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CHAPTER 2 PNEUDRAULICS GENERAL
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TM-1-1500-204-23-2 General Aircraft Maintenance (Pneudraulics Maintenance and Practices) Volume 2 Manual
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Figure  2-3.  Pascal's Law

TM 1-1500-204-23-2 (a) Force computation.   The force (F) in pounds can be obtained by multiplying the known values of area (A) and pressure (P). (b) Pressure computation.  Similiary, if the force (F) and area (A) are known, F can be divided by A to obtain pressure (P) In pounds per square inch. (c) Area computation.  Finally, to obtain area In square inches, force (F) is divided by pressure (P) c. Computation of Volume, Area, and Length of Stroke.  You can use the same type of triangular equation to compute volume, area, and length of stroke.  The following definitions apply for this manual. (1) Volume.  Volume is a measurement of quantity expressed in cubic inches, for example, the amount of liquid in a cylinder or the amount of liquid displaced by a pump or an actuating cylinder. (2) Area.   As in the previous equation, area is a surface measurement expressed in square inches. (3) Length  of  stroke.      Length  of  stroke  is  a  measurement  of  distance  expressed  in  inches.    The  stroke length with which you will be concerned in this manual is the distance a piston moves in a cylinder. (4) Computation.   If you know any two of these factors, you can compute the third (see figure 2-2).  As in the  previous  equation,  multiply  the  two  lower  factors  together  to  obtain  the  top  factor  and  divide  the  top  factor  by  the known lower factor to obtain the unknown lower factor.  For example, a piston having an area of 8 square inches moves a distance of 10 inches within a cylinder.  To find the volume of liquid moved, multiply the two lower factors together-8 square inches (A) times 10 inches (L)- to obtain V: 80 cubic inches d. Pascal's Law .  Practical applications of hydraulic principles are based on Pascal's law, which may be stated in  simple  terms  as  follows:    when  a  force  is  applied  to  a  confined  fluid,  the  pressure  is  transmitted  equally  in  all directions.  Pascal's law applies for confined fluids only.  It follows then that the law does not apply for fluids in motion since moving fluid is not confined in the true sense of the word.  Figure 2-3 shows graphic illustration of how Pascal's law applies in an aircraft hydraulic system.  Note that when a force is applied to the piston in cylinder 1, it is transmitted to all portions of the confined fluid.  If, for example, the applied force is 5 psi, the pressure In cylinders 1, 2, and 3 and in the tubing will be 5 psi.  But suppose a change takes place in which a lack of resistance causes either piston 2 or 3, or both, to  move  upward.  This  momentarily  lowers  the  pressure  in  cylinders  2  and  3  while  in  cylinder  1  it  is  still  5  psi.    This unbalanced condition cannot last.  Fluid will flow from cylinder 1 to cylinders 2 and 3.  This is because pistons 2 and 3 are not confining the fluid as long as they move upward.  Pascal's law does not apply to this condition.  When pistons 2 and 3 reach the end of their strokes, the fluid stops flowing.  At this point the fluid is again confined and the pressure again equalizes-Pascal's law applies once more. e. Mechanical Advantage.  In simple terms, mechanical advantage is defined as the use of a small force over a great distance to obtain a great force over a short distance. In other words, it is the amount by which the input effort is multiplied in the output of a device.  Using a claw hammer to remove a nail from a two-by-four piece of lumber or using a jack to raise a vehicle are examples of mechanical advantage.  The aircraft hydraulic system Is designed to make full use  of  this  principle  since  it  is  a  system  for  transmitting  engine  power  to  distant  points  in  the  aircraft  where  power  is needed.    This  is  accomplished  by  multiplying  the  input  effort  (or  force)  enough  to  do  the  required  job-in  other  words, gaining a mechanical advantage. Figure  2-2.  Computing Volume, Length, and Area 2-2

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