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Hangar Flying / Oil Heater
« on: July 26, 2006, 02:34:15 PM »
I may have missed something...but I think that you can build a safe oil cooler/heater installation in the nose of the plane without spending the money and gaining the weight of an additional oil pump (which, if it is feeding oil from the sump, which is at low pressure, needs to be able to pump cold oil, in order to be able to move cold oil through the system and replace it with hot oil).
You install a one-way valve on the return oil line at the point where it feeds back into the engine. You also install a cable-operated on-off valve in the oil line that feeds from the engine, again in the engine cpmpartment close to the engine feed take-off for the oil.
If you suspect an oil leak in the heater/cooler circuit in flight, you pull the shut-off cable, and the entire nose oil circuit is isolated from the engine, preventing any further loss of oil. You will lose your cabin heat, but a controlled cold descent with an engine is bettter than a controlled cold descent with no engine...
Bear in mind that you will have up to 1 quart of oil in the nose circuit that cannot be drained at each oil change, unless you devise a special arrangement to bleed that oil using a drain fitting or valve in the nose area at the lowest point in the nose circuit. If you are using a high-pressure feed from the engine oil gallery, that may be more difficult to engineer than a circuit using low-pressure oil from the sump. Depending on where your engine compartment oil cooler is currently mounted, this may or may not be a negative operating factor. In my case, the current oil cooler is mounted at the top of the firewall, and cannot be drained at a normal oil change unless you remove the cooler from its mounting, disconnect it from the circuit and drain it separately. So, with my current configuration, moving the cooler to the nose does not make the oil retention problem much worse. (I plan to remove the engine compartment oil cooler and replace it with a Setrab cooler in the nose, since I currently do not have an oil cooling problem in the engine - I have to blank off the cooler in the winter to get the temperature up to 180 degrees).
You install a one-way valve on the return oil line at the point where it feeds back into the engine. You also install a cable-operated on-off valve in the oil line that feeds from the engine, again in the engine cpmpartment close to the engine feed take-off for the oil.
If you suspect an oil leak in the heater/cooler circuit in flight, you pull the shut-off cable, and the entire nose oil circuit is isolated from the engine, preventing any further loss of oil. You will lose your cabin heat, but a controlled cold descent with an engine is bettter than a controlled cold descent with no engine...
Bear in mind that you will have up to 1 quart of oil in the nose circuit that cannot be drained at each oil change, unless you devise a special arrangement to bleed that oil using a drain fitting or valve in the nose area at the lowest point in the nose circuit. If you are using a high-pressure feed from the engine oil gallery, that may be more difficult to engineer than a circuit using low-pressure oil from the sump. Depending on where your engine compartment oil cooler is currently mounted, this may or may not be a negative operating factor. In my case, the current oil cooler is mounted at the top of the firewall, and cannot be drained at a normal oil change unless you remove the cooler from its mounting, disconnect it from the circuit and drain it separately. So, with my current configuration, moving the cooler to the nose does not make the oil retention problem much worse. (I plan to remove the engine compartment oil cooler and replace it with a Setrab cooler in the nose, since I currently do not have an oil cooling problem in the engine - I have to blank off the cooler in the winter to get the temperature up to 180 degrees).