Talk:Fan blade

It is utterly wrong for 'fan blade' to redirect to 'turbine blade'. The term 'fan blade' in gas turbine engines refers to the large first rotor stage of an axial compressor. The term 'turbine blade' is used to refer to the hot end (downstream of combustion) diffusion rotor blades, as illustrated in that page. Cebderby (talk) 00:20, 20 April 2018 (UTC)
 * You'd be best taking this to WP:RfD. Redirects often go entirely untouched for many years so this message may never get dealt with here. 89.240.136.195 (talk) 01:26, 20 April 2018 (UTC)