 and two forced landings already. It sure would be nice not depending on a single powerplant. Are two 40 hp engines unable to do the work of a 80hp? Not an ultralight but it does have a pair of engines. http://www.zenithair.com/gemini/index.html I didn't see a single engine service ceiling on the web page. I saw one a year or so ago in a magazine, and recall that is was so miserable, as to be assured of the one engine taking it to the crash site, if you were at any density altitude, at all. -- Jim in NC |
#19
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#20
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Think "hatch". As in "Liberty Bell 7."
Ron "Try another one, Nauga" Wanttaja oh ok...... but the bolts WORKED didnt they ? and it think that ships lift to drag ratio was rather poor.....but the power to wiegth ratio kicked ass take care Blll |
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