SE458295B - COMBINED SEALING AND INNER COATING FOR THE INNER END OF A LINE OF COMPRESSOR LEADERS WITH A ROTATING MACHINE - Google Patents
COMBINED SEALING AND INNER COATING FOR THE INNER END OF A LINE OF COMPRESSOR LEADERS WITH A ROTATING MACHINEInfo
- Publication number
- SE458295B SE458295B SE8207315A SE8207315A SE458295B SE 458295 B SE458295 B SE 458295B SE 8207315 A SE8207315 A SE 8207315A SE 8207315 A SE8207315 A SE 8207315A SE 458295 B SE458295 B SE 458295B
- Authority
- SE
- Sweden
- Prior art keywords
- vane
- jacket ring
- compressor
- sealing
- tongue
- Prior art date
Links
- 238000007789 sealing Methods 0.000 title claims description 8
- 239000011248 coating agent Substances 0.000 title 1
- 238000000576 coating method Methods 0.000 title 1
- 239000000463 material Substances 0.000 claims description 9
- 239000003566 sealing material Substances 0.000 claims description 6
- 229920000728 polyester Polymers 0.000 claims description 3
- 229910018487 Ni—Cr Inorganic materials 0.000 claims description 2
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 claims description 2
- 238000005219 brazing Methods 0.000 claims 2
- 210000002105 tongue Anatomy 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 239000003082 abrasive agent Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910000907 nickel aluminide Inorganic materials 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Sealing Devices (AREA)
Description
458 295 10 15 20 25 30 35 2 statorskovlar 10, av vilka endast en visas, men sträcker sig inåt från höljet eller yttermanteln och är anordnade mellan bladraderna. Skovlarnas ytterändar kan vara hårdlödda vid yttermanteln för säker infästning i denna. 458 295 10 15 20 25 30 35 2 stator vanes 10, of which only one is shown, but extends inwards from the housing or the outer casing and is arranged between the rows of blades. The outer ends of the vanes can be brazed to the outer jacket for secure attachment to it.
Inneränden av varje skovel har en tunga 12, som sträcker sig inåt genom en öppning ll: i innermanteln 16. Dessa tungor är företrädesvis hârdlödda vid innermanteln. Innermanteln är anordnad i form av ett trág med sidoväggar 18 eller flänsar som sträcker sig inåt från konstruktionen såsom visas. Det inåtriktade tråget är fyllt med något nötningsbart tätningsmaterial, som kan vara något godtyckligt av olika material, såsom gummi, nickelaluminidpolyester, nickelgrafit eller nickelkrompolyester och som oberoende av det använda materialet kan sprutas in i tråget till önskat djup. Detta arrangemang medger rutinmässigt ett större djup av tätnlngsmaterial än i den sedvanliga konstruk- tionen, och fenorna på rotorn bildar lämpliga tätningsspår i det nötningsbara materialet när motorn arbetar.The inner end of each vane has a tongue 12 which extends inwardly through an opening 11 in the inner jacket 16. These tongues are preferably brazed to the inner jacket. The inner jacket is arranged in the form of a trough with side walls 18 or fl extending inwards from the construction as shown. The inwardly facing trough is filled with any abrasive sealing material, which may be any of a variety of materials, such as rubber, nickel aluminide polyester, nickel graphite or nickel chromium polyester and which, independently of the material used, may be injected into the trough to the desired depth. This arrangement routinely allows a greater depth of sealing material than in the conventional construction, and the fins on the rotor form suitable sealing grooves in the wearable material when the engine is operating.
Eftersom tätningsringen eller tråget bildar en integrerad del av inner- manteln, är det uppenbart att tätningsmaterialet .i tråget väsentligen kan ha mantelns diameter och således tillåter tätningen att befinna sig närmare gasbanan och orsaka minsta möjliga störning av kompressorns gasbaneflöde.Since the sealing ring or trough forms an integral part of the inner jacket, it is obvious that the sealing material in the trough can have substantially the diameter of the jacket and thus allow the seal to be closer to the gas path and cause the least possible disturbance of the compressor gas path flow.
Bladen har innermantlar väsentligen anordnade i linje med innermantlarna för att avgränsa innerväggen för gasbanan genom kompressorn.The blades have inner sheaths substantially arranged in line with the inner sheaths to define the inner wall of the gas path through the compressor.
Viktminskningen är också betydande, eftersom tätningen och manteln utgör en enda enkel ringkonstruktion.The weight loss is also significant, as the seal and jacket form a single simple ring construction.
Uppenbarligen resulterar minskningen av delar och vikt i en betydande kostnadsreduktion.Obviously, the reduction in parts and weight results in a significant cost reduction.
Underhållskostnaderna blir betydligt lägre, eftersom det nötningsbara materialet vid behov kan ersättas vid en reparationsanläggning och materialet lätt kan avlägsnas, om så önskas, genom sandblästring. Detta är särskilt önskvärt, när tillträde till någon tunga krävs såsom för skovelbyte. Det nötningsbara materialet kan sandblästras bort på den utvalda ytan intill tungan. Trågets eller rännans djup och bredd kan varieras efter önskemål och mycket effektiv tätning blir följden genom att tätningsfenorna tillåts nöta bort en del av materialet och därigenom bilda spår i tätningsmaterialet som tätt passar till tätningsfenorna. Även om uppfinningen visats och beskrivits med avseende på en före- dragen utföringsforrn är det självklart för fackmannen på området att andra olika förändringar och utelämnanden vad gäller dess utformning och detaljer kan göras utan att man avviker från uppfinningens omfattning.Maintenance costs will be significantly lower, as the abrasive material can be replaced at a repair facility if needed and the material can be easily removed, if desired, by sandblasting. This is especially desirable when access to any tongue is required such as for blade replacement. The abrasive material can be sandblasted away on the selected surface next to the tongue. The depth and width of the trough or gutter can be varied as desired and very effective sealing is the result of allowing the sealing fins to wear away a part of the material and thereby form grooves in the sealing material which fit snugly to the sealing fins. Although the invention has been shown and described with respect to a preferred embodiment, it is obvious to those skilled in the art that other various changes and omissions as to its design and details may be made without departing from the scope of the invention.
Claims (3)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US33460781A | 1981-12-28 | 1981-12-28 |
Publications (3)
Publication Number | Publication Date |
---|---|
SE8207315D0 SE8207315D0 (en) | 1982-12-21 |
SE8207315L SE8207315L (en) | 1983-06-29 |
SE458295B true SE458295B (en) | 1989-03-13 |
Family
ID=23307975
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8207315A SE458295B (en) | 1981-12-28 | 1982-12-21 | COMBINED SEALING AND INNER COATING FOR THE INNER END OF A LINE OF COMPRESSOR LEADERS WITH A ROTATING MACHINE |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS58119996A (en) |
DE (1) | DE3244874A1 (en) |
FR (1) | FR2519096B1 (en) |
GB (1) | GB2112878B (en) |
IT (1) | IT1195967B (en) |
SE (1) | SE458295B (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2553822B1 (en) * | 1983-10-24 | 1987-12-31 | Snecma | DEVICE FOR FIXING BLADES OF TURBINE DISTRIBUTOR |
US6533285B2 (en) * | 2001-02-05 | 2003-03-18 | Caterpillar Inc | Abradable coating and method of production |
US7604455B2 (en) | 2006-08-15 | 2009-10-20 | Siemens Energy, Inc. | Rotor disc assembly with abrasive insert |
DE102010055435B4 (en) | 2010-12-21 | 2018-03-29 | Rolls-Royce Deutschland Ltd & Co Kg | Innendeckband a gas turbine and method for producing a Innenendeckbandes |
DE102013212465B4 (en) * | 2013-06-27 | 2015-03-12 | MTU Aero Engines AG | Sealing arrangement for a turbomachine, a vane assembly and a turbomachine with such a sealing arrangement |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR998220A (en) * | 1949-10-26 | 1952-01-16 | Soc D Const Et D Equipements M | Advanced training in the assembly and fixing of fixed blades for turbomachines |
GB791568A (en) * | 1956-03-26 | 1958-03-05 | Gen Motors Corp | Improvements in axial flow compressors |
GB780137A (en) * | 1955-07-07 | 1957-07-31 | Gen Motors Corp | Improvements relating to axial-flow compressors |
CH489699A (en) * | 1968-03-22 | 1970-04-30 | Sulzer Ag | Guide vane ring for turbo machines |
US3849023A (en) * | 1973-06-28 | 1974-11-19 | Gen Electric | Stator assembly |
FR2404102A1 (en) * | 1977-09-27 | 1979-04-20 | Snecma | Labyrinth seal for fixed blades of jet engine compressor - has abradable resin surface in contact with ridges of rotor seal |
JPS5550393U (en) * | 1978-09-29 | 1980-04-02 | ||
FR2452590A1 (en) * | 1979-03-27 | 1980-10-24 | Snecma | REMOVABLE SEAL FOR TURBOMACHINE DISPENSER SEGMENT |
-
1982
- 1982-12-01 GB GB08234183A patent/GB2112878B/en not_active Expired
- 1982-12-03 DE DE19823244874 patent/DE3244874A1/en active Granted
- 1982-12-21 SE SE8207315A patent/SE458295B/en not_active IP Right Cessation
- 1982-12-23 IT IT24934/82A patent/IT1195967B/en active
- 1982-12-24 FR FR8221749A patent/FR2519096B1/en not_active Expired
- 1982-12-27 JP JP57234996A patent/JPS58119996A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS58119996A (en) | 1983-07-16 |
FR2519096A1 (en) | 1983-07-01 |
FR2519096B1 (en) | 1988-07-15 |
SE8207315L (en) | 1983-06-29 |
SE8207315D0 (en) | 1982-12-21 |
JPH0319398B2 (en) | 1991-03-14 |
IT1195967B (en) | 1988-11-03 |
GB2112878B (en) | 1985-12-04 |
DE3244874C2 (en) | 1991-03-07 |
IT8224934A0 (en) | 1982-12-23 |
GB2112878A (en) | 1983-07-27 |
DE3244874A1 (en) | 1983-07-07 |
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