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FURIA 自制式直升機
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5 s# Y3 x8 f8 m! l# ZFURIA ULTRALIGHT HELICOPTER Plans
; {. C6 T. j: K( r0 TFuriaHelicopter Specifications
0 s& _! r1 R; H0 q Main Rotor Diameter : " Y X# J" G3 I& Z% p3 N. P
Main Rotor Blade Chord
$ C+ n# O# l f0 a9 K, ? Main Rotor Speeds: 7 S- [4 Q4 T4 g, l1 t
) E# ]5 {# A8 |! p) ] Tail Rotor Diameter :
7 H" ^9 J4 l, C% {2 Z4 C( Y Tail Rotor Chord :
2 q; k1 q. e0 O* n Tail Rotor Speeds: / J. V4 C3 ^! d9 q
% k$ r/ a/ b# J9 N0 l; H# c/ j; [ Length : 5 h6 k! I0 Z% Y- Z G: V( F
Height : # y% r- z$ u: b5 L8 ^. D
Width :
1 F. ~4 h+ b }* a7 k Empty Weight :
! R) p5 Q" m b# X7 P* B Gross Weight :
( z% m+ L) [, n5 D/ e Payload ( w / full fuel ) : * C* }5 D" Z/ R3 b
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Rotax 582UL DCDI Engine : 7 {" V. }) S$ W7 u
Engine Weight :
2 ]5 ~2 {* Y, f6 z GearBox out : 4 P8 H! t. n, M3 M) ]' j
Fuel Capacity : 4 b% \4 K: s, i9 P( S6 ~
/ F9 Y1 H" P4 a Performance :
+ B2 o4 ?2 K; r5 [2 q, R$ A7 E Range :
* f- H, d- ^% N! v Vmax : + _% { _' l4 a" s, O. b
Cruise speed : # a$ m: N( m# V/ Q% {
Climb rate (msl) : ! z9 u/ K5 a! ?0 ?
Service Ceiling :
) Y% b+ w' ]0 T" ]. n1 S Hover in ground effect:
7 w3 t( Z, w3 p7 M% e1 a9 L Hover out of ground effect:
$ u! C5 \: B! K/ a Max. Endurance
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) } U( T. V5 O2 Q- K Design Load Factor :
|# S/ U. k" |
( n; f3 N' o. N5 M/ m Seats :
, D& k3 y3 T3 o l& n Price: 18’500.00$
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Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations) ' [3 l) I( i3 ]0 v
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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