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| This page describes a
simple method of making a two bladed composite propeller. The basic idea
is to make an open mold using an existing propeller as a plug. The curved
side of the new propeller is made in the mold and the flat side is filled,
ground, filed and sanded for the proper shape. This method requires the
use of metal bushings (inserts) for propeller bolts instead of drilling
holes and cutting fibers in the prop hub. The method was successfully used
in making the propellers for the ATE-3 and JT-5 autogyros. Since the laminating procedure is a pretty messy business I never took photos of the actual work. Instead I am using schematic pictures made using ClarisDraw and form•Z programs. What are the characteristics of a composite propeller: 1) Easy to fabricate. What are the drawbacks of a composite propeller: 1) It may be too strong! In an aircraft with retractable gear a belly
landing may result in a damaged crankshaft. THEREFORE, NOTE THE FOLLOWING! 1) Don't use polyester resins, they are not
heat resistant. Always use the best heat resistant
epoxies. MAKING THE PROPELLER MOLD. 1) Make a copy of the propeller flange in steel or aluminium and bolt
it onto the curved side (pusher side) of the prop serving as a plug. In
some cases like VW based engines you can use the original prop
flange. |
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| Laminating the Mold on the Plug | ||||||||||||||||||||||||
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LAMINATING THE PROPELLER IN
THE MOLD:
When the mold has been completed take the following steps to make a composite propeller: 1) Calculate the desired pitch of the propeller at .75 R and at the
tip. You may try the various propeller
design programs in the net. Adjust the pitch screws as
necessary. |
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| Mounting the propeller on
the propeller flange.
The picture below shows the right and wrong method to install the propeller on the flange. It is dangerous to install the propeller so that the thin threaded portion of the bolts will carry all the torque loads. The propeller flange must have long nuts to carry the torque loads. In addition, use conical spring washers under the bolt heads to prevent any play from arising if the propeller shrinks due to an exessively hot flange. |
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| If you have any comments on this page, send me e-mail! | ||||||||||||||||||||||||
| COMMENTS
I've just found your composite propeller page and want
to tell you my compliments. It is a wonderful page. Note: Great prop making ideas. I added a link to your site
on our site. I might suggest you orient the carbon cloth plus and minus 45
degrees for increased torsional blade stiffness. Also use a metal blade as
a mold when ever possible to take advantage of the increased prop
efficiency afforded by the thinner blade. Thanks for doing that. Many of
our readers need that sort of information.
Although this looks interesting please read below. DISCLAIMER As with all amateur built aircraft, the aircraft builder has final responsibility for engineering soundness, installation practices, and compliance with national regulations. Since there can be a huge variation in builder skills and actual practices, no warranty of engineering soundness or applicability is made or implied. This Website represents "the way others have done it " and is presented for peer review and educational purposes only.
RELEASE OF LIABILITY IF YOU CANNOT BE RESPONSIBLE FOR YOUR OWN ACTIONS YOU ARE HEREBY DIRECTED NOT TO USE ANY OF THE INFORMATION PRESENTED IN THIS OR RELATED DOCUMENTS.You, the aircraft builder, understanding that the information contained in this and related documents is of an experimental nature and is not approved by any national authority and is not approved for aircraft use; Whereas: If you choose to implement any of the ideas presented you hereby agree to be solely responsible for any outcome resulting from your own choices and actions. Whereas: You agree to hold the Webmasters / site owner and authors harmless from, and the aircraft builder hereby assumes, the entire liability for any and all damage or injury of any nature whatsoever, including death. Whereas: You agree to indemnify and hold harmless any author from and against any and all loss, claim, expense, damage or injury that the aircraft builder may sustain.
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