Engines-List Digest Archive

Tue 09/09/03


Total Messages Posted: 2



Today's Message Index:
----------------------
 
     1. 04:46 AM - What is this engine worth? (Ronschreck99@aol.com)
     2. 09:36 PM - Re: Question about electronic ignition (Bob Buckthal)
 
 
 


Message 1


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    Time: 04:46:45 AM PST US
    From: Ronschreck99@aol.com
    Subject: What is this engine worth?
    --> Engines-List message posted by: Ronschreck99@aol.com Hi listers, I have a very good friend who was once building a HyperBipe but gave up on the project after buying almost everything he has to complete the airplane. He has offered to sell me the engine and propeller but neither of us knows what either are worth. Here is what I know about each: The engine is an IO360-B1E, rated at 180 HP at 2700 RPM. It was overhauled a few years ago and I know it got new rings, bearings and valves. However the engine has been sitting on his hangar floor ever since and the plug holes and accessory holes have been open to the air all that time. I see a slight surface rust on some of the accessory gears but the valves and cylinders are bright and shinny. I suppose they have a good coating of lubricant that is doing it's job. Two bendix mags of unknown condition are included. They are all in one piece and include all the plug wires. They both turn freely. A new Airflow Performance fuel injector is included as well as a used Prestolite starter and a used alternator of unknown make. The prop is a Hartzell CS 2-blade that was rebuilt after a prop strike incident. The blades were bent and although the rebuild was done by a reputable propellor shop they could not yellow tag it because the bent tips were bent past the allowable angle to meet certification standards. It is legal to use on an experimental aircraft. I haven't seen the prop governor but I assume there is one somewhere in the hangar. I'll keep looking. If the engine is suitable in other respects I assume that the rear-facing injection can be remedied with a new sump. Given the information above I welcome the list's comments on estimating the value of the engine and prop and the cost of replacing the sump. Have at it guys. Thanks for your help. Ron Schreck RV-8 Gold Hill Airpark, NC PS: Anyone interested in a HyperBipe?


    Message 2


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    Time: 09:36:02 PM PST US
    From: "Bob Buckthal" <n223b@comcast.net>
    Subject: Question about electronic ignition
    --> Engines-List message posted by: "Bob Buckthal" <n223b@comcast.net> John, Most of the information you are looking for is on the web at www.cafefoundation.org/research.htm. Although their research compares electronic ignition with magnetos the data is still telling. The mission that you have selected for your airplane is the key. If you intend to fly low and fast, developing the maximum horsepower then there is little advantage to E.I. However, If you live in the west where you'll need to cross big mountains or if you plan to travel long distances and fuel economy is a major consideration then E. I. will produce better performance because it optimizes ignition timing at low manifold pressures and/or lean mixtures. I fly in the west and I use my IO360 powered Glasair for long distance travel. I don't mind slowing down in order to save fuel and extend range. I selected the Lightspeed Plasma I because it produces 5 times the spark duration and 5 times the spark energy of a Plasma II. All this extra energy will ignite leaner mixtures at lower manifold pressures. My engine came fuel injected. With some manipulation of the injectors I've been able to achieve very even running of each cyl which with E.I. allows me to cruise at over 100F lean of peak EGTs. At 150 to 160 Kts TAS I usually see 25 MPG fuel economy in a 2100LB gross wt airplane. I don't have any experience with the Electroair E.I.(Jeff Rose). But I am extremely pleased with my Plasma I. While the C.A.F.E. test airplane is not fuel injected, they have spent countless hours in matching the intake runners to produce even airflow to each cyl. It is the even airflow and therefore the matching performance of each cyl that enables the E.I. to produce the improvements in fuel economy at altitude. It is my experience that it is extremely unlikely that a carbureted engine will have anywhere near matched performance of each cyl. With a E.I. your carbureted engine will start better and run smoother, but I don't think you'll get much improvement in fuel economy. I think the challenge for homebuilders in the future is not to produce faster airplanes but rather to produce better fuel efficiency. To better understand some of the ways to get that fuel burn down read John Deakins series of columns on how to operate airplane engines. They're at www.avweb.com. Good luck with your decision and with your new airplane. Bob -----Original Message----- From: owner-engines-list-server@matronics.com [mailto:owner-engines-list-server@matronics.com]On Behalf Of John Swartout Subject: Engines-List: Question about electronic ignition --> Engines-List message posted by: "John Swartout" <jgswartout@earthlink.net> As with most decisions in airplane building, I have a choice to make and have no solid basis for making the decision. I just ordered a Teledyne Mattituck Services TMX-360 carbureted ECI kit engine. I'm going to install dual electronic ignition, and leaning towards Jeff Rose's Electroair ignition over Klaus Savier's Lightspeed Plasma II. There are differences, and each will claim his version is better. Any users of these systems care to weigh in here? Thanks for the help. John




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