U.S. patent application number 14/851679 was filed with the patent office on 2015-12-31 for shrouded face seal and components thereof.
The applicant listed for this patent is United Technologies Corporation. Invention is credited to Colin D. Craig, Enzo DiBenedetto, Christopher P. Kmetz, Jonathan Logan Miller, Mark R. Sondeen.
Application Number | 20150377361 14/851679 |
Document ID | / |
Family ID | 37885923 |
Filed Date | 2015-12-31 |
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United States Patent
Application |
20150377361 |
Kind Code |
A1 |
Craig; Colin D. ; et
al. |
December 31, 2015 |
SHROUDED FACE SEAL AND COMPONENTS THEREOF
Abstract
One embodiment of the seal housing for a face seal described
herein include a base with a seal element support and a shroud both
extending from the base in a common direction. The seal element
support and the base define a space for receiving a seal element.
The shroud includes a tip having a head portion that tapers toward
a neck portion that is reduced in size relative to the head
portion. The tip is secured to a stem of the shroud through a set
of circumferentially distributed countersunk holes.
Inventors: |
Craig; Colin D.; (West
Hartford, CT) ; DiBenedetto; Enzo; (Middletown,
CT) ; Kmetz; Christopher P.; (Amston, CT) ;
Miller; Jonathan Logan; (Ware, MA) ; Sondeen; Mark
R.; (West Hartford, CT) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
United Technologies Corporation |
Hartford |
CT |
US |
|
|
Family ID: |
37885923 |
Appl. No.: |
14/851679 |
Filed: |
September 11, 2015 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
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14665068 |
Mar 23, 2015 |
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14851679 |
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12826629 |
Jun 29, 2010 |
9004492 |
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14665068 |
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11266454 |
Nov 3, 2005 |
7837199 |
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12826629 |
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Current U.S.
Class: |
277/370 |
Current CPC
Class: |
F16J 15/3468 20130101;
F01D 11/003 20130101; F05D 2240/55 20130101 |
International
Class: |
F16J 15/34 20060101
F16J015/34; F01D 11/00 20060101 F01D011/00 |
Claims
1. A face seal assembly, comprising a seal seat and a seal element
carried by a seal housing and cooperating with the seal seat to
establish a seal, the seal housing including a seal element support
and a shroud, wherein the shroud includes a tip having a head
portion that tapers toward a neck portion that is reduced in size
relative to the head portion, the tip secured to a stem of the
shroud through a set of circumferentially distributed countersunk
holes.
2. The assembly of claim 1, wherein the shroud is axially elongated
relative to the support.
3. The assembly of claim 2, wherein the seal element includes a
blank with a nose extending axially therefrom, the blank being
stepped so that a first radial region extends axially beyond a
second radial region of the blank.
4. The assembly of claim 3, wherein the first and second radial
regions define respective first and second steps, and the tip is
axially between the first and second steps.
5. The assembly of claim 1, wherein the seal seat is a seal ring,
and the seal element is a carbon ring residing radially between the
support and the shroud.
6. The assembly of claim 1, wherein the shroud is radially inboard
of the support.
7. The assembly of claim 1, wherein the seal housing exclusive of
the tip is made of a parent material and the tip comprises a second
material different than the parent material.
8. The assembly of claim 7, wherein the second material is selected
from the group of materials consisting of: a) materials more
lubricious than the parent material; b) materials harder than the
parent material; and c) materials more abradable than the parent
material.
9. The assembly of claim 1, wherein the tip is a molded tip.
10. The assembly of claim 1, wherein the tip completely fills a
corresponding one of the circumferentially distributed holes when
the tip is secured to the stem of the shroud.
11. The assembly of claim 1, wherein the neck portion is positioned
radially between the head portion and the seal element.
12. The assembly of claim 1, wherein the tip is configured to
contact the seal seat.
13. The assembly of claim 1, wherein the seal housing is configured
such that all portions of the tip reside radially inside the seal
element.
14. A seal housing for a face seal comprising a base with a seal
element support and a shroud both extending from the base in a
common direction, the seal element support and the base defining a
space for receiving a seal element, wherein the shroud includes a
tip having a head portion that tapers toward a neck portion that is
reduced in size relative to the head portion, the tip secured to a
stem of the shroud through a set of circumferentially distributed
countersunk holes.
15. The seal housing of claim 14, wherein the seal element includes
a blank with a nose extending axially therefrom, the blank being
stepped so that a first radial region extends axially beyond a
second radial region of the blank, wherein the first and second
radial regions define respective first and second steps, and the
tip is axially between the first and second steps.
16. The seal housing of claim 14, wherein the tip comprises a
molded tip.
17. The assembly of claim 1, wherein the tip completely fills a
corresponding one of the circumferentially distributed holes when
the tip is secured to the stem of the shroud.
18. The seal housing of claim 14, wherein the neck portion is
positioned radially between the head portion and the seal
element.
19. The seal housing of claim 14, wherein the tip is configured to
contact the seal seat.
20. The seal housing of claim 14, wherein the seal housing is
configured such that all portions of the tip reside radially inside
the seal element.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application is a divisional of U.S. application Ser.
No. 14/665,068, which was filed on 23 Mar. 2015. U.S. application
Ser. No. 14/665,068 is a divisional of U.S. application Ser. No.
12/826,629, which was filed on 29 Jun. 2010 and has issued as U.S.
Pat. No. 9,004,492. U.S. application Ser. No. 12/826,629 is a
divisional of U.S. application Ser. No. 11/266,454, which was filed
on 11 Nov. 2005 and has issued as U.S. Pat. No. 7,837,199. Each of
these applications is incorporated herein by reference.
TECHNICAL FIELD
[0002] This disclosure relates to face seals and particularly to a
carbon face seal whose performance deteriorates in a relatively
benign way in comparison to conventional seals.
BACKGROUND
[0003] Carbon face seals are used in machinery, such as turbine
engines, to effect a fluid seal between regions of high and low
fluid pressure. For example, carbon seals are used to prevent hot,
high pressure air from entering a bearing compartment operating at
a lower pressure. A typical carbon seal for a turbine engine
includes an annular carbon ring secured to an annular,
nonrotatable, axially translatable seal housing. The seal also
includes a seal seat affixed to a rotatable shaft and positioned
axially adjacent to the carbon ring. The carbon ring comprises a
base (or blank) and a nose projecting axially from the base. The
nose is urged into contact with the seal seat by a combination of
spring forces acting on the seal housing and the net resultant of
axially opposing fluid pressure forces acting on the seal housing
and the carbon ring. The contact area between the carbon ring and
the seal seat equals the annular area of the nose. The contact
between the nose and the seal seat resists fluid leakage across the
seal in the radial direction, i.e. toward or away from the axis of
rotation of the seal seat.
[0004] During operation, the nose gradually wears away. Ordinarily,
the seal is replaced or refurbished before the nose is completely
worn away. Occasionally, however, accelerated seal wear can result
in complete wear of the nose so that the base of the carbon ring
contacts the seal seat. As a result, the contact area between the
carbon ring and the seal seat equals the annular area of the base,
which is larger than the contact area of the nose. This affects the
resultant of the axially opposing fluid pressure forces such that
the net pressure force is less favorable for maintaining reliable,
positive contact between the carbon ring and the seal seat.
Unfortunately, the transition between the normal condition in which
the nose contacts the seal seat, and the highly deteriorated
condition in which the base contacts the seal seat, although it
occurs very infrequently, can occur with little warning. In
addition, more abrupt failure or deterioration of the carbon ring
can have a similar adverse effect on the resultant of the fluid
pressure forces. As a result there may be an unanticipated period
of engine operation during which fluid leaks past the seal
[0005] What is needed is a carbon seal that deteriorates gracefully
in order to exhibit a detectable and benign operating
characteristic that clearly indicates that maintenance is
required.
SUMMARY
[0006] A face seal assembly according to an exemplary aspect of the
present disclosure includes, among other things, a seal seat and a
seal element carried by a seal housing and cooperating with the
seal seat to establish a seal. The seal housing includes a seal
element support and a shroud. The shroud includes a tip having a
head portion that tapers toward a neck portion that is reduced in
size relative to the head portion. The tip is secured to a stem of
the shroud through a set of circumferentially distributed
countersunk holes.
[0007] In another exemplary embodiment of the above-described face
seal assembly, the shroud is axially elongated relative to the
support.
[0008] In another exemplary embodiment of any of the
above-described face seal assemblies, the seal element includes a
blank with a nose extending axially therefrom. The blank is stepped
so that a first radial region extends axially beyond a second
radial region of the blank.
[0009] In another exemplary embodiment of any of the
above-described face seal assemblies, the first and second radial
regions define respective first and second steps, and the tip is
axially between the first and second steps.
[0010] In another exemplary embodiment of any of the
above-described face seal assemblies, the seal seat is a seal ring,
and the seal element is a carbon ring residing radially between the
support and the shroud.
[0011] In another exemplary embodiment of any of the
above-described face seal assemblies, the shroud is radially
inboard of the support.
[0012] In another exemplary embodiment of any of the
above-described face seal assemblies, the seal housing exclusive of
the tip is made of a parent material and the tip comprises a second
material different than the parent material.
[0013] In another exemplary embodiment of any of the
above-described face seal assemblies, the second material is
selected from the group of materials consisting of: a) materials
more lubricious than the parent material; b) materials harder than
the parent material; and c) materials more abradable than the
parent material.
[0014] In another exemplary embodiment of any of the
above-described face seal assemblies, the tip is a molded tip.
[0015] In another exemplary embodiment of any of the
above-described face seal assemblies, the tip completely fills a
corresponding one of the circumferentially distributed holes when
the tip is secured to the stem of the shroud.
[0016] In another exemplary embodiment of any of the
above-described face seal assemblies, the neck portion is
positioned radially between the head portion and the seal
element.
[0017] In another exemplary embodiment of any of the
above-described face seal assemblies, the tip is configured to
contact the seal seat.
[0018] In another exemplary embodiment of any of the
above-described face seal assemblies, the seal housing is
configured such that all portions of the tip reside radially inside
the seal element.
[0019] A seal housing for a face seal according to yet another
exemplary aspect of the present disclosure includes, among other
things, a base with a seal element support and a shroud both
extending from the base in a common direction. The seal element
support and the base define a space for receiving a seal element.
The shroud includes a tip having a head portion that tapers toward
a neck portion that is reduced in size relative to the head
portion. The tip is secured to a stem of the shroud through a set
of circumferentially distributed countersunk holes.
[0020] In another exemplary embodiment of the above-described seal
housing, the seal element includes a blank with a nose extending
axially therefrom. The blank is stepped so that a first radial
region extends axially beyond a second radial region of the blank.
The first and second radial regions define respective first and
second steps, and the tip is axially between the first and second
steps.
[0021] In another exemplary embodiment of any of the
above-described seal housings, the tip comprises a molded tip.
[0022] In another exemplary embodiment of any of the
above-described seal housings, the tip completely fills a
corresponding one of the circumferentially distributed holes when
the tip is secured to the stem of the shroud.
[0023] In another exemplary embodiment of any of the
above-described seal housings, the neck portion is positioned
radially between the head portion and the seal element.
[0024] In another exemplary embodiment of any of the
above-described seal housings, the tip is configured to contact the
seal seat.
[0025] In another exemplary embodiment of any of the
above-described seal housings, the seal housing is configured such
that all portions of the tip reside radially inside the seal
element.
[0026] The foregoing and other features of the various embodiments
of the disclosed seal will become more apparent from the following
detailed description and the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0027] FIG. 1 is a cross sectional side elevation view showing an
improved carbon seal.
[0028] FIGS. 2, 3 and 4 are schematic views similar to FIG. 1, but
circumferentially offset from FIG. 1, showing fluid pressure forces
acting on a traditional seal in a normal or normally deteriorated
condition, a highly deteriorated condition and a damaged or
severely degraded condition respectively.
[0029] FIGS. 5-8 are schematic views similar to FIGS. 2 through 4
showing fluid pressure forces acting on an improved seal in normal,
highly deteriorated, severely deteriorated and damaged conditions
respectively.
[0030] FIG. 9 is a view illustrating a seal housing with a shroud
whose tip is made of the same material as the rest of the seal
housing.
[0031] FIG. 10 is a view similar to FIG. 9 showing a seal housing
made of a parent material and having a shroud with a bonded or
impregnated tip made of a second material.
[0032] FIGS. 11-13 are views similar to FIG. 9 but with a shroud
having a tip in the form of an insert or attachment.
DETAILED DESCRIPTION
[0033] Referring to FIG. 1, a shaft 20 for a rotary machine, such
as a turbine engine, is rotatable about an axis 22. A seal seat in
the form of an annular ring 24 is secured against a shoulder on the
shaft by a nut 26. The seal seat extends radially outwardly from
the shaft and circumscribes the axis. The seal seat is one
component of a face seal assembly.
[0034] The face seal assembly also includes an annular,
nonrotatable seal support 28 and a pair of annular seal housings
32. Each seal housing includes a base 34 and a grooved secondary
seal holder 36 at one end of the base. The secondary seal holder
holds a secondary seal 38 in contact with a cylindrical bore of the
seal support. The other end of the seal housing includes an axially
extending shroud 42 and an axially extending support lip 44 that
serves as a seal element support. The shroud 42 is radially offset
from the lip 44 to define an annular space 46 for receiving a seal
element. The shroud is also axially elongated relative to the lip.
An annular flange 48 with circumferentially distributed slots 50
projects radially outwardly from the lip 44.
[0035] The face seal assembly also includes a seal element 52
residing in the space 46 and secured to the lip 44 by an
interference fit. The seal element includes a base or blank 54 and
a nose 56 extending axially from the blank. The blank is double
stepped such that a first, radially inboard region 58 of the blank
extends axially beyond a second radially outboard region 60 of the
blank to define a first or radially inner step 61 and a second or
radially outer step 63. Moreover, inner step 61 resides axially
beyond the tip of shroud 42 whereas outer step 63 does not reside
axially beyond the shroud tip. In other words, the tip of the
shroud is axially between the steps 61, 63. The seal element is
typically made of a graphitic carbon material and is often referred
to as a carbon element even though it is not made of pure carbon.
In the illustrated application, the carbon element is annular and
therefore can be referred to as a carbon ring.
[0036] A set of circumferentially distributed support pins such as
representative pin 64, each projects axially from the seal support
28 and passes through a corresponding slot 50 in the flange 48.
Springs 66 (depicted in FIGS. 5-8) are circumferentially offset
from the pins 64. The springs are compressed between the flange 48
of housing 32 and the support 28 so that they exert a force on the
flange 48 to urge the nose of the carbon ring into contact with the
seal seat 24. The interface between the nose and the seal seat may
be unlubricated or "dry" as seen at the left side of the
illustration, or it may be lubricated or "wet" as seen at the right
side of the illustration. In a wet seal, lubricant flows to the
interface by way of circumferentially distributed lubricant
passages 68 in the seal seat.
[0037] During engine operation, high pressure air is present in the
annular cavity 70 radially inboard of the seal and radially
outboard of the shaft 20. Lower pressure air intermixed with oil
occupies a bearing compartment 72, which is the region outboard of
the seal. The seal resists leakage of the higher pressure air into
the lower pressure bearing compartment.
[0038] Referring additionally to FIG. 2, the operation of the
above-described shrouded seal is best understood by first
considering a conventional seal. FIG. 2 shows the conventional seal
in a normal or substantially undeteriorated condition. FIG. 2 also
suffices to show the seal in a normally deteriorated condition,
i.e. with the nose only partially worn away. The arrow F.sub.s
represents the force exerted on the seal housing 32 by the springs
66. Force graphs f.sub.o and f.sub.c show the axially opposing,
radially distributed forces F.sub.O, F.sub.C acting on the seal
housing, carbon ring and secondary seal as result of the disparate
pressures in cavity 70 and compartment 72. The force vectors in
graphs f.sub.o and f.sub.c are illustrated as terminating on
respective common planes to facilitate comparisons of the aggregate
pneumatic forces. However those skilled in the art will recognize
that the forces actually act on the axially facing surfaces of the
seal housing, carbon ring and secondary seal. Graph f.sub.c shows a
relatively high pressure acting on the high pressure side of the
seal and a low pressure acting on the low pressure side of the
seal. Graph f.sub.o shows high pressure acting on the high pressure
side of the seal, low pressure acting on the low pressure side of
the seal, and a radially varying pressure in a transition region
across the nose 56 of the carbon ring. As is evident, the nose
throttles the high pressure down to the low pressure across a
narrow radial region. The combination of F.sub.S and F.sub.C
exceeds F.sub.O to keep the seal closed.
[0039] FIG. 3 shows the conventional seal in a highly deteriorated
condition in which the nose has been entirely worn away. F.sub.C is
the same as in FIG. 2. However because the nose has been worn away,
the base portion 54 of the carbon ring throttles the high pressure
down to the low pressure across a radial transition region that is
relatively wide in comparison to the transition region of FIG. 2.
As a result higher pressure, and therefore higher forces, act over
a larger radial region than is the case in FIG. 2. Accordingly, the
aggregate force F.sub.O acting on the highly deteriorated seal of
FIG. 3 exceeds the aggregate force F.sub.O acting on the normal or
normally deteriorated seal of FIG. 2. Furthermore, F.sub.S is
slightly smaller than it is in FIG. 2 due to the increased spring
elongation (decompression) and consequent reduction in spring
force. Due to the change in forces acting on the seal, there is a
potential for F.sub.O to exceed the combination of F.sub.S and
F.sub.C resulting in separation of the carbon ring 52 from the seal
seat 24. This separation will allow leakage through the resulting
gap as indicated by the small fluid flow arrows. The force graphs
and forces would be as shown in FIG. 4 if the carbon ring were
broken away along part or all of its circumference. This would also
result in the potential for leakage as indicated in FIG. 4.
[0040] As mentioned previously, the transition between the normal
condition in which the nose contacts the seal seat, and the highly
deteriorated condition or severely deteriorated conditions occurs
very infrequently, but can occur with little warning. As a result
there may be an unanticipated period of engine operation during
which fluid leaks past the seal.
[0041] FIG. 5 corresponds to FIG. 2, but shows the improved, double
stepped shrouded seal in an undeteriorated or normally deteriorated
condition. As is evident, the forces are substantially the same as
those of FIG. 2, with the result that the seal is urged closed.
[0042] FIG. 6 shows the improved, double stepped shrouded seal in a
highly deteriorated condition similar to the condition of the
conventional seal in FIG. 3. The blank of the carbon ring of FIG. 6
includes the first radial region 58 and its associated step 61
extending axially beyond the second radial region 60 and its
associated step 63. In addition, the seal of FIG. 5 includes the
shroud 42 on the seal housing. The axially extended first region 58
throttles the high pressure across a radial transition region that
is radially narrower than the transition region of FIG. 3.
Accordingly, the aggregate force F.sub.O of FIG. 6 is less than the
aggregate force F.sub.O of FIG. 3. As a result, the carbon ring 52
of FIG. 6 is less likely to separate from the seal seat 24 than is
the carbon ring of FIG. 3.
[0043] FIG. 7 shows the improved, shrouded seal in a more severely
deteriorated condition. In comparison to FIG. 6, FIG. 7 shows the
carbon ring 52 worn back essentially to the shroud 42 and therefore
shows a throttling effect attributable to the shroud. The shroud
and the axially extended first region 58 of the carbon ring
throttle the high pressure across a radial transition region that
is radially narrower than the transition region of FIG. 3.
Accordingly, the force magnitude F.sub.O of FIG. 7 is less than the
force magnitude F.sub.O of FIG. 3. As a result, the carbon ring of
FIG. 7 is less likely than the carbon ring of FIG. 3 to separate
from the seal seat 24 and permit leakage. As further wear of the
carbon ring occurs, the shroud tip will eventually contact the seal
seat 24 resulting in a more pronounced throttling effect.
[0044] FIG. 8 shows the improved, shrouded seal in a damaged
condition in which the carbon ring has been broken away over all or
part of its circumference. The shroud 42 contacts the seal element
and throttles the high pressure across a radially narrow transition
so that the seal remains closed and resists leakage.
[0045] As is evident, the improved, shrouded seal deteriorates more
gradually than a conventional unshrouded seal. The gradual
deterioration is desirable because it manifests itself as
noticeable but minor anomalies in engine performance. These minor
anomalies make the engine operator aware that seal replacement or
repair is required. Such replacement or repair may then be effected
before the seal deteriorates enough to cause more significant
problems.
[0046] With the construction and operation of the seal having now
been described, certain variants may now be better appreciated.
[0047] FIG. 9 shows a seal like that of FIGS. 1 and 5-8 in which
the housing 32 is made of a selected material. The shroud has a tip
74 at its axial extremity remote from the housing base 34. The tip
is made of the same material as the rest of the housing.
[0048] FIG. 10 shows a seal in which the housing 32 is made of a
parent material and the shroud has a tip 74 which is a region of
the shroud impregnated with a second material. Alternatively, the
shroud tip may be a feature made of or impregnated with a second
material and bonded to the rest of the shroud or may be a coating.
The second material may be any material having characteristics that
are desirable when the tip contacts the seal seat 24. These include
materials more lubricious than the parent material, materials
harder than the parent material and materials more abradable than
the parent material.
[0049] FIGS. 11-13 show a seal in which the shroud comprises a stem
76 and a tip in the form of an insert or attachment 78 affixed to
the stem. In FIG. 11 the insert is affixed with a radially outer
snap 82. In FIG. 12 the insert is affixed with a radially inner
snap 84. In FIG. 13 the insert is a molded tip secured to the stem
76 through a set of circumferentially distributed countersunk holes
86. The tip insert may be made of a material having characteristics
that are desirable when the tip contacts the seal ring 24. These
include materials more lubricious than the parent material,
materials harder than the parent material and materials more
abradable than the parent material.
[0050] Although the improved seal has been shown and described with
reference to specific embodiments thereof, it will be understood by
those skilled in the art that various changes in form and detail
may be made without departing from the invention as set forth in
the accompanying claims.
* * * * *