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FURIA 自制式直升机7 |# s3 E( t4 \; _
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FURIA ULTRALIGHT HELICOPTER Plans
7 Z0 u: o4 c% \FuriaHelicopter Specifications - T5 O' |4 T! r/ X6 B9 l. L
Main Rotor Diameter : 6 M. p+ r# Q7 X' d
Main Rotor Blade Chord ; B0 I. \* @( G' m# Z
Main Rotor Speeds:
$ n) J/ A' o; p E$ U+ O' ` 1 a7 O3 V: W6 L$ G) ]9 h/ e& }
Tail Rotor Diameter : 8 B& R) T/ Q4 d
Tail Rotor Chord : . B) _3 e4 S( k; i0 _
Tail Rotor Speeds: - j. R% Z3 f/ I, l6 M
2 _6 w; t1 I) v, B2 f Length :
( B( j7 L' L8 c# F Height :
' A# M3 i0 _0 S2 g Width : 9 p, ~" K4 _ P* F% L. Y
Empty Weight : $ D8 Z9 G9 @5 [; i
Gross Weight : ! I8 G _& M2 l9 I; r
Payload ( w / full fuel ) :
m0 r+ t& {) h. n8 ~, j
( @5 \# U/ X0 I Rotax 582UL DCDI Engine : * V' j% A- H8 r/ f0 A
Engine Weight :
2 y% p1 L& Y m% G# b6 H GearBox out :
/ R3 D6 z) s2 t+ ` Fuel Capacity :
$ Y9 O3 q8 h Y. O % f6 q& [, ^/ L( P
Performance : 9 Y" O* Q& {8 u( P" X; y
Range : 8 U7 P6 F4 \0 `9 {. A9 d
Vmax : & ? M. n8 k) X7 z, Q# _
Cruise speed :
+ m# f+ F, |* w4 |! z% } Climb rate (msl) : . v1 p4 ]' n# E
Service Ceiling :
0 W' i T, ~* M! x Hover in ground effect: 1 x' z( V4 a2 E2 u" F4 Y1 E
Hover out of ground effect:
( ^# ?- P b& z, |7 E @# a Max. Endurance
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( D& T5 T5 `9 A8 ? Design Load Factor : " {# Z! ?# g" A0 q& J' y5 `% v2 d
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Seats : 4 V5 w" B/ ^& |
Price: 18’500.00$
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Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations)
: h- H' @8 |+ @ 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. ) ? f5 @, l: Z1 o9 z$ V: B
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