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CHAPTER 1 INTRODUCTION
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TM-1-1500-204-23-2 General Aircraft Maintenance (Pneudraulics Maintenance and Practices) Volume 2 Manual
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Mechanical Advantage.

TM 1-1500-204-23-2 CHAPTER 2 PNEUDRAULICS GENERAL 2-1. Pneudraulics  Theory  and  Basic  Principles.    The  aircraft  hydraulic  system  transmits  engine  power  to  distant points on the aircraft.  This force is carried by hydraulic fluid confined In a system of tubing and hoses a. Qualities of Hydraulic Fluid.  Hydraulic fluid can be described In terms of three physical qualities (1) Incompressibility.      For  practical  purposes,  liquids  are  incompressible  This  means  that  even  under extremely high pressure a liquid cannot be made much smaller. (2) Expansion and contraction.  Liquids expand and contract with changes in temperature.  When a liquid in a closed container is heated, the liquid expands and puts pressure on the walls of the container.  As the liquid cools, the pressure decreases. (3) Pressure  transmission.      Pressure  applied  to  a  confined  liquid  is  transmitted  equally.    If  an  opening exists in a system, such as an actuator, the fluid will act on it, causing it to move. b. Computation  of  Force,  Area,  and  Pressure.    Hydraulic  systems  are  designed  to  take  advantage  of  the characteristics of liquids as they relate to force, area and pressure.  These terms as used in hydraulics are defined as follows: (1)  Force.   Force is the amount of push or pull applied to an object.  The force applied to a piston head, for example, is the energy applied to the total area of the piston head.  In this manual, we measure force in pounds. (2) Area.   Area is the measurement of a surface In the aircraft hydraulic system, we are concerned with the  areas  of  piston  heads  If  we  know  this  area,  we  can  compute  the  amount  of  force  needed  to  start  a  mechanism moving In this manual, area Is measured in square inches. (3) Pressure.    Pressure  is  the  force  applied  to  one  unit  of  area-usually  1  square  inch.    The  pressure  on  a piston head develops the force that operates a mechanism.  In our work, we measure pressure in pounds per square inch (psi). (4) Computation.  If  you  know  any  two  of  these  factors,  you  can  easily  compute  the  third  by  using  the equation illustrated In figure 2-1.  To apply this equation, multiply the two lower factors together to get the top factor, and divide the top factor by the known lower factor to get the unknown lower factor. Figure  2-1.  Computing Force Pressure, and Area 2-1

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