DE815971C - Steam or gas turbine blade with little radial clearance loss - Google Patents

Steam or gas turbine blade with little radial clearance loss

Info

Publication number
DE815971C
DE815971C DEL648A DEL0000648A DE815971C DE 815971 C DE815971 C DE 815971C DE L648 A DEL648 A DE L648A DE L0000648 A DEL0000648 A DE L0000648A DE 815971 C DE815971 C DE 815971C
Authority
DE
Germany
Prior art keywords
steam
gas turbine
turbine blade
radial clearance
little radial
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
DEL648A
Other languages
German (de)
Inventor
Franz Dipl-Ing Burghauser
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to DEL648A priority Critical patent/DE815971C/en
Application granted granted Critical
Publication of DE815971C publication Critical patent/DE815971C/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
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/20Specially-shaped blade tips to seal space between tips and stator

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

Der radiale Spaltverlust der Schaufeln bei Dampf-und Gasturbinen drückt besonders im Hochdruckteil den Wirkungsgrad wesentlich herab. Beträgt z. B. die radiale Spaltweite 2°/o von der ganzen Schaufellänge, so beträgt der Verlust nicht etwa 2°/0, sondern mindestens 6°/0, wie durch Versuche erwiesen ist, aber auch folgende Überlegung zeigt: Neben den 2°/0 Dampf, welche die Schaufel überhaupt nicht treffen, rutschen auch noch die dem Spalt nahe gelegenen Dampfstrahlen in den Spalt ab, ohne ihre Arbeit an die Schaufel abgegeben zu haben.The radial gap loss of the blades in steam and gas turbines is a problem especially in the high-pressure part significantly reduces the efficiency. Is z. B. the radial gap width 2% of the entire length of the blade, then the loss is not about 2 ° / 0, but at least 6 ° / 0, as has been proven by experiments, but also the following Consideration shows: In addition to the 2 ° / 0 steam, which do not hit the shovel at all, the steam jets close to the gap also slide into the gap without to have given their work to the shovel.

Wesentlich verringert wird der radiale Spaltverlust, wenn nach vorliegender Erfindung die Schaufeln in der Nähe des Spaltes etwas entgegen der Dampfrichtung gekrümmt werden, wie in der Zeichnung dargestellt ist.The radial gap loss is significantly reduced if it is present Invention of the blades in the vicinity of the gap slightly against the direction of the steam be curved as shown in the drawing.

Fig. r zeigt eine Lauf- oder Leitschaufel im Längsschnitt durch das Lauf- oder Leitrad; x ist die Schaufellänge, s ist der radiale Spalt, a ist die Dampfströmungsrichtung; Fig. 2 zeigt eine Ansicht auf die Schaufeln und die Richtung a des die Schaufeln treffenden Dampfstrahles; Fig. 3 zeigt einen Längsschnitt c-c durch die Schaufeln.Fig. R shows a rotor or guide vane in a longitudinal section through the Impeller or idler wheel; x is the blade length, s is the radial gap, a is the Steam flow direction; Fig. 2 shows a view of the blades and the direction a of the steam jet hitting the blades; Fig. 3 shows a longitudinal section c-c through the shovels.

Gemäß der Erfindung erhalten die Kanten k der Schaufeln am Spalt s eine Bördelung entgegen der Dampfströmung. Bei geeigneter Ausführung der Bördelung strömt nur eine dem Verhältnis s/z entsprechende Dampfmenge in den Spalt ab, während der übrige Strom seine Arbeit voll an die Schaufel abgibt. Auch hohle Schaufeln können in der beschriebenen Weise ausgeführt, werden.According to the invention, the edges k of the blades are given at the gap s a bead against the steam flow. With a suitable design of the flanging only an amount of steam corresponding to the ratio s / z flows into the gap while the rest of the current gives its work to the shovel. Also hollow blades can be carried out in the manner described.

Claims (1)

PATENTANSPRUCH: Dampf- oder Gasturbinenschaufel mit geringem radialen Spaltverlust, dadurch gekennzeichnet, daß die zugeschärfte Endkante (k) der Schaufel umgebördelt und der Dampfströmung (a) entgegengesetzt ist. PATENT CLAIM: Steam or gas turbine blade with little radial gap loss, characterized in that the sharpened end edge (k) of the blade is flanged and the steam flow (a) is opposite.
DEL648A 1949-12-22 1949-12-22 Steam or gas turbine blade with little radial clearance loss Expired DE815971C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEL648A DE815971C (en) 1949-12-22 1949-12-22 Steam or gas turbine blade with little radial clearance loss

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEL648A DE815971C (en) 1949-12-22 1949-12-22 Steam or gas turbine blade with little radial clearance loss

Publications (1)

Publication Number Publication Date
DE815971C true DE815971C (en) 1951-10-08

Family

ID=7254982

Family Applications (1)

Application Number Title Priority Date Filing Date
DEL648A Expired DE815971C (en) 1949-12-22 1949-12-22 Steam or gas turbine blade with little radial clearance loss

Country Status (1)

Country Link
DE (1) DE815971C (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2456865A1 (en) * 1979-05-12 1980-12-12 Papst Motoren Kg FAN ROTOR
EP1770244A1 (en) * 2005-09-30 2007-04-04 Snecma Compressor blade with chanferred tip
EP1953344A1 (en) 2007-02-05 2008-08-06 Siemens Aktiengesellschaft Turbine blade
US8092178B2 (en) 2008-11-28 2012-01-10 Pratt & Whitney Canada Corp. Turbine blade for a gas turbine engine
EP2778346A1 (en) * 2013-03-14 2014-09-17 Pratt & Whitney Canada Corp. Rotors for a gas turbine engine, corresponding gas turbine engine and method
US9175574B2 (en) 2009-12-16 2015-11-03 Siemens Aktiengesellschaft Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2456865A1 (en) * 1979-05-12 1980-12-12 Papst Motoren Kg FAN ROTOR
EP1770244A1 (en) * 2005-09-30 2007-04-04 Snecma Compressor blade with chanferred tip
FR2891594A1 (en) * 2005-09-30 2007-04-06 Snecma Sa AUBE COMPRESSOR WITH CHANFREINE TOP
EP1953344A1 (en) 2007-02-05 2008-08-06 Siemens Aktiengesellschaft Turbine blade
US8092178B2 (en) 2008-11-28 2012-01-10 Pratt & Whitney Canada Corp. Turbine blade for a gas turbine engine
US9175574B2 (en) 2009-12-16 2015-11-03 Siemens Aktiengesellschaft Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
EP2778346A1 (en) * 2013-03-14 2014-09-17 Pratt & Whitney Canada Corp. Rotors for a gas turbine engine, corresponding gas turbine engine and method
US10760499B2 (en) 2013-03-14 2020-09-01 Pratt & Whitney Canada Corp. Turbo-machinery rotors with rounded tip edge

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