It is currently Sat Nov 23, 2024 11:26 pm



Reply to topic  [ 25 posts ]  Go to page Previous  1, 2
 R44s grounded in Australia 
Author Message
User avatar

Joined: Tue Nov 05, 2013 9:30 pm
Posts: 1248
Location: UP A GUMTREE
Has thanked: 1949 times
Been thanked: 1688 times
TitaniumAutoGyro carbon composite rotor ... in extreme stress testing.... Neils brief email report...... & picture!


"Some additional test done yesterday on blades ,

The required flexion test was done with a safety factor of 3.25 needing a load of 40.5 KG .

We then kept loading the blade to see what would happen and they took it up to over 660 Kg and still couldn’t break the blade

They then did a shear load test on the root end of the blade and exceeded 2055 KG and couldn’t break the blade , this would normally be negligible in flight because everything is relying on centrifugal force not shear , but just goes to show the strength of the blade .

If you had a aluminium blade you could not reach anywhere near these test figures .

Regards

Neil


You do not have the required permissions to view the files attached to this post.

_________________
Image


Sat Feb 28, 2015 2:42 pm
Profile
Online
User avatar

Joined: Thu Nov 07, 2013 12:56 am
Posts: 3073
Location: VERY LOW LOW LOW EARTH ORBIT
Has thanked: 3078 times
Been thanked: 3854 times
An unrealistic 'test' the whole machine would of quit flying long before the loads would get that high.

High cyclic low load test would suite it better.

resonance with airframe / cyclic fatigue more of a problem not outright strength. :bunny


Sat Feb 28, 2015 4:06 pm
Profile
Online
Site Admin
User avatar

Joined: Tue Sep 02, 2014 7:45 am
Posts: 10129
Location: Poona, Qld, OZZY
Has thanked: 21874 times
Been thanked: 6221 times
You are quite correct Hillbilly, however, even tho it will be physically impossible for the rotors to be in this predicament in flight (bar in a crash) I think it is comforting to know that the rotors themselves are that tough....Knowing Neal, all of the centrifugal and other normal load testing will follow and be equally as thoroughly tested..... Neal is very methodical in his approach to everything, by the time he is prepared to release the rotors for sale, he will know every single imaginable figure as to their performance whether stationary, turning on the ground or in flight.... I think that is a good thing, as I am sure anyone purchasing (or thinking of purchasing) a Titanium will agree :like :laughing :wol2 :Wolvie

_________________
I do all of my own stunts..... most of them are even planned! Ok, Ok.... some of them are planned..

If electricity comes from ELECTRONS, then surely morality comes from MORONS??


Sun Mar 01, 2015 6:07 am
Profile
User avatar

Joined: Tue Nov 05, 2013 9:30 pm
Posts: 1248
Location: UP A GUMTREE
Has thanked: 1949 times
Been thanked: 1688 times
SHEESH!!!!

:whip :whip :whip ...... for you detail-challenged readers .... :calmdown .

READ AGAIN ..... FIRST LINE of Neil's email......

. Some additional test done yesterday on blades ,

Knowing how detail-orientated a guy is Neil & those blade guys ( manf for helo rotors) ..... those other tests were LONG done!!!!!


:head

:dropbear

_________________
Image


Sun Mar 01, 2015 10:14 am
Profile
Online
User avatar

Joined: Thu Nov 07, 2013 12:56 am
Posts: 3073
Location: VERY LOW LOW LOW EARTH ORBIT
Has thanked: 3078 times
Been thanked: 3854 times
Tested to what standards? :bunny :pbunny


Sun Mar 01, 2015 1:44 pm
Profile
Reply to topic   [ 25 posts ]  Go to page Previous  1, 2

Who is online

Users browsing this forum: Freebird, Henry Bowman, skyguynca and 779 guests


You cannot post new topics in this forum
You cannot reply to topics in this forum
You cannot edit your posts in this forum
You cannot delete your posts in this forum
You cannot post attachments in this forum

Jump to:  
Powered by phpBB® Forum Software © phpBB Group
Designed by ST Software.
Americanized by Maël Soucaze.