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8 O' c" k: N! S' [2 Y3 aFURIA 自制式直升機(jī)& f4 d9 k( O! b9 b
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FURIA ULTRALIGHT HELICOPTER Plans 4 i, B0 u7 Y% q/ u1 f
FuriaHelicopter Specifications 2 ~" Z0 g* W2 }8 N. T
Main Rotor Diameter : * n! k; x! B. O8 a7 W0 x. n! |! r& L
Main Rotor Blade Chord
2 I$ K" ~) T Z/ D4 u& X Main Rotor Speeds:
, S: ]3 X, _" A, x $ p' p b" A2 H4 }3 S9 m$ d
Tail Rotor Diameter :
2 t) [% z2 h, m( a" @/ ^6 S) |: c Tail Rotor Chord :
1 `; Q: ^+ j3 b( M) o; F& r! ? Tail Rotor Speeds: ( \6 P/ q, i3 E( [
+ K! v& V! e, e: K
Length : . A- v3 \/ C4 p- h
Height : 5 z% f9 Z% q% \4 Z3 u
Width :
4 j1 q+ d2 i5 c1 Q Empty Weight :
3 N' j! u+ \3 W" p; C6 Y Gross Weight : $ @! _4 P" T& P# B2 q! r
Payload ( w / full fuel ) :
, `7 y r' J- k6 e5 y
: [3 x- a$ _# r3 @. s9 E, c Rotax 582UL DCDI Engine :
2 | a2 `3 k4 J( @3 l5 ? Engine Weight :
d* A M" d$ j6 B$ D4 G5 V GearBox out : ; o# D, ^! V" n/ {# g" K" c {& f
Fuel Capacity : 8 C" V8 G0 g, ~+ m
7 B, {9 G- C+ ]; _' c7 f( G
Performance :
' G4 c% c/ v, \) R6 d Range :
$ X ]2 r2 y9 d) W, o! w Vmax : # p( S2 a( P# k& r6 [% M) L
Cruise speed : . ?6 G3 z& P7 q* c5 u% G
Climb rate (msl) : # V! ~ x* Q; Z1 U* M
Service Ceiling : 5 \. ]+ S% h7 F7 p) K3 n9 C
Hover in ground effect: 6 V7 e8 D0 N( U0 e
Hover out of ground effect: / A; X9 Y" P$ Z4 _- \
Max. Endurance
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7 a3 t1 t/ C4 B! ?, j: r: ?% k/ U2 s Design Load Factor : : W/ Z. |+ R. |/ G' p
4 [' u9 X- ~6 J" ]" g
Seats : $ W0 ~5 S; {: v' z7 m! S b
Price: 18’500.00$ & M' h( N4 t- Y. }+ m j2 U
/ X/ d# `$ o5 C' o& G4 j Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) 7 Q- k/ m% q5 Q; i; X8 F
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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