v9 s5 @% H7 k; W$ g% p% Q; P7 {
FURIA 自制式直升机" w @) h, B! r. Y# k; M
4 O, G; Y# f4 G n+ g
' ]: j G1 v8 G( ?6 jFURIA ULTRALIGHT HELICOPTER Plans
0 _5 p- P; K2 b+ `" z9 t# WFuriaHelicopter Specifications 1 q% \5 t# k5 f
Main Rotor Diameter :
. E, I5 ]# U* N1 |& { Main Rotor Blade Chord 0 h3 h7 K- f3 G. K1 L0 M, C7 a- C* |
Main Rotor Speeds: 8 B& v) `. S: r3 ?2 x
& p% J9 ]! x# Y Tail Rotor Diameter :
" N3 c) ?' z$ @ Tail Rotor Chord : : t/ R! b: n1 f1 K' E k" t
Tail Rotor Speeds: - Z! _# [( \+ L& h
: k- a# x' s; P- x" c E7 c
Length :
6 e( S" {5 }( Y- L% h% F7 ?3 } Height : ' {" R% U7 y2 L/ Y. E( Q& A# Z
Width :
6 A" q+ n4 ^) B! p- v Empty Weight : ) x& T; q. \' z4 t
Gross Weight :
7 H/ j2 [! ~8 W3 R Payload ( w / full fuel ) : 7 X( f* z$ @5 z( {! B
/ t0 ]+ G& X+ t/ h M3 f
Rotax 582UL DCDI Engine :
0 y1 a7 o/ L1 p" \6 @ Engine Weight : 5 m2 g7 J, n/ M: C
GearBox out :
- A# i% @: D; u/ d) o Fuel Capacity : 9 i+ K0 c' `7 E* _: \ l! b
1 x5 Z$ g' T& h Performance :
* K; E; b, i4 K# J Range : 6 ?. v. [7 L0 f7 a! Y
Vmax : ! [" _! Q! |" B7 w
Cruise speed : + I' |7 x( e6 L$ B- {' a' s
Climb rate (msl) : % R0 @9 L( w. c" _* n$ Z! K( N0 ]- H
Service Ceiling : " [2 A9 t4 o; B
Hover in ground effect: 3 c' s% O* C- ~5 B) v
Hover out of ground effect: . ~9 ]) m5 Z9 S% y: e/ d. N
Max. Endurance . h: q4 \8 K# e* l# q2 ^
* K+ E) a/ B6 K+ ~ Design Load Factor : # s0 U& B( c6 V+ R0 x" L6 Q
$ \, H/ U6 K* O8 Q. K" x2 @& K
Seats : " Q7 l) T! z+ P# E N- ]
Price: 18’500.00$ . D% e% m& E# G" K0 L
* f- z: ?; T0 d. p Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) 0 Y! ~9 r3 T' u7 m7 d2 U1 t
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.
- l$ l/ X3 l, A8 a/ G
+ L: {; b0 O9 N' [( F, t
( o* |0 i5 ? X# `, H8 D |