Hyquip Data Book
Mass / Force
1 lbf 4.448N
1 kg 2.205lb
1 kg 9.81N
1 ton 1.016x103kg
1 N 0.2248 lbf
Energy
1 kWh 3.6x106J
1 kcal 4.187x103J
1 Btu 1.055x103J
Power
1 hp 745.7W
1 kW 3412Btu/h
1 W 1J/s
Torque
1 lbft 1.356Nm
Speed
1 ft/s 0.3048m/s
Length
1 ft 0.3048m
1 µm 1x10-6m
1 in 25.4x10-3m
Pressure
1 Pa 1N/m2
1 bar 105N/m2
1 psi 68.95x10-3bar
1 bar 14.5psi
Density
1 lb/ft3 16.02kg/m3
Area
1 in2 0.6452x10-3m2
Volume
1 in3 16.39cc
1 in3 16.39x10-6m3
1 gallon UK 4.546x10-3m3
1 gallon US 3.785x10-3m3
1 L 10-3m3(dm3)
1 ft3 0.0283m3
1 m3 220gallon UK
1 barrel 205L
Flowrate
1 L/min 0.22gall/min
1 L/min 1.66x10-5m3/s
1 ft3/min 28.32x10-3m3/min
Viscosity
1 cSt 10-6m2/s
Key
lbf - Pounds Force µm - Micrometre
N - Newton Pa - Pascal
kWh - Kilowatt Hour L - Litre
kcal - Kilo Calorie m - Metre
Btu - British Thermal Unit cSt - Centistoke
W - Watt hp - Horse Power
J - Joule cc - cm3(mL)



HYDRAULIC

a) PUMPS & MOTORS
FLOW RATE (L/min) Q = D.n
1000
SHAFT TORQUE (Nm) M = D.p
20
SHAFT POWER (kW) P = M.n
9554
HYDRAULIC POWER (kW) P = Q.p
600
p = Pressure (bar)
D = Displacement (cm3/rev)
n = rev per min
CYLINDERS
Area, piston A1 =
Area, piston rod A2 =
Area, piston annulus A3 =
Force, push F1 =
Force, regenerative F2 =
Force, pull F3 =
Stroke, speed s =
s =
Required flow Qth =
Qth =
Q =
Stroke volume V =
Stroke time t =
A1 = piston area (cm2)
A2 = piston rod area (cm2)
A3 = piston annulus area (cm2)
d1 = piston diameter (mm)
d2 = piston rod diameter (mm)
F1 = push force (kN)
F2 = regenerative force (kN)
F3 = pull force (kN)
not including frictional losses
p = operating pressure (bar)
s = stroke speed (m/s)
h = stroke (mm)
t = stroke time (sec)
V = stroke volume (litre)
Q = flow (l/min)
taking leakage losses into consideration
Qth = flow (l/min)
excluding leakage losses
nvol = volumetric efficiency
taking leakage losses into consideration



b) CYLINDERS - Conversion Factors
Multiply By To obtain
Area
in2 6.4516 cm2
ft2 929.0304 cm2
yard2 8361.274 cm2
Flow
US Gal/min 3.785412 l/min
UK gal/min 4.546 l/min
ft3 28.31685 l/min
Force
lb f 0.00444822 kN
kg f 0.00980665 kN
ton f 9.9640 kN
Length
inch 25.4 mm
ft 304.8 mm
yard 914.4 mm
Multiply By To obtain
Pressure
N/m2(Pa) 0.00001 bar
kN/m2(kPa) 0.001 bar
lbf/in2 0.06894757 bar
N/cm2 0.980665 bar
Velocity
ft/min 0.0050 m/s
ft/sec 0.3048 m/s
Volume
cm3 0.001 litre
in3 0.0163866 litre
US gal 3.785412 litre
UK gal 4.546092 litre
ft3 28.3161 litre
m3 1000.0 litre
c) FLOW
FLOW (L/min) ie, if you double the flow you get 4 times the pressure change
p = Pressure change (bar)
PRESSURE DROP IN PIPE (N/m2) =
FLUID VELOCITY (m/s) See section Hydraulic Pipes and Hoses.
f = Friction factor
l = Length (m)
v = Velocity (m/s)
d = (m)
p = Density (kg/m3)

Pneumatic

a) FLOW THROUGH PIPES:
p = where
b) VELOCITY THROUGH PIPES:
v = 1273Q
(p+1)d2
where
If the free air flow is known, the minimum inside diameter to keep velocity below 6 m/s, can be found from:
d in mm =
For normal installations, where the pressure is about 7 bar gauge, this can be simplified to:
d in mm should be greater than
p = Pressure drop (bar) v = Flow velocity in metres/s
Q = Free air flow (m3/s)=L/s x 10-3 p = Initial pressure (bar)
1 = Pipe length (metres) d = Inside pipe diameter (mm)
Output force and maximum rod lengths
Example: Knowing the output force required (200kN) and the pressure of the system (160 bar), connect Output force through pressure to cut cylinder diameter. Answer: 125 millimetres
To find the maximum length of a piston rod. Connect output force required (200kN) through rod diameter (70mm) to cut the maximum rod length scale; this gives you the (Lm) dimension. Answer: 2800mm.
To find the actual length stroke (LA) for a specific mounting use formulae below.
Maximum stroke lengths for specific mounting cases
Foot mounted, eye rod end LA = Lm x 0.8
Foot mounted, rigidly supported rod LA = Lm
Front flange, eye rod end LA = Lm x 0.8
Front flange, rigidly supported rod LA = Lm
Rear flange, eye rod end LA = Lm x 0.4
Rear flange, rigidly supported rod LA = Lm x 0.8
Rear eye, eye rod end LA = Lm x 0.3
Trunnion head end, eye rod end LA = Lm x 0.3
Trunnion gland end, eye rod end LA = Lm x 0.6
Trunnion gland end, rigidly supported end LA = Lm x 0.8
For intermediate trunnion positions scaled multiplier factors must be taken. Clevis and spherical eye mountings have the same factor as eye mountings.
Example: Having found Lm (2800mm) for rear flange mount with eye rod end
LA = Lm x 0.4 = 2800 x 0.4 = 1120mm.
Click image to enlarge



Click image to enlarge
Nomogram for determining pipe sizes in relation to flow rates and recommended velocity ranges.
Based on the formula:

Velocity of fluid in pipe (m/s) = Flowrate(L/min) x 21.22
d2
where d = Bore of pipe (mm)
Recommended velocity ranges based on oils having a maximum viscosity grade of 70cSt at 40°C and operating between 18°C and 70°C.



Storage Applications Formula to estimate accumulator volume for storage applications.
Slow charge

Slow discharge
Fast charge

Fast discharge
Slow charge

Fast discharge
The precharge pressure is chosen to 90% of the min. working pressure. n varies between 1 and 1.4 depending on whether the course is slow (isothermal) or fast (adiabatic).
Pump Pulsation Formula to size accumulator to reduce pump pulsations.

a) Minimum effective volume (litres) V1 = k. Q
n
Note: It is good engineering practice to select an accumulator with port connection equal to the pump port connection.
b) To check the level of pulsation obtained.
Volume of fluid entering accumulator = D.C

For pulsation damping precharge pressure P1 = 0.7 . P2
and assuming change from P1 to P2 is isothermal, then V2 = 0.7 . V1
Hence: Percentage pulsation above and below mean is
V1 = effective gas volume
V2 = min. gas volume
V3 = max. gas volume
P1 = precharge pressure
P2 = min. working pressure
P3 = max. working pressure
Va = V3-V2 = working volume (fluid)
k = a constant *
Q = Pump flow (L/min)
n = Pump speed (rpm) if n>100 use 100
D = Pump displacement (L/rev)
C = a constant *
* Dependent upon no. of piston. For multi piston pumps >3 pistons. k=0.45 and C=0.013.



COOLING
The tank cools the oil through radiation and convection.
P= T . A . k so T = P . 1000
1000 A.k
k = 12 W/m2,°C at normally ventilated space
      24 at forced ventilation
       6 at poor air circulation

Required volume of water flow through the cooler:
Q = 860 x Power loss
               T water   
HEAT EQUIVALENT OF HYDRAULIC POWER
in kj/sec = Flow (L/min) x Pressure (bar)
                      600
HEATING
Heating is most necessary if the environmental temperature is essentially below 0°C.

Requisite heating effect:
P= V . T kW
35 . t
ENERGY
(J) = M.C.T
M = Mass (kg)
C = SHC J/kg°C
T = temp change (°C)
t = time (mins)
Note
1MJ = 0.2777 kW/Hr

CHANGE OF VOLUME AT VARIATION OF TEMPERATURE
Change of volume V = 6.3 x 10-4.V. T

CHANGE OF PRESSURE AT VARIATION OF TEMPERATURE
Note: With an infinite stiff cylinder.
Change of pressure p = 11.8 . T (in general - affected by many variables)
Example: The temperature variation of the cylinder oil from night time (10°C) to day time/solar radiation (50°C) gives:
P = 11.8 x 40 = 472 bar
KEY
T = Temp change (°C)
P = Power (Kw)
k = heating coefficient (W/m2°C)
A = Area of tank excluding base (m2)
t = time change (mins)
p = change in pressure
C = Specific heat capacity (J/Kg°C)
V = Volume (L)



 

TERMINOLOGY
The main source of fluid power terms and definitions is the International Standard - ISO 5598 - Fluid Power Systems and Components - Vocabulary, 1985, however, new definitions are arising from recent work on E.E.C. - CEN standards.
The following are just a few of the fluid power terms in every day use for hydraulic and pneumatic applications:-
Fluid Power - The means whereby signals and energy can be transmitted, controlled and distributed, using a fluid as the medium.
Hydraulics - Science and technology which deals with the laws governing liquid flow and pressure.
Pneumatics - Science and technology which deals with the use of air or neutral or gases as the fluid power medium.
System - Arrangement of interconnected components which transmits and controls fluid power energy.
Machinery - An assembly of linked parts or components, at least one of which moves, with the appropriate actuators, control and power circuits etc., joined together for a specific application.
Component - An individual unit (e.g. actuator, valve, filter) comprising one or more parts, designed to be a functional part of a fluid power component or system.
Actuator - A device which converts energy into force and movement. The movement may be linear (e.g. cylinder), semi-rotary (e.g. torque unit), or rotary (e.g. motor).
Operating conditions - Operating conditions are indicated by the numerical values of the various factors relating to any given, specific application of a unit. These factors may vary during the course of operations.
Working Pressure - Pressure at which the apparatus is being operated in a given application.
System pressure - Nominal pressure usually measured at the inlet to the first valve or at pump outlet (normally the relief valve setting).
Pilot pressure - Pressure in a pilot line or circuit.
Hydraulic pumps - Units which transform mechanical energy into hydraulic energy.
Compressors - Devices which cause a gas to flow, against a pressure: they convert mechanical energy into pneumatic fluid power.
Directional control valve - Device connecting or isolating one or more flow paths.
Control mechanisms - The means whereby components change their state. Control mechanisms may be manual, mechanical, pressure or electrical in operation.
Pressure relief valve - Valve which limits maximum pressure by exhausting fluid when the required pressure is reached.