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Is that really enough? What's your actual flow rate - not just the burn rate - at "war emergency" power? I would think that good engineering practice is to have a supply capacity that exceeded that flow by about 20%.
Dale R.
COZY MkIV #1254
From: Finn Lassen <finn.lassen@verizon.net>
Date: 2004/11/27 Sat AM 10:16:52 EST
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Subject: [FlyRotary] Re: Bubbles in fuel line from pump - new valve
That's right. Oddly enough it will gravity flow about 17 GPH through that hole.
Finn
Bulent Aliev wrote:
>>The inlet hole to the flow sensor turbine is only 1/8" !
>> >>
>
>Finn, are you saying that all the fuel going to the engine has to be sucked
>through an 1/8" hole? If that's the case, this could be your problem?
>Bulent
> >
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