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FURIA 自制式直升機(jī) S, P( b/ {/ Z2 x5 S
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/ z% e" r# m5 T4 X. U, V2 uFURIA ULTRALIGHT HELICOPTER Plans 5 p; T. ^+ B. _. @' @7 P
FuriaHelicopter Specifications
& @5 R- n/ V& ~8 {' u+ i Main Rotor Diameter :
4 V8 n( H$ _" W K Main Rotor Blade Chord * ~: Z* S8 W0 n X( n+ ~/ m5 _
Main Rotor Speeds: ! K$ F. @! c6 Z) N0 Q
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Tail Rotor Diameter : * r* k! r' U2 {! d, c4 o
Tail Rotor Chord :
6 ]* P/ z% x# {5 m3 W# w Tail Rotor Speeds:
8 m8 K e4 V) T" Z5 H 5 q1 S3 V" C$ D& B3 T6 I
Length : % S, V/ o- U/ [% ]* a5 X/ \9 X& z
Height :
2 U/ J8 Y' i$ i) e Width :
7 H1 \* N6 B f- f) o) G5 b2 s Empty Weight : $ i: o5 M% J5 T& U2 s: s
Gross Weight :
~7 n) G' E1 w8 I* @* Q: K. d% U Payload ( w / full fuel ) :
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Rotax 582UL DCDI Engine :
. L5 g8 _2 M4 J V+ R. y Engine Weight :
* \5 Q* G8 e1 L; Z9 \/ w GearBox out :
; o0 _8 U6 P% H$ K4 r. W Fuel Capacity :
) g3 A3 Q3 G: W/ a3 V: l 5 o' {, \) [2 ^% o! ?$ S
Performance : ; |5 |5 \" f" s. e' ?0 H
Range : 2 P1 V) ^( `6 n$ F6 x% b, N9 g
Vmax :
3 `# I$ `! ^# G& U' l Cruise speed :
% M: B7 p7 x: R4 `! j" Y( b: o* q Climb rate (msl) :
0 d1 B6 P7 C$ d4 O4 D' m) e Service Ceiling :
, G6 X" |9 L+ T0 J# z' r& [ Hover in ground effect: % v0 t6 f' Q: ~6 u
Hover out of ground effect: 2 [" w7 w w6 x, A ~$ N
Max. Endurance ( K5 g9 F* m" K6 z- D% B% b: n
# ~' y" n* z) ` Design Load Factor : ! [& S4 U% x% i. b
3 C+ T, C. o& Y Seats :
1 N7 {/ [1 v4 w& r0 c6 {% ` Price: 18’500.00$
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8 A0 |7 `7 L# y l/ E4 J& B) e Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) / V/ H( e8 }/ g& z3 C' K$ G
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. + G$ j0 f! m* e! c
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