Ninguna marca
Referencia: 92/91
Brida rodamientos autolubricantes 6 x 10 x 3 mm
Política de seguridad
Política de envío
Política de devolución
No hay reseñas de clientes en este momento.
Reference: 117/20
The standard version of our mechanics includes ground thrust bearing shafts with a of 8 mm Ø and a length of 110 mm.Thrust bearings absorb the high centrifugal forces exerted by the main rotor blades. The effect of the axial bearings is retained in full when the blade holders rotate.Thrust bearing set, complete as shown.
Reference: 79/10
The length of the flybar itself also plays an important role in the model's flight characteristics: the longer the flybar, the smoother the hover. A longer flybar increases the control deflections. 450 mm length is considered normal, while 510 mm provides more docile handling.
Reference: 72/18
Aluminium centre piece, rigid, for 10 mm main shaft
Reference: 707/2
Rotor head cover for 4-blade head incl. screw.Laminated of carbonapprox. 120 mm ∅, 25 mm high
Reference: 80/20
Control bridge 2-part metal, for 4 mm Ø flybar.
Reference: 72/42
This rotor head hub with its bonded-in carbon fibre plates is a real head-turner. The plates are simply glued into the existing recesses on both sides. We recommend silicone rubber, Ord.No. 10/11, as adhesive.CFRP plates for aluminium hub matching Ord.No. 832/72pack quantity: 2 plates
Reference: 71/20
Pitch compensator, complete, for 10 mm ∅ main shaft, centre piece GRP
Reference: 722/71
Pitch compensator, complete, for 12 mm Ø main shaft, centre piece aluminium.For use with the rotor head Ord.No. 722/72.
Reference: 76/9
Blade holder arm, aluminium. Content of the package: 1 piece.
Reference: 78/40
Mixer levers are an essential part of every flybar-controlled rotor head. From the swashplate a pushrod runs to the ballraced mixer arm which is screwed to the blade holder arm. The mixer levers transmit the control movement to the flybar via the double ball-link.Additionial accessories for the use of mixer levers are either two flanged ballraces or two...
