Gravity always acts downward on every object on earth. Gravity multiplied by the object's mass produces a force called weight. Although the force of an object's weight acts downward on every particle of the object, it is usually considered to act as a single force through its balance point, or center of gravity. If the object has its weight distributed equally throughout, its balance point is located at its geometric center. If the object has unequal weight distribution, its balance point or its center of gravity may not be at its geometric center. It is possible for the center of gravity to entirely outside the boundaries of the object, as does a boomerang.
The force that opposes the force of weight for an aircraft is lift. The lift force must be greater than the weight for an airplane to fly
For aircraft, it is important that the location of the center of gravity fall within the limits specified by the design of the aircraft. If it falls outside these limits, it will have adverse effects on how the airplane will fly.
A moment or a torque is caused by a force acting on a body some
distance from the center of gravity. Its formula is:
where the force is always acting perpendicular to the moment arm. In the diagram below, item A is at a distance X from the fulcrum or pivot point, while item B is at distance Y from the fulcrum. If the system shown is balanced, then the product of A and X must equal the product of B and Y
The product of the weight of item A and its distance from the pivot point (X) produces a counterclockwise torque and the product of the weight of item B and its moment arm Y produces a clockwise torque. When the clockwise torques equal the counter clockwise torques, the airplane or object is balanced along that plane. in an airplane, any moment in front of the center of gravity is considered a negative value, having a negative moment arm, while and torque behind the center of gravity is considered to be a positive value with a positive moment arm.
Finding the balance point: Given the following setup below, where the length of the beam is 80 inches long but weightless. if we wish to find the balance point of this system, or where to locate the fulcrum, we first must set up an arbitrary zero reference point. This can be located anywhere on the line of the beam. For this example, we will choose the zero reference point to be at A.
By constructing a simple chart of weight, moment arms and moments as
shown above, and placing the values in each space. Item A has
a weight of 45 pounds. Since the zero reference point was selected at
A, its arm length is 0. Zero times 45 is 0, so A's
torque or moment is zero. B weighs 75 pounds and its arm
length is 80 inches. Since 80 times 75 equals 6000 inches-pounds,
B has a torque of 6000 inches-pounds. The total weight is 120
pounds and the total moment 6000 inches-pounds, the balance point is
found by dividing the total moment by the total weight. This value is
50 inches located to the right of point A or since 80 - 50 =
30, it is also 30 inches to the left of B.
Checking these values, letting the moment arm of A be negative, then
B's torque = force x distance = 75 pounds x 30 inches = 2250 inches -pounds
Since the counterclockwise torque (-2250) and the clockwise torque (2250) sum to zero, the beam will balance at the point located 50 inches to the right of point A.
Problem:
Extension:
An aircraft that has additional equipment installed on the plane or
replacements made by technicians needs to have the information about
its center of gravity updated.
Table for question 1
Find the following information: the new empty weight
is____________,
and the new location of the CG is__________.
(Answer)