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' L! ^# Q5 j* ?1 D) u$ G6 iFURIA 自制式直升機
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5 O+ P0 f. j7 iFURIA ULTRALIGHT HELICOPTER Plans 1 t9 |/ K( u9 Q8 y) Z( V+ z
FuriaHelicopter Specifications
; p0 Y9 x* B/ @$ N8 Y Main Rotor Diameter : $ v0 h1 S6 [( s
Main Rotor Blade Chord - P: l; m* `2 B6 A0 t
Main Rotor Speeds:
9 F/ ~1 {: W# c& k0 A R0 A
/ k/ g) k# i7 `3 s1 t% R% h Tail Rotor Diameter :
7 b% S7 ]! S9 a( m- A, I9 ~0 G Tail Rotor Chord : 0 T+ [' I4 s0 `( S
Tail Rotor Speeds:
; F" M" y7 b# \2 r/ a
. W+ s- ^/ f, _6 h/ s# b Length :
6 o2 _ t! S, {" z) ~ Height :
3 R/ i# k+ E; S Width : ; c) u5 E3 j; J; A$ I
Empty Weight : # T; k* l; ~7 y( A8 s6 m% K
Gross Weight : p. }) R& ^. ]1 K+ N
Payload ( w / full fuel ) :
0 Y- i9 w- w1 h. E) R" ]) T+ v 9 r+ L+ r" H% z& G1 c Q
Rotax 582UL DCDI Engine :
) x" g/ ]) s: Z- g* A2 c G Engine Weight :
" v' _, S7 `) _- p U GearBox out : 5 a# e4 F% L9 x2 Z
Fuel Capacity :
" [ K/ }6 }* `) q $ D" E0 r$ u" ~4 @# W2 b
Performance : 2 C ^" e( X& I1 E( S
Range : . d4 g8 s6 E4 i# R. ~# o
Vmax :
% ]1 d F: z) C1 [2 S Cruise speed : ) J8 T b5 a6 ^
Climb rate (msl) : 3 J K9 W( u! h$ y0 k
Service Ceiling : - n# Q) V2 \: N% A% a
Hover in ground effect:
. H/ X0 F6 w5 @" P# U: ?: E Hover out of ground effect: 9 f* g# O5 E" y2 [
Max. Endurance
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Design Load Factor : 8 \, W3 `% S, {% i5 o- _+ w6 s5 L
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Seats : 6 g& Z; A; y0 k: p* y# C7 O M# s
Price: 18’500.00$
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/ g/ Y8 Y- |8 i4 [1 ^/ R9 ]" N Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) : q2 h2 x7 I7 ?
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. - q7 R, t1 s8 E0 c2 j' o- U
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