DanivasaRamesh
General Manager-R&D, Wipro Fluid Power Limited, Bangalore
Abstract
Hydraulic Cylinders are the 'muscles' of Mobile and Industrial
Hydraulic machines. They handle enormous to tiny implements at ease with
tremendous velocities. These implements quickly reveres back and both
and forth. The gathered momentum and rate of change of momentum causes
huge impact on the end covers. This is detrimental to cylinders as well
as to equipment and operator comfort. So there is a need to "soften
the blow".
The locked up oil just before the end butting stroke is allowed through
a "carefully designed flow resistance path'. This produces the back
up pressure hence opposing braking. This force decelerates the motion
and result in a smooth butting. This is termed as "Cushioning in
Hydraulic Cylinders".
There are many problem associated with cushioning since the comfort of
cushioning is assessed by the fineness of feeling of operator. Hydraulic
and motion parameters relevant to cushioning are
- Smooth change of velocity
- have restriction leading to 'hydraulic shock'
- less restriction leading to mechanical shock
- hydraulic noise ( turbulence)
- Mechanical Noise ( butting / rubbing)etc
This paper describes a systematic approach to cushioning in
hydraulic cylinders.
- design aspects
- study of chamber pressure, cushion stroke & velocity
- pressure and stroke sensing in cushion zone
- noise aspects
- Cushioning hydraulic cylinders (small an big ) range from
connected load of tiny buckets to huge mass.
Hydraulic Cylinder Cushioning - The problem definition

In
the simplest of the schematics, the problem can be represented in the
following diagram.
P - Pressure ( due to load)
Q - Pump flow into cylinder
A - Port Cover (Cap)
B - Port on Head End Cover
af - Full area ( Piston)
ac - Annular Area (Piston area-rod area)
W - Connected Weight
WR - Weight of rod + piston
V - Velocity of load / rod ( initial)
X - Piston of rod
When the mass comes to a halt at the bottom of cylinder or head side,
an impact jolts the cylinder i.e., impact = m. v / D t - short duration
when the initial velocity terminates to zero.

Looking
at the x vs. t diagram, load moving with velocity is D x / D t and
becomes zero at end butting point. The problem is to reduce this
velocity D x / D t to some acceptable level so that end butting impact
is reduced. This is called as "cushioning in "hydraulic
cylinders" or sometimes referred as "softening the blow".
A small part of thestroke towards the end is used to create opposing
force in the back area of the piston and this stroke is called as "cushion
length / cushion stroke".
The time to reduced the velocity and butting is called "cushion
time".
The trapped area and cushion length called as "cushion chamber /
volume".
Applications
Invariably in mobile and industrial machines using hydraulic cylinders
to actuate the loads / masses it is inevitable that end butting of
piston will take place. Some examples are shown below.



The end butting shock explained earlier has effect not only on the
machine but also on the operator comfort.
The shock has to be absorbed and the load needs to be braked to reduce
to velocity and hence to reduce the impact.
Creation of the opposing force towards the end

in the normal working range of the rod the cushion length ls1 and ls2 do
not enter the covers thus the oil freely flows from service ports A&B
to chambers C1 & C2
When Ls1 enters ds1 or Ls2 enters ds2 then the oil between piston and
covers get locked up and will pass through clearance thus creating
throttling for the chamber oil. This throttling produces back pressure
hence opposing force (back pressure x area)
Kinetic Energy E = ½ mv
2
M - Moving mass
V - Velocity
Total Energy
E total = ½ mv
2 + mgl
s sin a 10 - 3
a = Actuator orientation
g = 9.81 m / sec
2
l
s = length in mm
m = mass in kg
v = m/sec
Substituting and equating the above and assuming that vp reduce 0.1 vi
the maximum pressure in the chamber at impact is given by :
Dpmax = AP2 K vi2 3x10-6/A02
A0 = Orifice Area
K = Orifice Constant
Inference:
Orifice diameter is easy to calculate but has highest pressure at
impact and does not provide restriction after the impact (velocity
drastically reduces ). This leads to hydraulic shock with damped
oscillation.
- Combination of annular and orifice generally provide a better effect.
Multiple Orifices

Where
enough cushion length LB available, than multiple orifice combinations
provide increased pressure drop cushion advances.
As plunger into the bore, the orifices cut out one by one thus
increasing the restriction for the reduced flow due to decreasing
pressure.
Stepped Sphere
Similar to multiple orifices stepped sphere produces annular
restrictions a1 a2 & a3 length L1, L2, & L3. Generally this
approach is adopted where sufficient cushion stroke and volume of oil
available so that spread out restrictions are possible.

Fine
tuning annular restriction:

While
the annular restriction in terms of annular clearance and the cushion
travel length, two / three notches on the plunger / bush produces a
variable restriction.
The notches control the area and reduce the velocity against time &
also produce hydrostatic balancing effect to float the plunger / bush

H = tan a x lB
W = 2 r Sin b / 2
H = w / 2 tan b/4
Area = Pr2b/360 - W (r - h)/2
= @ 2 / 3 w x h
Basic Energy Equation
1 Annular Restriction

Equating energies
E
total = W
mech + W
1
= W
F + W
2 + W
3
W
mech = F
mech x lb
W
mech = Mechanical Work Done
F
mech = Mechanical Force
L
b = Distance Traveled
W1 = ½ x F
1x1
b
( Pressure drops to zero during stroke of l
b)
The above applied force is equated by the following:
W
F +F
2.L
b+W
F+ W
2+W
3
1.18 m l
b 3 D
m3 /
(C
Rad)
3 t
t
W
F = Friction Force
F
2 = Opposing force due to back pressure
W
3 = Hydraulic work done
C
rad = Radial clearance
m = Viscosity
T
t = Cushion Time
F
1 = Drive Force
V
1 = Initial Velocity
D
m = Cushion Diameter
Equating above equations we get
C
rad = l
b.Dm
3 (1.18m / t
t
/ 0.5 mv
2) ½ + ( F
mech + 0.5 F
1-
F
2) Lb - W
F
In the above, the acceleration and compressibility of fluid not
considered.
The cushion power W
pl
W
pl = 1.18 ml
b3D
m3/
C
rad3t
t Cushion power is directly
proportional to viscosity cube of length & diameter and inversely
proportional to cube of clearance ( radius) & cushion time
( l
b/ C
Rad )
3 play an important
role
Inference :
- Increasing cushion length and decreasing clearance provide cubic
increase in cushion power ( lb / CRad )3
- Cushion power is proportional to velocity ( lb / tt)
- For defined parameters cushion time is inversely proportional to
(CRad)3
II Orifice restriction (assuming zero friction and no spring
action)

Newtons law of motion is sufficient to equate force and acceleration
i.e.,
F = m . d
vp /dt
VP = Piston Velocity
DP = Chamber Pressure
AP = Piston area for DP
For an orifice & oil, the head loss is given by DP @ K v02 3 x 10-6
As plunger travels, height and depending a tapers to zero. Thus in
addition to annular restriction the notch produces variable area hence
orifice effect.
Cushion chamber pressure decreases as the plunger is completing its
travel, also the velocity decreases. Hence when piston hits the cover,
it would have reduced the velocity to lower value hence the impact
magnitude gets reduced. The slope of the stroke curve at which it gets
flattened decides the effect on cylinder and connected structure. If the
structure is on wheels / track then the machine gets blow ( hammer
type).

Excavator boom, arm bucket up operation
Example of end blow :
Figures shows a typical excavator when operated to lift up the boom,
arm and bucket to extreme condition - butting.
The moving mass ( boom, arm & bucket structure) ultimately pull the
boom rod fully up and if not cushioned will hit the cover hence creates
jolting force at the rod end joint. This acts on machine, hence the
machine hops a down. This results in
- structural damage to cover and
- operator discomfort
Extreme case of non-cushioning, heavy moving mass with high velocity
may lead to toppling / capsizing / cover coming off / shearing off.
The Cushioning length and shaping of velocity curve by proper design of
restriction play an important role, considering component, machine,
operator safety and comfort.
Cushion Stroke Sensing :
Studying the behavior of stroke vs time during the plunger travel into
the bush / cover provide the state of -
- Position x - (sense)

- velocity & (x/t) = v - (compute)
- acceleration of the connected load v /t ( compute)
A - Plunger / bush enters the bore
B - Indicates unrestricted movements = butting load
C - Indicates acceptable restriction - smooth end
D - Indicates too much restriction leading to heavy Reduction of
velocity at entry.
OAB - is characterized as " mechanical shock" all Velocity
reduction / changes at B
OAD - is characterized as "hydraulic shock" max. Velocity
change at A
OAC - is characterized as "smooth change" very Small change
in velocity at A (x / t) and C (x /t)
Cushion Pressure Sensing :
When the cushion / plunger bush enters the bore thus providing
restrictions for the locked up oil in the cushion chamber then the
chamber pressure increase

The typical characteristics of cushion chamber pressure during the
cushion period are shown above.
Curve ABC :
Indicates a kick up pressure spike at the Entry of the plunger / bush
and slow discharge with long cushioning time. This is termed as
hydraulic shock. If the vehicle gets into dynamic oscillation, the
discharge will also have oscillation. This is not comfortable to
operator. Also the spike pressure may be very high (approx. 1000 Kfg
/cm2 in big equipments / masses ) which is detrimental to structure as
well as sealing elements.
Heavy restriction - close working clearance and longer cushion length
have strong influence on these characteristics.
Curve ADE :
This indicates a pressure peak not a spike. Also lesser discharge time.
Entry chamfer / radius annular restriction and cushioning length play an
important role in generating these characteristics.
If the pressure peak is within the design limits, operator comfortable
and vehicle does not experience shock / joint then cushion performance
may be acceptable. Laboratory and field trials necessary to check
cushion performance.
AFGH :
This indicates multiple pressure peaks due to changed annular
restrictions / cutting out chain of orifices in the cushion plunger.
While handling very large masses and sizes in terms of bore and rod it
become necessary to provide sufficient area for chamber flow in the
beginning and cut off the areas as the plunger travels in the cushion
bore.
Curve APQ.
In this chamber pressure raises slowly to steady value and discharges
slowly to minimum. Looks like an ideal cushioning. This is a case of
pure orifice restriction. This is characterized as parabolic (x vs. t )
cure will be a parabola and not linear. This indicates orifice flow (DQ
u DP) 1 /2 or P u v2 u x2).
While entry and annular restriction provide the coarse part of
cushioning, the notch and orifice will provide finer aspects of
cushioning.
Curve ARS :
Short small duration and small pressure indicates no restriction for
the cushion flow. In this case the entire momentum gained by the
connected mass bangs the cover ad hence equipment. This is a jolt and
heavy mechanical shock.
Cushion Performance Evaluation Tests & Tests Setups
Cushion performance is evaluated by quality of cushion in terms of
- smoothness
- softness
- no shake up / shocks
- comfortness
Following table indicates parameters which control cushion performance
and measurable to evaluate performance.
| Inputs |
Measurables |
| - Annular Clearance |
- Position |
| - Entry chamfer / radius |
- Drive Pressure |
| - North width / angle |
- Chamber Pressure |
| - Orifice |
- Noise |
Test Setups ( any of them or combination )
Test 1 : Free Cycling with drive pressure

Connect free cycling - under no load (rod free end) hydraulic power
supply to cylinder (nominal flow and relief pressure adjustable in the
range 50 .320 Kgf cm2)
Pressure transducers P1 and P2 pick up time histories of the pressures.
Position transducer will pick up the position of the plunger. Velocity
and deceleration are computed from xvs.t.
Test 2 : Crank Mass System

Small cylinders operating smaller masses- best result can be achieved
by testing using cranking mass. Typical example is a mini excavator boom
lifting once the bucket finishes digging and picks up the dug then boom
is lifted up (fully) followed by a swing and a dump. During this, the
cylinder cushion absorbs the mass energy to reduce velocity.
LVDT and pressure transducers pick up the waveforms to study the state
of position and pressure.
Test 3 : Connected Mass ( Axial)
Horizontal Set -up
For horizontal setup the mass is connected to rod ( rigid and very less
/ no friction). This is almost like a pure mass system.
In this, we can study the performance of cushion under.
A Influence of mass only ( by cutting of pump supply after achieving
motion).
B Influence of mass and drive pressure by retaining pump supply.
Vertical setup can be in low mass - small cylinder applications.
Horizontal setup is used in case of heavy large cylinder with heavy
connected mass ( on trolley).
Test4 : Actual measurements on equipment installation / machine ( final
approval )

A 100 mm or sufficient length spring return LVDT and 1000 Kgf / cm2
pressure transducer on the drive line and 100 Kgf / cm2 pressure
transducer on the cushion chamber pressure port (if available)
sufficient to assess the cushion performance.
Some aspects on noise ( during cushion action)
Since the cushioning achieved by narrow working clearance and small
orifices, following are the potential areas which can result in noise-
- Plunger / bush entry mechanical butting with bore (metallic noise)
- Plunger / bush travel inside bore - friction noise ( squeeching,
scratching)
- Annular clearance / orifice (turbulence - hissing, in extreme case
whistling)
- Sudden stoppage - mechanical butting ( bang noise)
- On retraction sometimes the oil starvation leads to cavitation noise
( Vacuum, bottle opening, marble, pebble etc.)
Engineers Stethoscope will help hear the noise at the location and
smoothness of cylinder cushion action).
Some aspects of heart during cushioning
Hydraulic cushioning is accomplished by creating restriction for the
flow, viscosity oil plays an important role in resistance hence
pressure. Viscosity decreases with increased temperature, hence the
chamber pressure thus reducing cushioning. Checking performance at 300C,
500C and 800C of oil ensure cushion effectiveness in he working
temperature rang.
Cylinder Retraction after cushioning :
Since close working clearance produced cushioning, it is important that
a quick start back should take place in the cylinder. Many designs
incorporate a free flow check value on the return side so that quick
flow of oil ensures quick start back action A right return leads to
jerky start.
A good cushion and retraction stroke vs time is in the figure
A - Start of cushioning
B - End of cushioning
C - Start of retraction
D - End of Cushion length travel
No change in the slope of x vs. t during the retraction in the region
CDE indicate retraction without jerk
Cushion Durability Tests :

Since cushioning is a accomplished with very small working clearance
creating high pressure in the cushion chamber both wear and strength
aspect are to be assessed in a laboratory durability test bench.
Critical areas for assessment during durability test
- Wear (scoring ) rubbing / scratching
- Bulging bush / tube
- Seals, Piston & Cover
- Flange bolts and piston nut integrity and strength
Summery :
1. Cushioning in hydraulic cylinder explained with physics and
mathematical model.
2. The controlling input parameters (design) and measurable output
parameters ( from performance consideration identified and sensitizes
explained.
3. Stroke and pressure waveforms use effectively to verify design
output
4. Test and setup described.
5. Heat and noise aspects discussed
Conclusion
A systematic approach presented to design cushioning for hydraulic
cylinders.
Acknowledgments
Thanks are due to Mr. K N Padmanabha, Vice President- Head of
Construction Equipment Hydraulic Business and his team members who have
systematically approached the cushioning problem and provided an
effective solution.
Thanks are also due to Mr. Seethapathy, President Managing Director for
permission present this work. Last But not the least Ms. E K Sandhya
deserves sincere thanks for excellent typing of the script.