X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail-gw0-f52.google.com ([74.125.83.52] verified) by logan.com (CommuniGate Pro SMTP 5.4.1) with ESMTPS id 5109704 for flyrotary@lancaironline.net; Wed, 31 Aug 2011 14:30:18 -0400 Received-SPF: pass receiver=logan.com; client-ip=74.125.83.52; envelope-from=rwstracy@gmail.com Received: by gwj15 with SMTP id 15so516349gwj.25 for ; Wed, 31 Aug 2011 11:29:43 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=gamma; h=subject:references:from:content-type:x-mailer:in-reply-to :message-id:date:to:content-transfer-encoding:mime-version; bh=CksaqMRuzLfgTgzm2VcRKaMBAD3fmjZHoLqJnSEIFt0=; b=iJQd6TYmwFOfmHBNcwdsxs18TsNF+RpiUAwpPw4DHEKxm1duLxS5aDlQ6TAYhxvsUn sqDYGQgKX4abby0u9tmYh2SHoPg0nausavfvGI4roOfWdVC5MGlzQZyIKEJ5N7EVhRCK gCoCc0fvkor3ty/veX5vM/xgFda9jIcY4iWrQ= Received: by 10.91.108.10 with SMTP id k10mr603470agm.158.1314815382984; Wed, 31 Aug 2011 11:29:42 -0700 (PDT) Return-Path: Received: from [10.0.1.2] (99-197-145-127.cust.wildblue.net [99.197.145.127]) by mx.google.com with ESMTPS id o8sm7493346anm.33.2011.08.31.11.29.33 (version=TLSv1/SSLv3 cipher=OTHER); Wed, 31 Aug 2011 11:29:41 -0700 (PDT) Subject: Re: [FlyRotary] Re: CG Products Intake Manifold References: From: Tracy Content-Type: multipart/alternative; boundary=Apple-Mail-73--646760266 X-Mailer: iPad Mail (8F191) In-Reply-To: Message-Id: <97265783-7329-455A-A2A1-1A351C593F5B@gmail.com> Date: Wed, 31 Aug 2011 14:29:19 -0400 To: Rotary motors in aircraft Content-Transfer-Encoding: 7bit Mime-Version: 1.0 (iPad Mail 8F191) --Apple-Mail-73--646760266 Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset=us-ascii Have to agree with Al W. on this one. I have never seen smoking gun eviden= ce that vapor lock occurs in the fuel rails. I have seen MANY smoking guns= pointing at problems in the pump inlet circuit. =20 That pump inlet filter on Bobby Hugh's installation raised a big red flag fo= r me as a possible cause of his power failure. It looks like the identical f= ilter that caused the same problem on my 20B. Ed Klepis talked with me abo= ut the problem but unfortunately Bobby is not communicating about it AFAIK. = =20 BTW, Here is one piece of advice when you experience a power loss at high t= hrottle. All engine systems are under maximum stress at full power and it i= s often the case that if you ask a bit less of them, they might work better.= I understand the urge to firewall the throttle when power sags at takeoff= but TRY reducing throttle momentarily to see if you get better engine perfo= rmance. This has saved me from at least three aircraft accidents. When th= at clogged inlet filter caused a power sag in the RV-8, backing off on the t= hrottle lowered the fuel demand of the engine and the fuel pressure recovere= d enough to let the engine run normally at reduced throttle. Same thing ap= plies to other situations. When my Rotax powered Twinstar started loosing p= ower on climb out I reduced throttle and the engine recovered. Piston seiz= ure was the problem but reducing throttle let the piston cool a bit and tota= l seizure was avoided. I replaced rings & scuffed pistons after nursing it= 80 miles to home. Tracy Sent from my iPad On Aug 31, 2011, at 9:50 AM, "Al Wick" wrote: > =20 > So you are saying every car built since 1990 has this "vapor lock" problem= ? We would see thousands of cars unable to start at every desert truck stop.= This concern for fuel rail is a myth. > =20 > Vapor lock is not a myth. It occurs at the fuel pump inlet. Very important= to minimize pressure drop there. You can actually measure how far your desi= gn is from vapor lock. You don't have to guess. > =20 > The bleed helps if you totally blew the plumbing from tank to fuel pump. B= ut much better to fix that plumbing error. =20 > =20 > =20 > -al wick > ----- Original Message ----- > From: Dave > To: Rotary motors in aircraft > Sent: Tuesday, August 30, 2011 9:14 PM > Subject: [FlyRotary] Re: CG Products Intake Manifold >=20 > HOWEVER..... if there is not a method to bleed down the rail the risk of v= apor lock exists, as the rail heats, the fuel boils, and the vapor gets trap= ped in the line. >=20 > If you DO put the regulator upstream of the rail, its imperative to be abl= e to be able to flow fuel past the injectors and to a return line to avoid a= ny possibility of vapor lock. The easiest way is simply to put the regulator= downstream of the rail and injectors, but again.. this arrangement is more a= bout preventing vapor lock, not ensuring adequate pressure.=20 >=20 > Chris and I were forced into the upstream approach by the Mistral fuel rai= l configuration, and I didn't want to mess with drilling out the pinhole and= then running a regulator downstream - Mistral was hard enough to get the in= take from, and we didn't expect getting a replacement part if we had an OOOP= S would have been easy. As others have now found out, Mistral isn't selling p= arts.=20 >=20 > So... anyways.. just wanted to clarify previous post. 1) can regulate pre= ssure anywhere in the fuel circuit between pumps and injectors. 2) Must prov= ide for mechanism to flow fuel past injectors to prevent vapor lock. >=20 > Dave >=20 > On 8/30/2011 11:06 PM, Dave wrote: >>=20 >> No... at the flows and pressures we are using (and barring any major obst= ructions between the regulator and the injectors), the regulator can be anyw= here in the circuit and adequately regulate the pressure. >>=20 >> On Chris Barber's install, I purchased the Mistral intake for use on his e= ngine. The fuel rail was a dead end tube with a pinhole on the end. Presumab= ly the pinhole was to prevent vapor lock in the fuel rail. The regulator HAD= to be upstream of the injectors when using the intake. We had stable fuel p= ressures and no problems getting fuel to the engine.=20 >>=20 >> We had return lines from the pinhole end of the rail, as well as from the= pressure regulator, that fed back to the sump tank. Since there were not ch= eck valves running from the wings to the sump, there was no chance of pressu= rizing the sump.=20 >>=20 >> Dave >>=20 >> On 8/30/2011 10:30 PM, CozyGirrrl@aol.com wrote: >>>=20 >>> Ed, I must have mispoke to give this impression, I thought the pressure r= eg HAD TO be last in line to maintain pressure in the fuel rail? >>> =20 >>> =20 >>> Chrissi & Randi >>> www.CozyGirrrl.com >>> CG Products, Custom Aircraft Hardware >>> Chairwomen, Sun-N-Fun Engine Workshop >>> =20 >>> In a message dated 8/30/2011 10:13:53 P.M. Central Daylight Time, eander= son@carolina.rr.com writes: >>> If the pressure regulator is place before the injectors then there is l= ess fresh fuel flowing through the rails.=20 >>=20 >=20 --Apple-Mail-73--646760266 Content-Transfer-Encoding: quoted-printable Content-Type: text/html; charset=utf-8
Have to agree with Al W. on this one. &= nbsp; I have never seen smoking gun evidence that vapor lock occurs in the f= uel rails.   I have seen MANY smoking guns pointing at problems in the p= ump inlet circuit.  

That pump inlet filter on= Bobby Hugh's installation raised a big red flag for me as a possible cause o= f his power failure.  It looks like the identical filter that caused th= e same problem on my 20B.   Ed Klepis talked with me about the problem b= ut unfortunately Bobby is not communicating about it AFAIK.  

BTW,   Here is one piece of advice when you experience a= power loss at high throttle.  All engine systems are under maximum str= ess at full power and it is often the case that if you ask a bit less of the= m, they might work better.   I understand the urge to firewall the thro= ttle when power sags at takeoff but TRY reducing throttle momentarily to see= if you get better engine performance.  This has saved me from at least= three aircraft accidents.   When that clogged inlet filter caused a po= wer sag in the RV-8, backing off on the throttle lowered the fuel demand of t= he engine and the fuel pressure recovered enough to let the engine run norma= lly at reduced throttle.   Same thing applies to other situations. &nbs= p; When my Rotax powered Twinstar started loosing power on climb out I reduc= ed throttle and the engine recovered.   Piston seizure was the problem b= ut reducing throttle let the piston cool a bit and total seizure was avoided= .   I replaced rings & scuffed pistons after nursing it 80 miles to= home.

Tracy


Sent from my iPad

On Aug 31, 2011, at 9:50 AM, "Al Wick" <alwick@juno.com> wrote:

<if there is not a method to bleed down the rail the risk of vapor l= ock=20 exists
 
So you are saying every car built since 1990 has this "vapor lock" prob= lem?=20 We would see thousands of cars unable to start at every desert truck stop. T= his=20 concern for fuel rail is a myth.
 
Vapor lock is not a myth. It occurs at the fuel pump inlet. Very import= ant=20 to minimize pressure drop there. You can actually measure how far your desig= n is=20 from vapor lock. You don't have to guess.
 
The bleed helps if you totally blew the plumbing from tank to fuel= =20 pump. But much better to fix that plumbing error.  
 
 
-al wick
----- Original Message -----
From:=20 Dave=20
Sent: Tuesday, August 30, 2011 9:14= =20 PM
Subject: [FlyRotary] Re: CG Product= s=20 Intake Manifold

HOWEVER..... if there is not a method to bleed down the rai= l=20 the risk of vapor lock exists, as the rail heats, the fuel boils, and the=20= vapor gets trapped in the line.

If you DO put the regulator upstrea= m of=20 the rail, its imperative to be able to be able to flow fuel past the injec= tors=20 and to a return line to avoid any possibility of vapor lock. The easiest w= ay=20 is simply to put the regulator downstream of the rail and injectors, but=20= again.. this arrangement is more about preventing vapor lock, not ensuring= =20 adequate pressure.

Chris and I were forced into the upstream appro= ach=20 by the Mistral fuel rail configuration, and I didn't want to mess with=20 drilling out the pinhole and then running a regulator downstream - Mistral= was=20 hard enough to get the intake from, and we didn't expect getting a replace= ment=20 part if we had an OOOPS would have been easy. As others have now found out= ,=20 Mistral isn't selling parts.

So... anyways.. just wanted to clarif= y=20 previous post.  1) can regulate pressure anywhere in the fuel circuit= =20 between pumps and injectors. 2) Must provide for mechanism to flow fuel pa= st=20 injectors to prevent vapor lock.

Dave

On 8/30/2011 11:06 PM,= =20 Dave wrote:=20
No... at the= flows=20 and pressures we are using (and barring any major obstructions between t= he=20 regulator and the injectors), the regulator can be anywhere in the circu= it=20 and adequately regulate the pressure.

On Chris Barber's install, I= =20 purchased the Mistral intake for use on his engine. The fuel rail was a d= ead=20 end tube with a pinhole on the end. Presumably the pinhole was to preven= t=20 vapor lock in the fuel rail. The regulator HAD to be upstream of the=20 injectors when using the intake. We had stable fuel pressures and no=20 problems getting fuel to the engine.

We had return lines from th= e=20 pinhole end of the rail, as well as from the pressure regulator, that fe= d=20 back to the sump tank. Since there were not check valves running from th= e=20 wings to the sump, there was no chance of pressurizing the sump.=20

Dave

On 8/30/2011 10:30 PM, CozyGirrrl@aol.com wrote:=20
Ed, I must have mispoke to give this impression, I thought the=20= pressure reg HAD TO be last in line to maintain pressure in the fuel=20= rail?
 
 
Chrissi=20 & Randi
www.CozyGirrrl.com
C= G Products, Custom=20 Aircraft Hardware
Chairwomen, Sun-N-Fun Engine Workshop
 
In a message dated 8/30/2011 10:13:53 P.M. Central Daylight Time,= e= anderson@carolina.rr.com writes:
  If the pressure regul= ator is place before=20 the injectors then there is less fresh fuel flowing through the=20 rails. 


= --Apple-Mail-73--646760266--