Thin-wing ailerons / flap control
AXR 7462-W MG-D combines a Iron-core motor with 7075 aluminium gears. It operates at 4.8–8.4 V and weighs 13 ±0.5 g. At 8.4 V, the listed stall torque is 4.9 kg·cm and no-load speed is 0.078 s/60°. Use the dimensions and rated-load data below to assess fit.
Wing installations need clearance for the arm, linkage and cable as well as the servo body. Aileron and flap loads change with flight conditions. Size the linkage for the maximum design load and validate mounting stiffness and centring in the assembled system.
Stall torque is not a continuous load rating. Consider rated torque and duty cycle when sizing the mechanism. The operating range specifies allowable supply voltage; it does not imply that test data exist at every voltage.
| Comparison voltage V | Stall torque kg·cm | No-load speed s/60° | Running current A | Stall current A |
|---|---|---|---|---|
| 5 | 3.8 | 0.112 | 0.042 | 1 |
| 6 | 4 | 0.096 | 0.048 | 1.15 |
| 7.4 | 4.5 | 0.083 | 0.051 | 1.4 |
| 8.4 | 4.9 | 0.078 | 0.06 | 1.6 |
The source lists a 1520 µs reference pulse and a 1500 µs position centre. Confirm the neutral setting and usable travel for the controller and delivered version.
Drawing and tabulated dimensions may use different datums. Confirm the final mounting drawing and interface version before machining mating parts.
Check the supply, pulse width, mounting pattern and arm connection first. Commission with the load removed or limited, verify centre position, direction and mechanical travel, then validate the working load gradually. Allow for transient current and prevent voltage drop, reversed connections and sustained contact with mechanical stops.
Select up to 4 models. Torque and speed use the comparison voltage selected above.
Select models to compare specifications and request a combined quote.
Thin-wing ailerons / flap control
Comparison voltage: 8.4 V
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Thin-wing ailerons / flap control
Comparison voltage: 8.4 V
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