GRYF magazine
GRYF magazine
News about Gryf and more...
information about Shark first prototype max speeds |
20th December 2009, Shark prototype OK - OUR 01 reached with propeller Woodcomp 3000 2W :
( Shark.aero sro information from test flights in Senica airport ) |
Weather in Czechia
003 final rear fuselage strength test |
Written by Jaroslav Dostál |
Wednesday, 13 October 2004 00:00 |
003 was strength tested in test bed for ultimate loads according to Czech UL2/2 and Germany LTF requirements: - Rear fuselage test for ultimate combination loads - Rear fuselage test for ultimate symmetrical loads All these loads was created in test bed by sand bags, checked by digital loads measurement. Result - OK, no continuing deformation till max. operational loads. Continuing deformation after 100% of ultimate loads were in “measurement mistake” range - and in fuselage rear cone only. We will increase strength by reinforcing of fuselage rear strength system to 120% for next serial production. In the same time we have aircraft empennages calculated for VD 300 km/hour, to have possibility to increase speeds in next aircraft models. |