DE858334C - Device for cooling an internally cooled, hollow rotor blade for gas turbines - Google Patents

Device for cooling an internally cooled, hollow rotor blade for gas turbines

Info

Publication number
DE858334C
DE858334C DED5230D DED0005230D DE858334C DE 858334 C DE858334 C DE 858334C DE D5230 D DED5230 D DE D5230D DE D0005230 D DED0005230 D DE D0005230D DE 858334 C DE858334 C DE 858334C
Authority
DE
Germany
Prior art keywords
cooling
gas turbines
rotor blade
hollow rotor
internally cooled
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
Application number
DED5230D
Other languages
German (de)
Inventor
Fritz A F Dr-Ing Habil Schmidt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deutsche Versuchsanstalt fuer Luftfahrt eV
Original Assignee
Deutsche Versuchsanstalt fuer Luftfahrt eV
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 Deutsche Versuchsanstalt fuer Luftfahrt eV filed Critical Deutsche Versuchsanstalt fuer Luftfahrt eV
Priority to DED5230D priority Critical patent/DE858334C/en
Application granted granted Critical
Publication of DE858334C publication Critical patent/DE858334C/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/085Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • F01D5/087Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor in the radial passages of the rotor disc
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/60Fluid transfer
    • F05D2260/601Fluid transfer using an ejector or a jet pump

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

Die Verarbeitung hoher Gastemperaturen in Ab- gas- oder Frischgasturbinen ist durch die Warm- festigkeit des für die Schaufeln verwendeten Bau- stoffes begrenzt. Um höhere Gastempcratureri verarbeiten zu können., sind Kühlverfahren für die Schaufeln entwickelt worden, von denen die Hohl- schaufel, die von Kühlluft durchströmt wird, be- sonders günstige Voraussetzungen bietet. Durch zweckmäßige Gestaltung der Kühlluftkanäle und durch Ausnutzung der Förderwirkung eitles im Innern des Turbinenrades angeordneten Förder- sternes für die Kühlluft ist es gelungen, die für einen bestimmten Schaufelbaustoff höchstzulässige Gas- temperatur wesentlich zu steigern. Die Absenkung der Schaufeltemperatur ist durch die Kühlluftmenge, die man durch die Schaufeln hindurchschicken kann, ferner durch die Luftge- schwindigkeit in den Kühlluftkanälen der Schaufel begrenzt. 7ur Erhöhung des #\7ärmeüliergangcs in (ieri Kühlluftkanälen .müssen diese möglichst eng ausgebildet werden, um eine möglichst große Ge- schwindigkeit zu erhalten. Damit ist aber auch ein Druckgefälle längs der Schaufel erforderlich, (las durch die Schleuderwirkung im Innein des hZades begrenzt ist, wenn man nicht vor-#-erdiclitete Luft in den Läufer einführen will. Schließlich ist der `Värnieübcrgang in den Kiililluftkanälen noch von der Dichte der Kühlluft abhängig. Da die erreich- bare Turbinenleistung im wesentlichen von der Temperatur der Gase am Turbineneintritt abhängt, ist es erwünscht, die Temperatur so hoch wie mög- lich zii steigern. Eine Möglichkeit hierfür bietet die weitere Absenkung der Schaufeltemperatur. Erfindungsgemäß soll dies dadurch geschehen, daß in die Kühlluft Wasser oder eine sonstige Kühl- flüssigkeit eingespritzt oder geträufelt wird. Infolge hoher Verdampfungswärme kann lici nur geringen Mengen der Kühlflüssigkeit eine erhebliche Wärme- menge aufgenommen werden. Die Aufnahme der Wärmemenge kann einmal aus der Kühlluft er- folgen, deren Temperatur damit herabgesetzt wird und die damit ihrerseits wieder- N-otl der Schaufel her eine größere Wärmemenge aufnehnicn kann, dann aber auch durch den unmittelbaren Wärme- übergang von der Schaufel an @assertrölifclien, die gegen die Schaufehvand gespritzt -,worden sind, wo- bei der Wärmeübergang an der Schaufel ganz erlicb- lich größer als bei Verwendung reiner Luft ist. Die "Zuführung des Wassers in dun Luftstrom kann auf verschiedene Weise entwe,lcr in der Niilie des Luft- eintritts in den Läufer o der weitci- aul:ierlialli zu den Schaufeln hin erfolgen. 1,.iienso können innerhalb des Laufrades unter Ausnutzung der Schleuder- wirkung des umlaufenden l@a(les die verschiedensten Verteilungs- oder Zerstäubungsvorrichtungen ange- ordnet werden, um eine Verteilung der 1Vassci-s in der ge@vünscliten Weise voi-nelinien zu können. Die Abb. i und 2 zeigen _ltisfiilirungsl)eispiele des Erfindungsgegenstandes. Dci- Gasturbine a wird z. 13. durch die hohle `4'ellc bi Wasser, z. 13. 201/1i, zugeführt, das sich mit der Luft, die bei c einströmt, mischt und durch die Hohlschaufel (1 abgeführt wird. Es kann auch an Stelle der 1)iise e eine Schutz- kante f vorgesehen sein, die die gleiche Wirkung erreicht, und das Wasser durch die Nahe b_ der Turbine zugeführt wer(len. The processing of high gas temperatures in gas or fresh gas turbines is due to the hot strength of the structural material used for the blades substance limited. To higher gas temperatures to be able to process., are cooling methods for the Blades have been developed, of which the hollow the blade through which cooling air flows. offers particularly favorable conditions. By appropriate design of the cooling air ducts and by exploiting the promotional effect of vain im Inside the turbine wheel arranged conveyor sternes for the cooling air has succeeded that for one certain blade building material, the maximum permissible gas to increase temperature significantly. The lowering of the blade temperature is through the amount of cooling air that goes through the blades can send through, also through the air speed in the cooling air ducts of the blade limited. To increase the # \ 7arming gangc in (ieri cooling air ducts. must be as narrow as possible be trained to achieve the largest possible to maintain speed. But that is also a Pressure gradient required along the blade, (read by the centrifugal effect inside the hZades is limited if one does not have - # - earthed air in wants to introduce the runner. After all, that is `Värnie transition in the Kill air canals still from depending on the density of the cooling air. Since the achievable actual turbine power essentially depends on the Depends on the temperature of the gases at the turbine inlet, it is desirable to keep the temperature as high as possible Lich increase zii. One possibility for this is offered by the further lowering of the blade temperature. According to the invention, this should be done in that in the cooling air water or some other cooling liquid is injected or dripped. As a result high heat of vaporization can only be achieved by lici Quantities of the coolant cause considerable heat amount to be absorbed. The inclusion of the The amount of heat can be extracted from the cooling air once follow, the temperature of which is thus reduced and those in turn- N-otl the shovel can absorb a larger amount of heat, but then also through the direct heat transition from the shovel to @assertrölifclien, the sprayed against the wall of the shop -, where- with the heat transfer at the shovel completely Lich is larger than when using pure air. the "Feeding the water in dun airflow can be on different ways either in the air line Entrance to the runner o der weitci- aul: ierlialli to the Shovels done. 1, .iienso can within of the impeller using the centrifugal effect of the circumferential l @ a (les the most diverse Distribution or atomizing devices. be assigned to a distribution of the 1Vassci-s in the greenest way to be able to draw lines. Figs. 1 and 2 show examples of the illustration Subject of the invention. Dci gas turbine a will z. 13. through the hollow `4'ellc bi water, e.g. 13. 201 / 1i, supplied, which is mixed with the air flowing in at c, mixes and is discharged through the hollow shovel (1. Instead of the 1) iise e, a protective Edge f can be provided which has the same effect reached, and the water through the Nahe b_ der Turbine who are fed (len.

Claims (1)

PATENT ANS I'LCCHE:
r. Einrichtung zur Kühlung einer innen- gekühlten, hohlen Laufscli@itifel für Gasturbinen, dadurch gekennzeichnet, (lall) in den zur Küh- lung verwendeten Luftstrom Wasser oder eine sonstige Kühlflüssigkeit eingesp ritzt oller ge- träufelt wird. 2. Einrichtung nach Anspruch i, dadurch ge- kennzeichnet, daß Teile des Laufrades mit zur Zerstäubung benutzt werden. 3. Einrichtung nach Anspruch i, dadurch ge- kennzeichnet, daß ini Innci-n des Laufrades ein Spritzring vorgesehen ist, an den das kühlende Wasser hingeleitet wird.
PATENT ANS I'LCCHE:
r. Device for cooling an indoor cooled, hollow Laufscli @ itifel for gas turbines, characterized in that (lall) in the treatment used air flow water or a other coolant injected oller is trickling. 2. Device according to claim i, characterized in that indicates that parts of the impeller with for Atomization can be used. 3. Device according to claim i, characterized in that indicates that ini innci-n of the impeller a Splash ring is provided to which the cooling Water is directed.
DED5230D 1940-09-29 1940-09-29 Device for cooling an internally cooled, hollow rotor blade for gas turbines Expired DE858334C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DED5230D DE858334C (en) 1940-09-29 1940-09-29 Device for cooling an internally cooled, hollow rotor blade for gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DED5230D DE858334C (en) 1940-09-29 1940-09-29 Device for cooling an internally cooled, hollow rotor blade for gas turbines

Publications (1)

Publication Number Publication Date
DE858334C true DE858334C (en) 1952-12-04

Family

ID=7031322

Family Applications (1)

Application Number Title Priority Date Filing Date
DED5230D Expired DE858334C (en) 1940-09-29 1940-09-29 Device for cooling an internally cooled, hollow rotor blade for gas turbines

Country Status (1)

Country Link
DE (1) DE858334C (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2988325A (en) * 1957-07-18 1961-06-13 Rolls Royce Rotary fluid machine with means supplying fluid to rotor blade passages
DE1110469B (en) * 1956-03-28 1961-07-06 Robert Pouit Gas turbine with reaction blades
FR2410729A1 (en) * 1977-12-02 1979-06-29 Hitachi Ltd METHOD AND APPARATUS FOR COOLING A GAS TURBINE BLADE

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1110469B (en) * 1956-03-28 1961-07-06 Robert Pouit Gas turbine with reaction blades
US2988325A (en) * 1957-07-18 1961-06-13 Rolls Royce Rotary fluid machine with means supplying fluid to rotor blade passages
FR2410729A1 (en) * 1977-12-02 1979-06-29 Hitachi Ltd METHOD AND APPARATUS FOR COOLING A GAS TURBINE BLADE

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