" \+ |1 Q. v+ M2 XFURIA 自制式直升机0 z6 C2 y l1 y; C7 T+ V
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$ _, z% f) T! O! p; kFURIA ULTRALIGHT HELICOPTER Plans
: a8 p0 Y9 ~! l9 Q5 tFuriaHelicopter Specifications
2 ~: n! ]0 A1 J2 h4 K1 G6 Z# O Main Rotor Diameter :
: k* e5 b8 E( A; F0 { Main Rotor Blade Chord
* ]/ r" [8 d k- l M: Z Main Rotor Speeds: $ |: p+ g: p }' N' O
) F( L+ D: A# l& t% p6 \$ q; d+ P9 n Tail Rotor Diameter :
9 \! b8 W0 ~% O" p Tail Rotor Chord : c# g! r! S2 E* }3 H2 x
Tail Rotor Speeds: 0 Y: m$ q6 N* {7 l* G- V
: x3 ]% x" e/ o: ^/ | Length :
% T3 G! S9 g) g* I- N Height : 0 B$ M+ f: e1 U% t( I/ |5 R
Width : 9 H# u* |4 _: d& M: X
Empty Weight :
1 J! B6 O0 L6 ~ Gross Weight : : K8 }( A: a2 z8 ~8 g
Payload ( w / full fuel ) : 9 J& c: F! {7 X: Z* t
$ ~' L1 y/ o c9 t Rotax 582UL DCDI Engine :
4 l$ R8 C# U. j T, ~% _ Engine Weight :
% V% t; P0 V' z" o9 e5 O" g1 n GearBox out : ! x0 L2 d4 x9 v2 t/ [8 A
Fuel Capacity : 0 I5 B9 K9 V l9 A' _) J
1 O( j0 k1 V, p6 i8 r4 Z Performance :
# p! f" w% o5 g$ f! X Range :
7 ^. g$ [8 d2 m, ?" z" C Vmax : - q0 f( r9 J7 x) H' b! B
Cruise speed :
. v/ u7 |7 \# c* t Climb rate (msl) : 4 }. w' d$ I' y+ f% h
Service Ceiling :
) D! r/ p6 [) ^ X' p" c Hover in ground effect:
! q+ o+ M4 {' h Hover out of ground effect:
A2 L# r0 A7 U/ N6 J0 I& w& r- a Max. Endurance
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Design Load Factor : % a/ W. H: i6 b, b; W9 s$ T
. `& L# F$ P5 o% D Seats :
+ e0 G" S* W- g& h- n% J! M Price: 18’500.00$ 9 _' t4 a) Q3 A( `5 j1 E: C$ \
% S4 @# \& W8 I* F Z Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) 1 B7 ^! z. W( X. K# ?2 m+ G6 ~
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.
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