US1831224A - Labyrinth packing - Google Patents
Labyrinth packing Download PDFInfo
- Publication number
- US1831224A US1831224A US315302A US31530228A US1831224A US 1831224 A US1831224 A US 1831224A US 315302 A US315302 A US 315302A US 31530228 A US31530228 A US 31530228A US 1831224 A US1831224 A US 1831224A
- Authority
- US
- United States
- Prior art keywords
- strips
- packing
- conical
- members
- secured
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/447—Labyrinth packings
- F16J15/4476—Labyrinth packings with radial path
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S277/00—Seal for a joint or juncture
- Y10S277/931—Seal including temperature responsive feature
Definitions
- the labyrinth packing concerned in this invention comprises an annular strip secured at one end to one of the relatively rotatable members and so arranged relativelyto another annular strip secured at one end to the other relatively rotatable member, that a constricted passage is formed therebetween.
- Such packing has already been described in the specification of Letters Patent No. 1,7 08,-
- At least one of the annular strips is conically formed and provides in combination with a radial or conical surface on the other strip an axial clearance constriction, the construction and arrangement-of these parts being such thatupon the occurrence of rubbing contact between the :strips at the constriction, said conical strip, by its expansion due to increased temperature at the region of contact, tends to increase theaxial width of the constriction by combined mation to obtain more effective throttling, or
- the strips on the respective members may coact in pairs wherein either or both strips maIy be of conical form.
- e invention also provides labyrinth packing comprising one or more pairs of coacting annular strips whereof one strip is secured at one end to'one of the relativelyirotatable members and theother strip to the other relatively rotatable member, the strips being shaped and arranged to form one or more axial clearance constrticted passages therebetween such that upon the occurrence of rubbingcontact between the strips, both of the strips, by expansion due to increased temperature at the places of contact, tend to, move apart so as to increase the axial width of such constricted passages. Furthermore,
- one strip may be shaped and arranged so as to form a plurality of constrictions together with one or more,
- the packing comprises a set of strips adapted to coact with one or a plurality'of other "strips
- constricted passages are not necessarily in line, but may be staggered or otherwise displaced so that, while the general direction of the steam orother'fluid through the'several passa es is more or less radial, it
- conical strips which are preferably inclined at an angle from 30 to 60 to the axis of rotation, while the angle made by each of said strips on the inside with respect to the ,coacting surface provided by an adjacent strip is less than and is pre erably also from 30? to 60.
- Figs. 1 to 17 are sectional views, taken on a In the single form shown in Fig. 1, the
- Fig. 2 shows a construction similar to Fig.
- the coni cal strips 6 carried by the member may be provided with annular root portions 7 extending inwardly, the conical portions of the strips extending outwardly from the inner ends of said root portions.
- This latter construction may be developed by the provision of a plurality of conical strips integral withv the common root portion, as shown for example, in Fig. 8 while Figs. 6 and 7 show similar developments applied to the form of construction indicated. in Fig.1,
- the buttress members 8, 9 shown in Figs. .7 and 8, resepctively, are stepped so that the constricted passages formed betweenthe coacting packing members are relatively staggered, thereby permittitng more effectivethrottling to be Fig.
- FIG. 9 shows a further modified construction wherein a buttress member such as shown in Fig. 6, is provided with laterally extending strips 10, the extremities of which form substantially radial constricted passages 11 in conjunction with the ends of the conical strips 12 carried by the -member A.
- This construction possesses the advantage over those in which a plain buttress member is employed, in that upon the occurrence of rubs.
- FIGs. l and 5 and 1017 Further examples of packing provided in accordance with the invention and comprising pairs of coacting conical strips are shown in Figs. l and 5 and 1017. WVith these constructions the arrangements are such that upon the occurrence'of rubbing contact be-' tween a pair of strips, each contacting strip tends to move away from the coacting surface of the opposed strip so as to tend to increase the axial width of the constricted passage therebetween.
- Figs. 4 and 5 showtliis feature ofthe invent-ion applied to the forms of packing shown in Figs. 2 and 3 the angular buttress members of the latter figures being replaced by conical strips 13, similar to those shown in Fig. 1.
- Fig. 10 shows a simple construction in which each packing member let, 15 comprises a plurality. of conical strips, the ends of which coact'to form a series of radial con stricted passages or axial clearances.
- Fig. 11 a somewhat similar construction is shown, the constricted passages being, however, formed between conical end surfaces of the strips, whereby a devious path is presented for the passage of fluid between the packing members. Devious paths are also afforded
- the conical strips are inclined at an angle by the constructions shown in Figs. 12 and 13 wherein the constricted passages formed between consecutive pairs of strips are relatlvly staggered.
- Figs. 14-17 show by way of example, and
- Fig. 17 also shows a feature which may, if desired be applied to certain ofthe constructions above described, namely, that the strips of the member 16 are arranged with a greater conical angle than those of the member 17.
- the axial width of the constrictions may be adjusted, for example, when assembling the packing, by axial movement of the packing members.
- the packing is particularly suitable for use in high pressure turbines to seal the interior of a turbine cylinder from communication with the external atmosphere or for balance pistons or as diaphragm packing between pressure stages of the turbine or elsewhere as may be desired.
- the packing members may be formed integrally with the relatively rotatable membersby which they are carried, or may be separately formed and secured in position in any convenient manner.
- FIG. 18 A constructional example showing the application of the packing to a turbine diaphragm is illustrated in Fig. 18.
- the packing rings are made up of arcuate packing members 18 having a plurality of strips 19, said members 18 being secured in grooves 20 formed in the rotor and held in position by means of caulking strips 21.
- the strips 22 of the packing carried by the diaphragm 23 are secured to the cylinder 24: through the intermediary of nozzle or blading portions 25 riveted or otherwise secured to the diaphragm 23 and held by caulking members 26 in a slot 27 formed inside the cylinder 24.
- the portions 25 are spigoted and grooved at 28, 29 to engage corresponding parts of slot 27 thereby preventing any possibility of the diaphragm closing in .and altering the position of the nozzle passages or the gland members.
- the axial width of the constrictions 30 will be adjusted to the desired dimensions when assembling the turbine, and
- a labyrinth packing for sealing the space between two relatively rotatable members comprising a plurality of annular conicalpacking elements disposed in telescopic rotatable members comprising .a plurality of annular conical packing strips disposed in telescopic relation and secured at their mner edges to one of said members, a plurality of other conical packing strips disposed in telescopic relation and secured at their inner edges to theother of said members, the free edges of the strips secured to one member opposing the free edges of the strips secured to the other member with axial packing clearances therebetween.
- a labyrinth packing for sealing the space between two relatively rotatable members comprising a plurality of annular conical packing elements disposed in telescopic relation and secured at their inner edges to one of said members, the outer free edges of said elements beingv disposed in closelyspaced axially-opposed relation to parts of the other member so as to provide axial packing clearances therewith, said conical packing elements being inclined at an angle from 30 to 60 to the axis of rotation.
- An axial'clearance labyrinth packing for sealingthe space between two relatively rotatable members comprising a plurality of annular conical packing strips disposed in telescopic relation and secured at their inner edges to one of said members, a plurality of other conicalpacking strips disposed in telescopic relation and secured at their inner edges to the other of said members, the free edges of the strips secured to one member opposing the free edges of the strips secured to the other member in end to end relation with axial packing clearances therebetween, said conical packing strips being inclined at an angle from 30 to 60 to the axis of rotation.
- An axial clearance labyrinth packing for sealing the space between two relatively rotatable members comprising a plurality of annular conical packing strips disposed in telescopic relation and secured at their inner ends to one of said members, a plurality of other conical packing strips also disposed in telescopic relation and secured at their inner strips secured to the other member with axial. packing clearances therebetweem said end surfaces being dispbsed out of alignment so that the packing clearances are not in alignment and thereby provide a devious path for the passage of fluid between the packing members.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Nov. 10, 1931v K. BAUMANN LABYRINTH PACKING Filed Oct. 26, 1928 2 Sheets-Sheet l INVENTOR Karl Buumann WITNESS ATTORNEY NOV. 10, 1931. BAUMANN LABYRINTH PACKING Filed Oct. 26. 1928 2 Sheets-Sheet 2 WITNESS url Bcumqnn ATTORNEY Patented Nov. 10, 1931 BAUMANN, or UBMST'ON, ENGLAND, ssrenon r WESTINGHOUSE ELECTRIC &0 MANUFACTURING COMPANY, A CORPORATION OF PENNSYLVANIA LAIBYRINTH PACKING Application filed October 26, 1928, Serial No. 315,302,.and in Great Britain November 7,1927.
- provide a devious path for the steam or other fluid which tends to pass from the high pressure to the low pressure side of the packing and for the purpose of considering the construction and arrangement of the packing strips it is convenient to refer to the cross-sec- .tional form which they present on a plane containing the axis of rotation. The strips considered in this manner are more or less of cantilever form, one end being free, and the other end, conveniently termed the root,
'25". being secured directly or indirectly to the appurtenant relatively rotating member. It is in this sense thatthe term end is hereinafter employed or the cross-section considered where stated. v c
The labyrinth packing concerned in this invention comprises an annular strip secured at one end to one of the relatively rotatable members and so arranged relativelyto another annular strip secured at one end to the other relatively rotatable member, that a constricted passage is formed therebetween. Such packing has already been described in the specification of Letters Patent No. 1,7 08,-
044, April 9, 1929. According to the present invention however, at least one of the annular strips is conically formed and provides in combination with a radial or conical surface on the other strip an axial clearance constriction, the construction and arrangement-of these parts being such thatupon the occurrence of rubbing contact between the :strips at the constriction, said conical strip, by its expansion due to increased temperature at the region of contact, tends to increase theaxial width of the constriction by combined mation to obtain more effective throttling, or
the strips on the respective members may coact in pairs wherein either or both strips maIy be of conical form. 1
e invention also provides labyrinth packing comprising one or more pairs of coacting annular strips whereof one strip is secured at one end to'one of the relativelyirotatable members and theother strip to the other relatively rotatable member, the strips being shaped and arranged to form one or more axial clearance constrticted passages therebetween such that upon the occurrence of rubbingcontact between the strips, both of the strips, by expansion due to increased temperature at the places of contact, tend to, move apart so as to increase the axial width of such constricted passages. Furthermore,
in any of the constructions one strip may be shaped and arranged so as to form a plurality of constrictions together with one or more,
coacting strips. In cases where the packing comprises a set of strips adapted to coact with one or a plurality'of other "strips, the
constricted passages ,therebetween. are not necessarily in line, but may be staggered or otherwise displaced so that, while the general direction of the steam orother'fluid through the'several passa es is more or less radial, it
is also necessary or said fluid to flow in a devious path.
It is evident that the invention may be car ried out in a variety of forms, all of which,
however, employ conical strips which are preferably inclined at an angle from 30 to 60 to the axis of rotation, while the angle made by each of said strips on the inside with respect to the ,coacting surface provided by an adjacent strip is less than and is pre erably also from 30? to 60.
obtained.
The above and other objects are effected by my invention, as will be apparent from the following description and claims taken in connection with the accompanying drawings, forming a part of this aplication, in which:
Figs. 1 to 17 are sectional views, taken on a In the single form shown in Fig. 1, the
'- conical strips 1, secured at one end to one of therelatively rotatable members, namely A, terminate at their free ends adjacent the sides of annular buttress-like projections 2, thereby forming substantially radial constricted passages 3 or axial clearances between the adjacent surfaces of the strips 1 and the projections 2. If rubbing contact should occur between these adjacent surfaces, the conical strips 1 will be immediately heated at their freejends and will tend to expand circumferentially, thereby moving in a direction partlyradial and partly axial away from the projections 2, as indicated (somewhat exaggerated) by dotted lines in Fig. 1. .The axial clearances between the coacting members 1, 2 of the packing are thus automatically adjusted in use so as to reduce to a minimum wear and friction losses due to rubbing contact.
Fig. 2 shows a construction similar to Fig.
1 in that it employs conical strips coacting with the sides of annular buttress-like projections, but in this case the conical strips A are secured to the outer member B and pass over the buttresses 5 and coact with the sides of the latter remote from the roots of the respective conical strips.
Alternatively, as shown in Fig. 3, the coni cal strips 6 carried by the member may be provided with annular root portions 7 extending inwardly, the conical portions of the strips extending outwardly from the inner ends of said root portions. This latter construction may be developed by the provision of a plurality of conical strips integral withv the common root portion, as shown for example, in Fig. 8 while Figs. 6 and 7 show similar developments applied to the form of construction indicated. in Fig.1, The buttress members 8, 9 shown in Figs. .7 and 8, resepctively, are stepped so that the constricted passages formed betweenthe coacting packing members are relatively staggered, thereby permittitng more effectivethrottling to be Fig. 9 shows a further modified construction wherein a buttress member such as shown in Fig. 6, is provided with laterally extending strips 10, the extremities of which form substantially radial constricted passages 11 in conjunction with the ends of the conical strips 12 carried by the -member A. This construction possesses the advantage over those in which a plain buttress member is employed, in that upon the occurrence of rubs.
bing contact at the constricted passages 11 there will be no tendency for the outer member to bulge or warp laterally as may possibly from 3 to 60 to the axis of rotation.
Further examples of packing provided in accordance with the invention and comprising pairs of coacting conical strips are shown in Figs. l and 5 and 1017. WVith these constructions the arrangements are such that upon the occurrence'of rubbing contact be-' tween a pair of strips, each contacting strip tends to move away from the coacting surface of the opposed strip so as to tend to increase the axial width of the constricted passage therebetween. Figs. 4 and 5 showtliis feature ofthe invent-ion applied to the forms of packing shown in Figs. 2 and 3 the angular buttress members of the latter figures being replaced by conical strips 13, similar to those shown in Fig. 1.
Fig. 10 shows a simple construction in which each packing member let, 15 comprises a plurality. of conical strips, the ends of which coact'to form a series of radial con stricted passages or axial clearances. In Fig. 11 a somewhat similar construction is shown, the constricted passages being, however, formed between conical end surfaces of the strips, whereby a devious path is presented for the passage of fluid between the packing members. Devious paths are also afforded It will also be noted that the conical strips are inclined at an angle by the constructions shown in Figs. 12 and 13 wherein the constricted passages formed between consecutive pairs of strips are relatlvly staggered.
Figs. 14-17 show by way of example, and
, With the constructions shown in Figs. 16'
and 17 constrictions g, '72. are formed between the edges of the end portions of the strips and it will be apparent that with these constructions also upon the occurrence of rubbing contact between the strips, both strips will tend to move or deflect so as to lessen the contact pressure or eventually to re-open the passage therebetween.
Fig. 17 also shows a feature which may, if desired be applied to certain ofthe constructions above described, namely, that the strips of the member 16 are arranged with a greater conical angle than those of the member 17.
This afi'ords convenience in manufacture as it enables the width of the grooves between the stri s to be made equal on both sets of strips, or example in constructions such as that shown in Fig. 12. M g
In all the forms of packing according to the invention the axial width of the constrictions may be adjusted, for example, when assembling the packing, by axial movement of the packing members. The packing is particularly suitable for use in high pressure turbines to seal the interior of a turbine cylinder from communication with the external atmosphere or for balance pistons or as diaphragm packing between pressure stages of the turbine or elsewhere as may be desired. The packing members may be formed integrally with the relatively rotatable membersby which they are carried, or may be separately formed and secured in position in any convenient manner.
A constructional example showing the application of the packing to a turbine diaphragm is illustrated in Fig. 18. The packing rings are made up of arcuate packing members 18 having a plurality of strips 19, said members 18 being secured in grooves 20 formed in the rotor and held in position by means of caulking strips 21. The strips 22 of the packing carried by the diaphragm 23 are secured to the cylinder 24: through the intermediary of nozzle or blading portions 25 riveted or otherwise secured to the diaphragm 23 and held by caulking members 26 in a slot 27 formed inside the cylinder 24. The portions 25 are spigoted and grooved at 28, 29 to engage corresponding parts of slot 27 thereby preventing any possibility of the diaphragm closing in .and altering the position of the nozzle passages or the gland members. The axial width of the constrictions 30 will be adjusted to the desired dimensions when assembling the turbine, and
will thereafter be more or less self adjusting in accordance with the principles set forth above.
While I have shown my invention in several forms it will be obvious to those skilled in the art that it is not so limited, but is susceptible of various other changes and modifications, without departing from the spirit thereof, and I desire, therefore, that only such limitations shall be placed thereupon as are imposed-by the priorart or as are spe cificall'y set forth in the appended claims.
What I claim is: 1 1 A labyrinth packing for sealing the space between two relatively rotatable members comprising a plurality of annular conicalpacking elements disposed in telescopic rotatable members comprising .a plurality of annular conical packing strips disposed in telescopic relation and secured at their mner edges to one of said members, a plurality of other conical packing strips disposed in telescopic relation and secured at their inner edges to theother of said members, the free edges of the strips secured to one member opposing the free edges of the strips secured to the other member with axial packing clearances therebetween.
3. A labyrinth packing for sealing the space between two relatively rotatable members comprising a plurality of annular conical packing elements disposed in telescopic relation and secured at their inner edges to one of said members, the outer free edges of said elements beingv disposed in closelyspaced axially-opposed relation to parts of the other member so as to provide axial packing clearances therewith, said conical packing elements being inclined at an angle from 30 to 60 to the axis of rotation.
4. An axial'clearance labyrinth packing for sealingthe space between two relatively rotatable members comprising a plurality of annular conical packing strips disposed in telescopic relation and secured at their inner edges to one of said members, a plurality of other conicalpacking strips disposed in telescopic relation and secured at their inner edges to the other of said members, the free edges of the strips secured to one member opposing the free edges of the strips secured to the other member in end to end relation with axial packing clearances therebetween, said conical packing strips being inclined at an angle from 30 to 60 to the axis of rotation.
5. An axial clearance labyrinth packing for sealing the space between two relatively rotatable members comprising a plurality of annular conical packing strips disposed in telescopic relation and secured at their inner ends to one of said members, a plurality of other conical packing strips also disposed in telescopic relation and secured at their inner strips secured to the other member with axial. packing clearances therebetweem said end surfaces being dispbsed out of alignment so that the packing clearances are not in alignment and thereby provide a devious path for the passage of fluid between the packing members. I
In testimony whereof, I have hereunto subscribed my name this fifth day of October,
' KARL BAUlVIANN.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1831224X | 1927-11-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
US1831224A true US1831224A (en) | 1931-11-10 |
Family
ID=10891566
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US315302A Expired - Lifetime US1831224A (en) | 1927-11-07 | 1928-10-26 | Labyrinth packing |
Country Status (1)
Country | Link |
---|---|
US (1) | US1831224A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2587077A (en) * | 1948-06-25 | 1952-02-26 | Martin P Winther | Labyrinth seal |
US2856208A (en) * | 1956-02-23 | 1958-10-14 | Gen Motors Corp | Closure |
US3690785A (en) * | 1970-12-17 | 1972-09-12 | Westinghouse Electric Corp | Spring plate sealing system |
US5037114A (en) * | 1990-01-26 | 1991-08-06 | Westinghouse Electric Corp. | Labyrinth seal for steam turbines |
US5639095A (en) * | 1988-01-04 | 1997-06-17 | Twentieth Technology | Low-leakage and low-instability labyrinth seal |
US20050194747A1 (en) * | 2004-01-28 | 2005-09-08 | Rolls-Royce Plc | Sealing arrangement |
US20070063449A1 (en) * | 2005-09-19 | 2007-03-22 | Ingersoll-Rand Company | Stationary seal ring for a centrifugal compressor |
US20070065276A1 (en) * | 2005-09-19 | 2007-03-22 | Ingersoll-Rand Company | Impeller for a centrifugal compressor |
US20110091315A1 (en) * | 2009-10-15 | 2011-04-21 | Asia Vital Components Co., Ltd. | Fan with pressurizing structure |
US8016553B1 (en) * | 2007-12-12 | 2011-09-13 | Florida Turbine Technologies, Inc. | Turbine vane with rim cavity seal |
US20130058766A1 (en) * | 2011-09-06 | 2013-03-07 | General Electric Company | Systems, Methods, and Apparatus for a Labyrinth Seal |
US20130071242A1 (en) * | 2011-09-16 | 2013-03-21 | Joseph T. Caprario | Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
EP3354858A1 (en) * | 2017-01-26 | 2018-08-01 | United Technologies Corporation | Gas turbine seal |
US20180355743A1 (en) * | 2015-12-09 | 2018-12-13 | Mitsubishi Hitachi Power Systems, Ltd. | Seal fin, seal structure, turbo machine, and method for manufacturing seal fin |
-
1928
- 1928-10-26 US US315302A patent/US1831224A/en not_active Expired - Lifetime
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2587077A (en) * | 1948-06-25 | 1952-02-26 | Martin P Winther | Labyrinth seal |
US2856208A (en) * | 1956-02-23 | 1958-10-14 | Gen Motors Corp | Closure |
US3690785A (en) * | 1970-12-17 | 1972-09-12 | Westinghouse Electric Corp | Spring plate sealing system |
US5639095A (en) * | 1988-01-04 | 1997-06-17 | Twentieth Technology | Low-leakage and low-instability labyrinth seal |
US5037114A (en) * | 1990-01-26 | 1991-08-06 | Westinghouse Electric Corp. | Labyrinth seal for steam turbines |
US20050194747A1 (en) * | 2004-01-28 | 2005-09-08 | Rolls-Royce Plc | Sealing arrangement |
US20070063449A1 (en) * | 2005-09-19 | 2007-03-22 | Ingersoll-Rand Company | Stationary seal ring for a centrifugal compressor |
US20070065276A1 (en) * | 2005-09-19 | 2007-03-22 | Ingersoll-Rand Company | Impeller for a centrifugal compressor |
US8016553B1 (en) * | 2007-12-12 | 2011-09-13 | Florida Turbine Technologies, Inc. | Turbine vane with rim cavity seal |
US8353671B2 (en) * | 2009-10-15 | 2013-01-15 | Asia Vital Components Co., Ltd. | Fan with pressurizing structure |
US20110091315A1 (en) * | 2009-10-15 | 2011-04-21 | Asia Vital Components Co., Ltd. | Fan with pressurizing structure |
US20130058766A1 (en) * | 2011-09-06 | 2013-03-07 | General Electric Company | Systems, Methods, and Apparatus for a Labyrinth Seal |
US8932001B2 (en) * | 2011-09-06 | 2015-01-13 | General Electric Company | Systems, methods, and apparatus for a labyrinth seal |
US20130071242A1 (en) * | 2011-09-16 | 2013-03-21 | Joseph T. Caprario | Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
US10119476B2 (en) * | 2011-09-16 | 2018-11-06 | United Technologies Corporation | Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
US10815903B2 (en) | 2011-09-16 | 2020-10-27 | Raytheon Technologies Corporation | Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
US20180355743A1 (en) * | 2015-12-09 | 2018-12-13 | Mitsubishi Hitachi Power Systems, Ltd. | Seal fin, seal structure, turbo machine, and method for manufacturing seal fin |
US11105213B2 (en) * | 2015-12-09 | 2021-08-31 | Mitsubishi Power, Ltd. | Seal fin, seal structure, turbo machine, and method for manufacturing seal fin |
EP3354858A1 (en) * | 2017-01-26 | 2018-08-01 | United Technologies Corporation | Gas turbine seal |
US10408077B2 (en) | 2017-01-26 | 2019-09-10 | United Tehnologies Corporation | Gas turbine seal |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1831224A (en) | Labyrinth packing | |
US4017088A (en) | Shaft seal for turbomachines | |
US3752598A (en) | Segmented duct seal | |
US3038698A (en) | Mechanism for controlling gaseous flow in turbo-machinery | |
US1708044A (en) | Labyrinth-gland packing | |
US8052380B2 (en) | Thermally-activated clearance reduction for a steam turbine | |
US3542483A (en) | Turbine stator structure | |
US3519366A (en) | Turbine diaphragm seal structure | |
US1689735A (en) | Labyrinth gland construction | |
US2649315A (en) | High-temperature expansion joint | |
CN103827558A (en) | Labyrinth seal | |
US1831242A (en) | Labyrinth packing | |
US20140346741A1 (en) | Stationary part sealing structure | |
US2801792A (en) | Cooling of machine structures | |
US20140361499A1 (en) | Shape memory alloy intersegment seals | |
US1626237A (en) | Turbine gland | |
US1419927A (en) | Packing | |
JP2017036799A (en) | Shaft seal device | |
US1680737A (en) | Elastic-fluid turbine | |
JPS63235771A (en) | Labyrinth seal | |
JP3662198B2 (en) | Non-stretchable split packing ring for fluid turbines with special springs to reduce forces during shaft friction | |
US1585670A (en) | Elastic-fluid turbine | |
US3042367A (en) | Fluid seal | |
US20050116425A1 (en) | Finned seals for turbomachinery | |
US2001492A (en) | Method of assembling packing rings in turbine rotors |