The term sliding seals was choosen, because these „contact seals“ only function, when in
the sealing effective region between the against each other moving a lubrication film forms.
This minimizes wear and is so requirement for a long time service. At the same time it acts stabilizing
at the operation temperature in the sealing gap. An especial advantage against labyrinth seals lays
in the tightness during stand still. To such seals count mechanical face seals (carbon seals,
sliding ring seals, chapter 23.4.2.2) and radial seals.
In the literature we find the seal type under different markings like
(rotary) shaft seal, radial seal
ring, shaft sealing ring. Often it is also named after a known producer as
`Simmerring'. These seals are frequently used in aeroengines to tighten against fluids. To these belong
aeroengine oil, fuel and hydraulic fluid. The limited
temperature stability of the elastomer, from which
the sealing element (sealing lip) consists, determines the use. Main field of application are
accessory gears, pumps, control units and oil lubricated accessory devices.
Up tp the 80s there was obviously a faulty imagination about the mechanism of the
sealing effect. It wass supposed, that only the lubrication film (meniscus) seals (Lit. 23.4.2.1-3).
Not before the following years (Lit. 23.4.2.1-1 and Lit 23.4.2.1-2) the actual
sealing mechanism was recognised during tests. This is based on
special pressure distribution in axial direction
under the sealing lip. For this, an axial
oriented micro topography acts, which elastomers
typically forms at the sliding surface (Ill.
23.4.2.1-1) during the running-in phase.
With this the running-in after the assembly of the sealing ring is crucial for the
operation behaviour. This finding is the cause, why especially in elder literature and such of newer
literature build on it, some influences have been
insufficient evaluated. Corresponding less was the
success of proposals for a remedy. This produced confusion in practice. In this chapter the corrected
awareness of the hydromechanical sealing effect is used.
Fig. "Sealing effect of radial ring seals" (Lit. 23.4.2.1-1 up to Lit. 23.4.2.1-5): To avoid
problems with radial sealing rings it is helpful to understand its
function.
The sealing effect of a radial sealing ring stands in tight connection with the
sealing film between sealing lip and shaft
surface. The little width of the sealing face at the sealing lip is sufficient
for hydrodynamic effects. So a sealing film, comparable the bearing lubrication film of a journal
bearing, develops. The optimum lubrication film
thickness is about 0,25 µm. A larger film thickness
increases the leakage rate, a smaller rises friction and wear. For long time there was the opinion, that at the
side of the medium to be sealed (meniscus), the surface tension of the sealing film is crucial (Lit.
23.4.2.1-3). This assumption however could not be confirmed in tests. Instead, these have showen the
following (Lit. 23.4.2.1-1 and Lit. 23.4.2.1-2):
The special pressure distribution together with a, for elastomers typical microscopic structure of
the run-in surface from the elastomer, is crucial for the sealing
effect. It is not the forming of the meniscus!
The necessary conditions depend from the tribological conditions in the sealing gap. So a sealing ring
is similar to a micro pump (Fig. "Conveying effect in the sealing gap"). Its
conveying effect/sealing effect is, according to
test results (Lit. 23.4.2.1-2) depending from several
influences:
Fig. "Conveying effect in the sealing gap" (Lit. 23.4.2.1-1): A suitable
wear pattern of the sealing edge is crucial for the
sealing effect. This develops during run-in with slight removal of the elastomer. The microscopic
structure of the race track is for rubber like materials particularly oriented across the circumferential
direction (sketch above). It is similar chattermarks
and is elastically distorted (sketch below) from the
friction forces during operation in the lubrication gap. So the distortion depends from the distribution of
the friction forces. The maximum is shifted to the fluid side. It is determined from the
unsymmetrical distribution of the contact pressure (Fig. "Sealing effect of radial ring seals", diagram in the lower sketch).
That a conveying to the inner side i.e. the sealing effect develops the contact pressure
maximum, respectively the maximum friction forces must be shifted to the inner
side. Then the orientated surface topography of the elastomere bends so, that at the air side the at the shaft surface moved material
is `caught' and transported to the inner side (arrows in the sketch below).
The developing conveying of the rotating
shaft transports continuously, independent from the sense
of rotation, air to the side of the medium to be sealed (inner side). This process is called
pump effect or conveying effect of the sealing ring. It determines the sealing effect.
It is influenced from different effects:
Fig. "Influence of shaft sliding surface dimension" (Lit. 23.4.2.1-1): Deviations from the aligned centrical position of the shaft against the sealing ring can obviously have very different consequences.
Note: The run-in process is of crucial meaning for the sealing effect of a radial sealing ring in the later service. Therefore specifications, which influence this process, must be kept most exactly.
Fig. "Sliding surface machining problems" (Lit. 23.4.2.1-1): The
topography of the shaft surface can be of considerable
meaning for the sealing effect. Usually grinding
surfaces of the plunge cut method are concerned (last
sketch below). Anyway it must always be reckoned with angular oriented machining marks. The twist effect
of theses microscopic traces was frequently overestimated. This changed with the awareness, that
the conveying effect acts by the structure of the elastomer sealing surface as the actual sealing
mechanism (Fig. "Conveying effect in the sealing gap").
Advantage can be taken from the conveying effect of the twist from the
grinding marks also if not crucial. For this, the
direction of the pitch at the rotation direction and sealing is adjusted
(sketch above). In such a case, the twist direction must be indicated unmistakable with a
sign on the part.
Fig. "Problems of radial sealing rings" (Lit. 23.4.2.1-3 and Lit. 23.4.1-5): Also radial sealing rings are
exposed specific failure mechanisms (Fig. "O-ring failures and its causes" and Fig. "Inner crack formation at O-rings").
Overheating of the sealing lip: The sealing function must be kept over sufficient
long operation periods. For this the sealing lip must slide on a lubricant film over the
shaft surface (details left). If this sealing film drops out only a short time (seconds), too
much friction heat develops (Lit. 23.4.2.1-5). Embrittlement
and crack formation in the sealing lip decrease the thightness. An
unsuitable microscopic structure and the
shift of the contact pressure distribution (creep, wear, Ill. 23.4.2.1-1) act with this
especially unfavourable. An increase of the hardness with a decrease of the elastic
expansion drops the deflection of the sealing lip, which is necessary for the sealing effect (Ill.
23.4.2.1-1.2). This can already lead to a leak without crack formation or wear. The typical
crack appearance of an overheating is a field of
parallel radial cracks. Often is the crack
formation limited to the circumference segment in which the `dry run' was most intense (sketch
above left).
This risk is from experience highest during the first run up/sealing run after the installation
of a sealing ring. The reason is an insufficient lubrication of the sealing
surfaces (lip, shaft) during assembly.
Is a sealing ring run-in as a start successful, further start up cycles in opreation typic
time periods are no problem. Merely after long stand still periods like a
'mothballing' of the aeroengine/airplane (Fig. "Aged O-rings") or the storage of the components (e.g., gear) attention
is necessary. We should assure us in the manual, if there are for the first run certain
measures prescribed to guarantee the lubrication of the sealing rings.
Shaft surface, roughness and damages: The wear of the seal lip depends primarily from
the roughness of the shaft sliding face. Roughness tips or notches can let the oil film get
locally thicker or to break down. Do roughness tips contact, it comes to
increased wear. On the other hand it must be considered, that a
too smooth shaft surface can deteriorate the wettability and adherence
of the oil film. Therefore the roughness should lay, independent from the circumferential speed,
between 0,25 µm and 0,5 µm.
Even smallest scratches and scores in the track, running angular to the sliding
direction/circumferential direction, can be responsible for an unexpected large leak. Also
pronounced angular running grinding marks (at axial feed spiraling) are dangerous if they disturb the
hydrodynamic pumping process (Fig. "Sliding surface machining problems"). Thereby the progression of the damage relatively to the rotating direction of the shaft
and the tightening direction, plays a role (detail below left).
Especially must be payed attention at this problem during the
overhaul of shafts. The race of the sealing ring must be removed, chromium plated and ground, because of wear (volume 1, Ill. 5.4.2.2-4).
Do anti friction bearings of the shaft have too much axial
clearance, this can perform an oscillating movement with hydrodynamic pumping effect,
relatively to the sealing lip. Movements of usual
bearing clearances can even support the sealing effect (Ill. 23.4.2.1-1).
Aging of the sealing lip: The operation tempreature of the sealing
lip is crucial for the aging. With this it influences the lifetime of the seal. In the most cases, the cause for a too high temperature is a
too high radial pretension of the sealing
lip. For this possible causes are wrong contact pressure fields
or a too small diameter of the sealing edge. Thereby it is remarkable:
A too high radial pretension does not produce a better sealing effect. It rather leads to a
deteriorating overheating with the failing of the seal.
A rise of the temperature exponential shortens the life
time. It leads, corresponding the used
elastomer, to a rise in hardness (Fig. "Conveying effect in the sealing gap"),
embrittlement and crack formation. The dependence of
the aging respectively lifetime of the seal, shows material specific the diagram above right. For the
aging of the elastomers also can serve data in connection with O rings of Fig. "O-ring failures and its causes" and Fig. "Influences of O-ring materials".
Brittle crack formation during normal operation temperature is explained as result of
shock loads (e.g. pressure shocks) or vibrations of the sealing
lip. From experience brittle aging cracks occur
only during disassembly and/or mechanical deformation.
Note: Therefore the visual inspection of the seal condition allows no dependable evaluation of an aging.
Wear as consequence of a contamination: Foreign particles like abrasion, coke and dust in the oil
can promote unacceptable wear, like too high roughness. Unfortunately in the oil system develop
coke particles with failure potential, which are so small, that they will not be separated from the usual
oil filters (Fig. "Comparison of sizes from particles in oil").
Therefore clean oil is a requirement for a wear free operation of a seal
ring. Also particles at the outer side can get into the lubrication gap under unfavourable condition.
Abrasive acting particles can also develop inside the lubrication gap. Too high friction at the sealing
lip heats the oil film in a manner, that the oil cracks and coke particles form (Fig. "Formation mechanisms and oil coke features").
Wear of the shaft race: From experience also this, comparatively very hard surface, underlies
wear. Obviously sufficient hard particles are embedded in the sealing lip, to machine a narrow,
polished looking groove into the shaft. As long as there is no offset of the sealing lip, a leak must not be
expected. However, such a groove is a reason for a repair during overhaul. Thereby the shaft is sufficient
ground and then coated, mostly chromium plated (volume 4, Ill. 16.2.1.8.3-1). Although this plating has a
high hardness, intense groove formation will be observed.
Damages during assembly are the most frequent cause for the failing of a radial seal. Therefore
during handling of the seals especially attention is needed. This is also true for the
storage. The seals must be in containers/packages, which guarantee a
clean and dry atmosphere. A treatment as `bulk
good' should be unacceptable, because of the damaging
danger.
Before the installation every seal must be checked by an experienced expert. Special attention needs
Immediately before the installation the seal can be
lubricated, according to the instructions
(e.g., grease or oil), to minimize the joining forces.
Note: During installation of a radial seal ring, it must be payed attention, that correspondent the specifications/instructions the sealing faces (sealing lip, sliding face/race of the shaft) must be treated. If necessary, care must be taken for sufficient lubricant (oil, grease).
Fig. "Damaging the sealing lip by handling" (Lit. 23.4.2.1-3 and Lit. 23.4.2.1-5: The
assembling method (lower sketch right)
depends from the insertion direction. It is important, if the seal
first is moved onto the shaft and then into
the casing (seat). The other possibility is first to insert the seal into the
seat and then to introduce the shaft. If possible the first method should be preferred. The introducing face side of the shaft should
have a chamfer (upper detail) or a radius. For
repaired sliding faces especially attention must be
payed, that they are free of burrs (volume 4, Ill. 16.2.2.2-3) and have
soft edges. That is also to apply to small break outs at the
edges of a cromium coating (volume 4, Ill. 16.2.1.8.3-5). For the safety, a
sleeve with a favorable edge can be slided on the shaft (right sketch). This is especially advisable, if the shaft
has flutes. A slight rotation movement
can ease the inserting.
The symmetric and gentle forced fitting, with this the alignment of the seal in the casing/seat, can
be assured with a bell shaped tool (sketch below left). Thereby the
outer seat of the seal can be lubricated, as specified. Also the entrance edge of the locating bore in the casing should have a
chamfer (detail above left). A continuous forced fitting
process can be executed without overload. Thereby the
sticking friction is avoided. Under unfavorable assembling conditions, it can be necessary to remove at first
the tension spring of the seal and to attach it afterwards after the positioning at the seal again. That
is recommended if the seal must be inserted reverse
side.
Example 23.4.2.1-1 (Lit. 23.4.2.1-4):
In several cases a `teflon seal' (seal with
PTFE sealing lip?) in the inlet gearbox (= IGB)
failed. Seemingly parts of the seal
membrane separated. These blocked the scavenge oil
sieve. This lead to an oil accumulation in the gear.
The consequence was oil entry into the high
pressure compressor with Oil vapour/smoke in
the cabin.
Comment: From the papers available, it
could not clearly seen, which type of seal is affected.
Obviously primarily concerned was an assembly problem. It rather may be a problem of the
material, production or design.
Fig. "Remedies at shaft seals" (Lit. 23.4.2.1-3: This chart should support the practitioner. However it
can not replace informations in manuals and specifications. That must be applied for
remedies for seal failures.
Realizing (features) the problem is premise for a constructive
remedy. For this the failure mechanism with the specific causes
must be identified.
Evidence of a maintenance problem: At this point begins the difficulty with the
identification of the failure attribute. Not always it attracts our attention. If its occurence lies
in spacial distance (oil drops , oil track) to the leak, sometimes this features can not be connected.
Next arises the question, if the observation can be seen as normal or if it is unusual.
A desicion needs satisfying informations in
manuals, together with expertise and
experience. For example it must be decided if bleeding oil is to be seen as a
leakage. The details in the manual need an interpretation if the instruction allows a
discretion. In such a case enough technical qualification is necessary. We must know concerned
functions and likely consequences.
For the attendant or supervisor, detectable
outside features of a failures of a radial
sealring are:
Is the indication recognized respectively classified as a failure, the cause must be
suggested from the relevant features of the finding.
References
23.4.2.1-1 M.Kammüller, H.K.Müller, „Physikalische Ursachen der Dichtwirkung von
Radial-Wellendichtringen” , ATZ Automobildtechnische Zeitschrift“ 88 (1986) 1, page 39-45.
23.4.2.1-2 W.Hermann, H.-W.Seffler, „Neue Erkenntnisse für den Abdichtungsmechanismus
von Radial-Wellendichtringen” , ATZ Automobildtechnische Zeitschrift“ 87 (1985) 9, page
475-484.
23.4.2.1-3 M.W.Brown, „Seals and Sealing Handbook” , Verlag „Elsevier“, page 137-166.
23.4.2.1-4 P.Lironi, „CF6-80C2 engine history and evolution” , Zeitschrift „Engine
Yearbook 2007“, page 80-85.
23.4.2.1-5 „Mitteilungen des Simrit-Werkes Nr. 700/60” , Publisher: Carl Freudenberg, 1960.