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FURIA 自制式直升機(jī)
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0 h) R ` x0 C, _6 Y2 B# _2 IFURIA ULTRALIGHT HELICOPTER Plans - Y4 U+ _1 _- @
FuriaHelicopter Specifications
6 E0 K6 f; A# C5 t% A# L5 | Main Rotor Diameter : 1 p8 Z0 w# b! u% }& O
Main Rotor Blade Chord
2 ?& C$ c. V+ R! R! y Main Rotor Speeds: 0 X+ K/ z6 \0 m
' F, B+ `" N% x Tail Rotor Diameter :
7 a. ~# j: W- L. S Tail Rotor Chord : : w! F% L Y O% Z; {6 K5 P5 W/ k
Tail Rotor Speeds:
, E |; ~4 I2 V' k" r& p 3 c: c9 G$ V8 a4 ]
Length : + f7 d* W I4 \" q q9 X% A
Height : ( c' C& ~% R. _% t: o! x- m% O" M9 O
Width :
, E; K5 d/ v8 g4 A0 j. b) w7 c* k Empty Weight : ' f/ ]$ u [$ v/ G7 n# I
Gross Weight : 4 \) Y9 z7 ?& H k* ~ [3 F- z/ U
Payload ( w / full fuel ) : ) z/ F2 P9 [' k9 t& T) }- z
' P+ X; \+ o+ n Rotax 582UL DCDI Engine :
: g J4 F# N2 r& ]# B" `. Z+ P$ { Engine Weight :
" `# j* a+ d0 K+ E+ U; \3 Y/ Q ~ GearBox out :
8 M* l# N9 Y% x( H+ m$ J3 y2 P Fuel Capacity :
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9 _0 F! H) ]3 u- Y# F+ @8 O2 x% Q+ n Performance :
7 |3 w p$ |4 Q5 i, {* w Range :
: e( S0 Z: P: b- C% u Vmax :
* n5 U+ H& X1 D: A; R0 V! d! @ Cruise speed :
0 K6 W, U1 ~: r0 D" I7 D" t Climb rate (msl) : 0 `2 q: z8 M0 a( u1 A
Service Ceiling :
( p8 t3 J) X" n3 R- m# {* m' L n Hover in ground effect:
# Z5 N2 F& P, D% {. ~- X Hover out of ground effect:
% [3 V2 H [' \/ c Max. Endurance
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Design Load Factor : ' K( D9 j6 @9 `# F# d
5 x# |1 l$ k5 p# |
Seats : 1 i9 C/ m7 t( D' [ r2 @! L% }
Price: 18’500.00$ 5 z3 b# N! a' k* O
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Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) $ _6 z1 A! C% j1 Q5 D0 w
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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