, k- Q3 l8 k# t& a! ^- x; ~) Q4 L# A
FURIA 自制式直升机 `9 {' Y& J' {% o4 r5 Y8 |
: z+ F7 L* {: n
0 E) ~1 j# E' p0 E% q/ S8 WFURIA ULTRALIGHT HELICOPTER Plans / }6 m' n+ b0 R" x
FuriaHelicopter Specifications ( n. R. v. ^9 O$ C
Main Rotor Diameter :
5 P/ }. g! K9 S6 n- E4 h- L Main Rotor Blade Chord
- N/ d( E6 I! i2 S1 w/ k Main Rotor Speeds:
/ f5 l1 T0 Y- O/ F8 g( V; ^. }- E
$ m$ d* Z @+ Z7 y7 \( y Tail Rotor Diameter :
" n* a! I$ h5 ]; Q3 i. Q) N Tail Rotor Chord : # C- J: `6 b( s% B. S/ p9 G
Tail Rotor Speeds:
H8 C) x+ E$ K3 W% h
& B3 W T. v8 S$ _# x' D7 K Length :
5 Y- ^& A4 h8 T' W$ z1 _& { Height : . [, i" s* k. T4 x
Width :
3 b! E: {4 J, x2 u) X2 L% g Empty Weight : 8 a$ l! Z4 Q; b8 l
Gross Weight : - h& U; K* l: Y
Payload ( w / full fuel ) :
2 h( G% E' d ^ , H9 A+ o& ~! c/ `0 |: B0 ]
Rotax 582UL DCDI Engine : Y! L6 s! f. z8 b5 W
Engine Weight :
/ F S5 R6 X# N* y GearBox out :
" S& g3 b0 `# J: E/ t$ M% D( m } Fuel Capacity :
# l5 H. b3 K+ x7 ]" P5 B
+ r4 a; {5 H0 k9 E0 ]/ ? Performance : & K2 l( u) E/ X7 J* B
Range :
7 Y% d+ ~0 Z- D0 x. L/ d! p Vmax : 9 A: Z! X+ d; o X" M' y- ]" a
Cruise speed :
" q9 H. F& G: \ Climb rate (msl) :
8 _7 `8 S: y/ f) T `# _# m5 h Service Ceiling : ( I$ k! n+ ~( w1 w i/ w' ~
Hover in ground effect:
/ }( F" s% a3 s! X6 R% M1 _9 i# K Hover out of ground effect:
' N, n" P: ~3 [3 ~ Max. Endurance
% F! y: J- _) }; L : l' x- @' ^1 r5 W
Design Load Factor :
* ?) s" o6 n9 {" j& o- O! ~0 J* g , q6 P2 Y% z; m0 A
Seats : , p5 C6 k3 K$ @- L) O
Price: 18’500.00$
+ D6 G* h8 y3 w5 z) ~% x; ]) G/ O
: [ \+ H. |# y# D. N# k( J Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations)
, \4 ^9 A: f8 W6 u1 L+ O# Z 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.
/ j8 ^7 @( Q1 {4 @5 m / F2 A% S: m% X! ?% |5 Z
$ ^4 u3 K4 ?& p g+ C" Z) c9 S( _ |