The Dynamic Amplification Factor (DAF) is calculated by comparing the maximum dynamic response of a structure to the static response under a given load. It is typically determined using the formula DAF = Maximum Dynamic Response / Static Response. This involves analyzing the system's behavior under dynamic loading conditions, often using methods such as time history analysis or frequency response analysis. Factors like the frequency of the load, the natural frequency of the structure, and damping characteristics are critical in this calculation.
K Factor Also called an Overhung Load Factor. A constant used to modify the overhung load rating of a gearbox based on the type of load applied on the shaft. Use the K factor either to increase the calculated overhung load, or to reduce the gearbox overhung load rating.
maximum demand load can be calculated as: # maximum demand=demand factor * Connected load or by # maximum demand = connected load * Diversity Factor Note: Demand factor and diversity factor are NOT same
A static load is the effect of gravity on an object or structure.A dynamic load is the forces that move or change when acting on a structure.Example of a dynamic load:Force of wind or the weight of a truckExample of a static load:Weight of a bridge
The design factor, also known as the factor of safety, is calculated by dividing the ultimate strength by the working load. In this case, the design factor is 10,000 pounds (design strength) divided by 2,000 pounds (working load), which equals 5. This means the system is designed to withstand five times the working load, providing a safety margin in case of unexpected loads or conditions.
Diesel Engine has high load factor
K Factor Also called an Overhung Load Factor. A constant used to modify the overhung load rating of a gearbox based on the type of load applied on the shaft. Use the K factor either to increase the calculated overhung load, or to reduce the gearbox overhung load rating.
maximum demand load can be calculated as: # maximum demand=demand factor * Connected load or by # maximum demand = connected load * Diversity Factor Note: Demand factor and diversity factor are NOT same
A static load is the effect of gravity on an object or structure.A dynamic load is the forces that move or change when acting on a structure.Example of a dynamic load:Force of wind or the weight of a truckExample of a static load:Weight of a bridge
The definiton of static load is to load something staticly. However, the definition of a dynamic load can be either that of a large load of something or to have something of great importance be placed onto someone in such a way that it is a "load".
The design factor, also known as the factor of safety, is calculated by dividing the ultimate strength by the working load. In this case, the design factor is 10,000 pounds (design strength) divided by 2,000 pounds (working load), which equals 5. This means the system is designed to withstand five times the working load, providing a safety margin in case of unexpected loads or conditions.
A static load varies slowly, a dynamic load changes with time pretty fast. In order for one to find the answer to this type of structural dynamic question, one might ask the help of a scientist.
a dynamic load is one that varies with time, sucha sproduced in road trandsportation. It could be amplified at resonance. An impact load is a dynamic load opf short duration, such as dropping a rock onto a surface, resulting in possible high acceleration depending on the stiffness.
The K-factor of a transformer is calculated using the formula (K = \frac{I_{rated}}{I_{load}}), where (I_{rated}) is the rated current of the transformer and (I_{load}) is the actual load current. It indicates the transformer's ability to handle overloads and varying load conditions. A K-factor greater than 1 suggests that the transformer can support nonlinear loads effectively, while a K-factor of 1 means it's suitable for linear loads. Additionally, the K-factor can also be influenced by the harmonic content of the load current.
Load Factor
Power factor doesn't necessarily 'improve with the load', but it is determined by the load.
the maximum load factor without structural damage to the aircraft. Load factor = 1 / (cos (angle of turn))
The dead load is the weight of the bridge itself. The live load is things like traffic, wind, rain, etc. The dynamic load are things like earthquakes, big gusts of wind, and other things.