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 MACHINE

Info

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
Application number
SE8207315A
Other languages
Swedish (sv)
Other versions
SE8207315L (en
SE8207315D0 (en
Inventor
B J Johnson
Original Assignee
United Technologies Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of SE8207315D0 publication Critical patent/SE8207315D0/en
Publication of SE8207315L publication Critical patent/SE8207315L/en
Publication of SE458295B publication Critical patent/SE458295B/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • F04D29/161Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001Preventing 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)

10 15 20 458 295 3 PATENTKRAV10 15 20 458 295 3 PATENT REQUIREMENTS 1. Kombinerad tätnings- och innermantelring för de inre ändarna av en rad av kompressorledskovlar hos en rotationsmaskin, vilka sträcker sig inåt mot en rotationsaxel, varvid varje skovel (10) har en tunga (12) vid sin inre ände som anpassar skoveln (10) till att ingripa i en del av mantelringen (16), varvid nämnda del av mantelringen (16) har en inre yta och en rad av öppningar (14) som sträcker sig genom mantelringen (16) till den inre ytan, kännetecknad av ett hârdlödningsmaterial vid varje skovel (10) som sträcker sig mellan nämnda del av mantelringen och tungan (12) hos varje skovel (10) för att hårdlöda tungan (12) i öppningen (1 ll) och bilda en integrerad enhet mellan skoveln (10) och den del av mantelringen (16) som är fäst vid skoveln (10), och ett på den inre ytan av mantelringen (16) anordnat nötningsbart tätnings- material för tätande ingrepp med rotationsmaskinens rotor, vilket täcker hårdlödningsmaterialet och som är väsentligen vid samma diameter som skovlarnas (l 0) innerändar.Combined sealing and inner jacket ring for the inner ends of a row of compressor articulated vanes of a rotary machine, which extend inwardly towards a axis of rotation, each vane (10) having a tongue (12) at its inner end which adapts the vane (10) to engage a part of the jacket ring (16), said part of the jacket ring (16) having an inner surface and a row of openings (14) extending through the jacket ring (16) to the inner surface, characterized by a brazing material at each vane (10) extending between said part of the jacket ring and the tongue (12) of each vane (10) to braze the tongue (12) in the opening (11l) and form an integrated unit between the vane (10) and the part of the jacket ring (16) attached to the vane (10), and an abrasive sealing material arranged on the inner surface of the jacket ring (16) for sealing engagement with the rotor of the rotary machine, which covers the brazing material and which is substantially the same diameter as the vanes ( l 0) in down ends. 2. Anordning erdigt patentkravet l, k ä n n e t e c k n a d av att det nötningsbara materialet är ett sprutbart material.Device according to claim 1, characterized in that the abradable material is a sprayable material. 3. Anordning enligt patentkravet 1 eller 2, k ä n n e t e c k n a d av att det nötningsbara tätningsrnaterialet är nickel- krompolyester.Device according to claim 1 or 2, characterized in that the abrasive sealing material is nickel-chromium polyester.
SE8207315A 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 SE458295B (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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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