- 1. Rocker Geometry (score: 1)
- Author: "Brad Kahler" <Brad.Kahler@141.com>
- Date: Thu, 27 Sep 2001 05:05:11 -0600
- I'm in need of the following information for a 1296 spitfire engine...... "The rocker geometry is a funtion of the difference between the lift at the pushrod, and the lift at the valve. Stock TR (we
- /html/fot/2001-09/msg00156.html (7,471 bytes)
- 2. Re: Rocker Geometry (score: 1)
- Author: Gt6steve@aol.com
- Date: Thu, 27 Sep 2001 09:31:42 EDT
- Brad, The Spits and Sixes typically are quoted at 1.51 or 1.52 rocker ratio. << Listers, I'm in need of the following information for a 1296 spitfire engine...... "The rocker geometry is a funtion of
- /html/fot/2001-09/msg00158.html (6,618 bytes)
- 3. Re: Rocker Geometry (score: 1)
- Author: "R. Kastner" <kaskas@earthlink.net>
- Date: Thu, 27 Sep 2001 08:33:38 -0700
- To the best of my knowledge all the Triumph engines had a 1.5 ratio plus or minus a slight fraction. Kas Kastner -- Original Message -- From: "Brad Kahler" <Brad.Kahler@141.com> To: <fot@autox.team.n
- /html/fot/2001-09/msg00159.html (8,211 bytes)
- 4. Re: Rocker Geometry (score: 1)
- Author: "Timothy F. Murphy" <timmurph@execpc.com>
- Date: Thu, 27 Sep 2001 19:03:30 -0500
- You can measure the rocker geometry and figure the ratio as follows: Measure the distance from the center line of the valve stem to the center of the pivot point of the rocker. Measure the distance f
- /html/fot/2001-09/msg00162.html (6,997 bytes)
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