Rick6a
Well Known Member
RE: Spinner Installation (Hartzell BA Constant Speed)
It is difficult for me to envision the limits of motion characteristic of a constant speed propeller and is the basis for my questions.
I have made the preliminary blade cutouts on Van's fiberglass spinner and have fitted it to the aircraft.
What is the recommended gap between the propeller blades and the spinner? As the first photo shows, for now I left the gap at approximately 1/8." Is this sufficient? Also, DWG C4 provides an illustration for the fabrication of filler plates to be installed directly behind the blades of a fixed pitch propeller. See photo on the right. It is unclear to me what dimensions I should seek when fabricating filler plates for the Hartzell constant speed propeller.
As you can see, my questions are based upon my lack of knowledge of the precise limits of motion of the prop blades around the hub of a constant speed propeller relative to its fixed spinner and thus the final shaping the spinner cut outs to account for such movement. Is there an approved way to rotate the prop blades to the full limits of travel around their respective hubs without causing (expensive) damage?
It is difficult for me to envision the limits of motion characteristic of a constant speed propeller and is the basis for my questions.
I have made the preliminary blade cutouts on Van's fiberglass spinner and have fitted it to the aircraft.
What is the recommended gap between the propeller blades and the spinner? As the first photo shows, for now I left the gap at approximately 1/8." Is this sufficient? Also, DWG C4 provides an illustration for the fabrication of filler plates to be installed directly behind the blades of a fixed pitch propeller. See photo on the right. It is unclear to me what dimensions I should seek when fabricating filler plates for the Hartzell constant speed propeller.
As you can see, my questions are based upon my lack of knowledge of the precise limits of motion of the prop blades around the hub of a constant speed propeller relative to its fixed spinner and thus the final shaping the spinner cut outs to account for such movement. Is there an approved way to rotate the prop blades to the full limits of travel around their respective hubs without causing (expensive) damage?