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' w/ n! L: B7 E% YFURIA 自制式直升機
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- L& k. Q2 }: Z T, j" | LFURIA ULTRALIGHT HELICOPTER Plans
, V1 @2 u3 j- D7 H# F6 [3 X* aFuriaHelicopter Specifications / W) D) [" I! U- @
Main Rotor Diameter :
4 A# S; |' \* m) E2 M$ Q Main Rotor Blade Chord
" P; c1 W2 D; F0 V3 K Main Rotor Speeds:
0 U& l$ X* f$ Y& Z - X+ B, t) B# U+ n
Tail Rotor Diameter :
6 c1 u' W4 z0 H8 a Tail Rotor Chord : N9 B$ E6 ]" p) `4 e
Tail Rotor Speeds:
6 k- S# p, y* F' F4 S& j ; y. R% {5 v: f) a
Length :
8 y0 Y( M" O2 ? k# P2 k- o Height :
* {! O0 \$ e5 i+ b- { Width :
" ^9 Z5 f7 M0 z4 s8 _3 {7 L1 M+ r8 z: S Empty Weight :
. U" x1 E; b) b+ J Gross Weight : 1 H% P+ r# w, \$ Z+ S. ^
Payload ( w / full fuel ) : ; G) G. G) G8 l1 Q6 Z6 q# }
* M, u; {- u! z Rotax 582UL DCDI Engine : 7 W; I( x0 V; H! V
Engine Weight : * i4 m- ?; L- `9 `; k, B9 ?
GearBox out : # c' w* X9 x. B7 t# K: ~+ d
Fuel Capacity : " c& z& y7 h) ?6 L9 }5 `0 P; w
& g" r* C- e# k( I) {5 L& y2 ` Performance : * T. a5 |" t+ o. `
Range :
3 A0 z9 a- V* V$ r- B$ x Vmax : ' N, ]* y/ N& j, o
Cruise speed : " r* G q: A/ T- Q1 G4 E
Climb rate (msl) : ( o. O, R$ T4 N1 i; Q9 [8 |* F
Service Ceiling :
+ I0 K2 u, D' j) [4 W( F Hover in ground effect:
/ r9 A- A7 |5 ]" \) R+ i Hover out of ground effect: 9 d2 x8 @/ H# a) ^7 f4 N# c' l% R
Max. Endurance
8 v4 `& c; s. z, y* u: ~
* b, o3 @% S! B) P0 z( Z; \9 x Design Load Factor : , r' l; _. {5 z9 j j
2 B$ X$ c, ]9 x$ D: O5 f- F( v6 A Seats :
6 d% F+ A9 _3 ?7 U7 m d Price: 18’500.00$ 6 [& P! {9 W. P" G' W
! ?- q, r3 D8 h# k Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) + y7 F: y- D" a
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. ) z0 s! P5 S/ V4 o# p
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