Hydraulics Basic Systems Flashcards

1
Q
  • power source (creates hyd fluid flow)
  • a method of transmitting the power (lines/pipes)
  • a component to use the power (actuator/cylinder)
A

Hydraulic Systems Requirements

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2
Q

Type of hydraulic SYSTEM that there is continuous flow of fluid like hydro-electric power plant

Not practical for aircraft application

A

Open System

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3
Q

Type of hydraulic system that hydraulic fluid is enclosed within the system and moves through rigid lines & flexible hoses

Used for aircraft & fluid is re-circulated and reused

A

Closed System

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4
Q
  1. STORE hydraulic fluid

2. ALLOWS thermal expansion and contraction

A

2 primary functions of RESERVOIR

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5
Q
  • valve that selects the direction of hydraulic fluid flow

- has 2 positions, directs fluid flow to actuator or directs fluid flow from actuator to the reservoir (return flow)

A

Selector valve

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6
Q

cylinder that ALLOWS 2-way hydraulic operation, pressure can move cylinder in both directions, UP OR DOWN

A

Double-Acting Cylinder

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7
Q

Selector Valve that SELECTS 2-way hydraulic path by alternating pressure & return paths), enabling cylinder to move 2 directions

A

4-port Selector Valve

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8
Q

It replaces the hand pump

A

EDP - Engine Driven Pump

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9
Q

Valve that OFF-LOADS/UNLOAD the pump pressure when system is not being used (nohydraulic demand) byrouting pump output flowback to reservoir (return flow)

A

Pump Control Valve

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10
Q

valve that REPLACES pump control valve and AUTOMATICALLY controls & amp; routes hydraulic fluid flow back to reservoir reducing pilot load and engine load to drive the EDP

A

Unloading Valve

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11
Q

Pump that Allows brake pressure to be built up before engine start can be used as back-up for EDP

A

Hand Pump

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12
Q

Primary fluid supply line EDP

fluid inlet is approx. ½ height of reservoir, this prevents the loss of all hydraulic fluid contents if leak develops at EDP

A

Stand-pipe

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13
Q

It keeps fluid system clean

A

return filter

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14
Q

relieve line pressure trapped in system by selector valves in closed (neutral) position. Fluid expands when heated!)

A

Thermal relieve Valve

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15
Q

for system monitoring system fluid pressure

A

System pressure Gauge

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16
Q

Hydraulic System used on lighter simpler aircraft

Selector Valves are always in series

A

Open-Center System

17
Q

Hydraulic system used on larger aircraft

Selector valves are connected parallel

A

Closed-Center System

18
Q

(Self Contained) system used for small simple systems

Single unit that contains many hydraulic components and functions

Common on light twin-engine aircraft

A

Hydraulic Power Pack System