( S. n8 A5 a7 V$ A, E& O
FURIA 自制式直升机
3 k/ e5 X6 R$ F5 A* [. n- c" b: k1 [
$ d4 b( }0 Q! C) b% Z, U3 l, {
FURIA ULTRALIGHT HELICOPTER Plans 3 o6 ?! H: A+ R* O. ?5 t
FuriaHelicopter Specifications ! G1 q* S) ?; j& O0 z! G
Main Rotor Diameter : . q( H5 s% t" Z7 b# Q4 R: f3 S
Main Rotor Blade Chord
8 C, Q, @/ Q! n8 G3 j. c5 v2 f2 x Main Rotor Speeds: 6 J5 }( {4 [ A2 P! d9 F% g; T$ {
- z; B n: d; i' H, D
Tail Rotor Diameter :
; K% n; u, b2 u7 x Tail Rotor Chord :
9 H1 }* R# J* ]: ^+ ~ Tail Rotor Speeds:
% U# w: d% b: q- M) r' } 2 b4 G5 @# N7 I4 K- ?
Length :
4 P' I7 |( n) k M9 F2 L Height :
* S8 V& f6 _" |& ]0 F/ a Width :
5 [' Q: k r7 Y3 p$ |, M& F Empty Weight : , `- T, w2 i/ [: [9 y
Gross Weight : 3 _7 K- w( v" w. t) |9 P) Z9 F
Payload ( w / full fuel ) : 2 s: J1 @' Y+ [/ F2 M! _
9 u2 H7 z; ` C6 x Rotax 582UL DCDI Engine :
. }) d' U: ?& y/ D) j Engine Weight :
8 ?) D. x `% C) g. T" d GearBox out : 8 K' y z/ g' J# S2 x# x
Fuel Capacity : 6 g8 `* `2 B1 l
7 g1 |7 [6 ^' R
Performance :
( I0 }. O5 v# V$ i1 c- u Range : # I& n9 M9 W% u' ]
Vmax : $ |* ~$ d3 t& O, x: Y. X# G
Cruise speed : & {1 n' Q& t- q) t" S4 i
Climb rate (msl) : * v( z. n3 c- J/ c- n3 }
Service Ceiling :
; ?. S, C% s4 L% K _5 ] Hover in ground effect: " v/ h& ]+ G z+ l+ x0 K1 s) l$ `
Hover out of ground effect:
0 F/ d" Z% H* O, h7 P8 z+ l Max. Endurance 0 j7 {+ R& G& z
2 l" ~( E, n4 I1 i9 M! U
Design Load Factor :
/ u0 P) L1 N0 b1 y 6 C( F _4 c, v2 a
Seats : " D, j# c8 U* k" A. \
Price: 18’500.00$ : L8 I4 R) ?" Z7 j2 h
" z: g( K9 R3 i
Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations)
6 E3 n5 b& d( {9 A; \9 a) X The FAA has ruled that the maximum speed of 63 mph normally applied to fixed wing ultralights does not apply to helicopters due to their unique power curve. ; k d. J: e' {. F
9 n* x' G# Q5 D1 k) N
% s/ H9 U) `6 B8 W" O; x |