The maximum torque occurs at somewhat lower speed than the full-load working speed of the motor, probably about 50% more than the torque at full power.
Assuming that the motor is a 2-pole one that runs at 90-95% of the synchronous speed, 3000 rpm on 50 Hz or 3600 rpm on 60 Hz, the amount of torque is proportional to the power of the motor.
In SI units the mechanical power equals the torque times the angular velocity, so watts = torque in Newton-metres times speed in radians per second (2.pi radians is one revolution).
So the main factor that determines maximum torque is the rated power of the motor. Double the power, double the torque for a motor running on a constant-frequency power system.
The amount of torque required by a tail rotor depends on factors such as the size and weight of the helicopter, the speed at which it's flying, and external forces like wind. Generally, tail rotors are designed to provide enough torque to counteract the torque produced by the main rotor and maintain stable flight.
The turning effect of forces, also known as torque, depends on the magnitude of the force applied and the distance between the force and the axis of rotation (lever arm). These factors determine how effectively a force can cause an object to rotate around a pivot point.
The magnitude of the torque depends on the force applied to the beam and the distance from the point where the beam is bolted. The torque can be calculated using the formula Torque = Force x Distance.
No, torque is a vector quantity that does not depend on the choice of origin. Torque is defined by the force applied to an object and the distance from the point of rotation, regardless of where the origin is located.
Torque is a measure of the force that can cause an object to rotate around an axis. The angle through which the object rotates is proportional to the torque applied. As torque increases, the rotational angle also increases, assuming all other factors remain constant.
The amount of torque required by a tail rotor depends on factors such as the size and weight of the helicopter, the speed at which it's flying, and external forces like wind. Generally, tail rotors are designed to provide enough torque to counteract the torque produced by the main rotor and maintain stable flight.
It is not really answerable, depends on many factors. Bolt size thread pitch of the bolt material the bolt is made of that material the bolt is screwed into lubricated/unlubricated and what with what it was initially torqued to If you have Snap on tech100/250 torque wrench it will give you a final torque #, I have seen torque readings double the intial torque # after the 90 degrees.
The turning effect of forces, also known as torque, depends on the magnitude of the force applied and the distance between the force and the axis of rotation (lever arm). These factors determine how effectively a force can cause an object to rotate around a pivot point.
torque
Depends on other factors such as compression, head port, etc. My 06 Fatboy put out 105 torque, 103 horsepower. Could have gotten more with bigger injectors, but I was fine with results.
Depends WHICH engine, all 2.4's don't have same torque.
Not necessarily. While torque directly affects acceleration, other factors such as weight, aerodynamics, and gearing also play a role in determining a vehicle's speed. Ultimately, a balance of torque, power, and other factors is needed to achieve faster speeds.
This depends on what engine you are working on.
Depends on the engine.
That depends on what engine it has.
The magnitude of the torque depends on the force applied to the beam and the distance from the point where the beam is bolted. The torque can be calculated using the formula Torque = Force x Distance.
it all depends on the mechanics of the car....horsepower, torque, and weight of the vehicle along with several other statistics are all factors in this equation