2 ~. a$ y& h% l4 D0 QFURIA 自制式直升機
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2 {% b+ S' o2 l: h; sFURIA ULTRALIGHT HELICOPTER Plans 4 K/ f1 Y! |, d" k; u6 h8 T9 r
FuriaHelicopter Specifications
; B) Z4 \" j( R. c Main Rotor Diameter : . {% w5 G2 C9 A. {1 s" x- V) R: G
Main Rotor Blade Chord
7 g9 `. v0 V. I2 s/ E* M Main Rotor Speeds:
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Tail Rotor Diameter : ) h: c+ N6 ~+ C5 z0 U
Tail Rotor Chord :
& b3 L3 @) C3 R( c2 P! Y4 W Tail Rotor Speeds: 3 E3 y2 j8 k6 K% p. q
' N% _+ j" L+ P' Z. t" [ Length : ! k. g4 H4 {" [4 i7 S
Height :
4 V5 z- o' {: r Width :
4 h' N( R" F# s+ i Empty Weight : : T/ q! E5 M( T+ I
Gross Weight : ' z3 }# g- N& `! V& c
Payload ( w / full fuel ) : 6 Q$ ]1 S% @" U& O1 M0 j# [ A: k
3 E" t1 c! L3 n ?* [1 e# i Rotax 582UL DCDI Engine :
8 F; i# v) u, q/ o8 L! g3 d9 G Engine Weight :
( r# t( ?( l7 f' g4 Y. y4 j5 [) w GearBox out : 2 _& q; B. G# Z" I$ _! B) d
Fuel Capacity : ' Y% `# H5 E4 [/ d; R6 k
7 l* ?! F r5 V4 J V3 h9 n Performance : # \5 i3 p7 `( O1 G! Y
Range :
$ t1 n5 f3 f: O% z& K6 O+ { Vmax :
3 ^' z& X9 m6 L9 g* \ Cruise speed : 2 O c3 y! w8 l) w0 Z$ B, |" B
Climb rate (msl) : 6 A4 J K/ z+ v& F. V" c. p) R
Service Ceiling :
5 X( f7 E3 x9 k; C) [, u9 R Hover in ground effect:
$ _2 ~+ h+ S0 C Hover out of ground effect:
) a, B2 J Z2 F0 ]4 | G4 E/ y6 u Max. Endurance , @* n2 g; O8 b
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Design Load Factor : 9 H2 Q- ~# L0 {
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Seats : 6 w7 c7 R3 y1 h& }& ~
Price: 18’500.00$ + M }3 G% H+ ?3 [, _$ }+ W& ^( u( J
1 D: X1 X9 S% c: r3 M- B Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations)
% }# G' _9 J) D; Z* O! D 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. 8 }# C. C- V& X2 I6 V
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