Mailing List flyrotary@lancaironline.net Message #31695
From: Al Gietzen <ALVentures@cox.net>
Subject: RE: [FlyRotary] Re: Fuel system pressure bleed off
Date: Sat, 6 May 2006 07:29:42 -0700
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

Subject: RE: [FlyRotary] Re: Fuel system pressure bleed off

 

Hi Bill... Welcome back.

 

The bleed circuit came about as a result of two Eggenfellner Subaru accidents/incidents traced to fuel starvation.  They hashed it over on the Subaru group and the simplest solution was to add a bleed circuit between the fuel rail and the return line (bypassing the pressure regulator), allowing any trapped air to be easily forced out of the system.  Preventing "weeping" of the injectors was a secondary benefit.

 

The need for a bleed is dependant on fuel system design.  If you can be sure that there is fuel at the pump inlet for re-prime, then there is no need for a bleed.  IOW, if there is any point in the line upstream from the pump that is higher than the pump, there is potential for a bubble of trapped air.  Air at the pump inlet may not allow the pump to force any flow through the pressure regulator.

 

A good way to avoid injector ‘weeping’ (which would only happen on a faulty injector), or residual pressure in the rail, is shutoff the pump first in your shutdown sequence.

 

At least that’s my opinion  . . .

 

Al

 

 

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