DE834408C - Prestressed axial blade root attachment for steam and gas turbines - Google Patents

Prestressed axial blade root attachment for steam and gas turbines

Info

Publication number
DE834408C
DE834408C DEM7614A DEM0007614A DE834408C DE 834408 C DE834408 C DE 834408C DE M7614 A DEM7614 A DE M7614A DE M0007614 A DEM0007614 A DE M0007614A DE 834408 C DE834408 C DE 834408C
Authority
DE
Germany
Prior art keywords
blade root
steam
gas turbines
axial blade
root attachment
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
DEM7614A
Other languages
German (de)
Inventor
Dipl-Ing Georg Achatz
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.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
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 MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Priority to DEM7614A priority Critical patent/DE834408C/en
Application granted granted Critical
Publication of DE834408C publication Critical patent/DE834408C/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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32Locking, e.g. by final locking blades or keys
    • F01D5/323Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor

Landscapes

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

Description

Die bekannte formschlüssige Schaufelfußbefestigung nach Laval stellt keine absolut starre form- und kraftschlüssige Verbindung zwischen Schaufelfuß und Laufradkörper dar. Infolge thermischer und mechanischer Verformungen im Betrieb kann ein Lösen dieser Verbindung eintreten auch dann, wenn bei der Montage eine gewisse Kraftschlüssigkeit durch strammes Einpassen der Schaufeln erreicht wurde. Es ändert sich damit auch die der Schwingungsrechnung zugrunde liegende freie Schaufellänge i, und somit auch die errechnete Schwingungszahl der Schaufel bzw. des Schaufelpaketes.The well-known form-fitting blade root fastening according to Laval provides no absolutely rigid positive and non-positive connection between the blade root and Impeller body. As a result of thermal and mechanical deformations during operation A loosening of this connection can occur even if a certain frictional locking was achieved by tight fitting of the blades. This also changes the free blade length on which the vibration calculation is based i, and thus also the calculated number of vibrations of the blade or the blade pack.

Auch die bekannten Spannungsverbindungen für radialen Einbau, die durch Beilagen und Keile unter den Schaufelfuß bewirkt werden, ergeben, abgesehen von der Schwierigkeit der Ausführung, keine genügend große Vorverspannung zwischen Schaufel und Laufradkörper und damit keine ausreichende Betriebssicherheit.Also the known voltage connections for radial installation, the caused by shims and wedges under the blade root, apart from that from the difficulty of execution, no sufficiently large pre-tensioning between Blade and impeller body and therefore insufficient operational reliability.

Um diese Unsicherheit in der Verbindung des Schaufelfußes mit dem Laufradkörper zu beseitigen, wird nach der Erfindung eine auch im Betrieb absolut starre, vorverspannte, also kraftschlüssige Schaufelfußbefestigung für Dampf- und Gasturbinen dadurch geschaffen, daß die Vorspannung des zweckmäßig trapezförmigen Schaufelfußes durch einen unter diesen geschobenen Keil, vorzugsweise einen Doppelkeil, erzeugt wird, wobei die Vorspannung größer als die Betriebsspannung ist. Hierdurch wird eine form- und kraftschlüssige Schaufelfußbefestigung erreicht, die auch höchsten Anforderungen gerecht wird. Der Keil bzw. Doppelkeil verspannt den trapezförmig ausgebildeten Schaufelfuß gegenüber dem Laufradkörper so, daß Formänderungen im Betrieb keinerlei Einfluß auf die Verbindung haben können.To this uncertainty in the connection of the blade root with the To eliminate the impeller body, according to the invention, an absolute also in operation rigid, pre-tensioned, i.e. force-fit blade root attachment for steam and Gas turbines created in that the bias of the appropriately trapezoidal Blade root by a wedge pushed under it, preferably a double wedge, is generated, the bias voltage being greater than the operating voltage. Through this a form-fitting and force-fitting blade root fastening is achieved, which is also the highest Requirements. The wedge or double wedge braces the trapezoidal shape trained blade root against the impeller body so that changes in shape in Operation cannot have any influence on the connection.

In der Zeichnung ist ein Ausfühningsbeispiel der Erfindung dargestellt. Es zeigt Fig. i eine Seitenansicht der Schaufelbefestigung und Fig. 2 eine Vorderansicht derselben.An exemplary embodiment of the invention is shown in the drawing. FIG. 1 shows a side view of the blade attachment and FIG. 2 shows a front view the same.

Die in den Laufradkörper i axial eingebrachte Schaufel 2 besitzt nach den Fig. i und 2 einen trapezförmigen Fuß 3 mit guten Abrundungen. Die Nut 4 im Laufradkörper ist dem Schaufelfuß angepaßt und unten abgerundet, wobei die Abrundung nicht unbedingt tangentialen Übergang haben muß. Ebenso kann das Nutende z. B. eine gerade Begrenzung aufweisen. In den Zwischenraum zwischen der flachen Unterseite des Schaufelfußes und dem Nutende sind zwei Keile mit entgegengesetzten Anzugsflächen 6 eingesetzt. Eine Madenschraube 7 sichert die Keile in ihrer Lage Die Neigung der Keile 5 muß so gewählt werden, daß die im Schaufelfuß erzeugte Vorspannung größer als die auftretende Betriebsspannung ist.The blade 2 axially introduced into the impeller body i has after FIGS. i and 2 show a trapezoidal base 3 with good roundings. The groove 4 in The impeller body is adapted to the blade root and rounded at the bottom, the rounding does not necessarily have to have a tangential transition. Likewise, the groove end z. Legs just have limitation. Into the space between the flat bottom the blade root and the groove end are two wedges with opposing tightening surfaces 6 used. A grub screw 7 secures the wedges in their position Wedges 5 must be chosen so that the preload generated in the blade root is greater than the operating voltage that occurs.

Claims (1)

PATENTANSPRUCH Vorverspannte axiale Schaufelfußbefestigung für Dampf- und Gasturbinen, dadurch gekennzeichnet, daß die Vorspannung des zweckmäßig trapezförmigen Schaufelfußes (3) durch einen unter diesen geschobenen Keil, vorzugsweise einen Doppelkeil (5), erzeugt wird, wobei die Vorspannung größer als die Betriebsspannung ist.PATENT CLAIM Pre-tensioned axial blade root attachment for steam and gas turbines, characterized in that the bias of the appropriately trapezoidal Blade root (3) by a wedge pushed under this, preferably one Double wedge (5) is generated, the preload being greater than the operating voltage is.
DEM7614A 1950-11-23 1950-11-23 Prestressed axial blade root attachment for steam and gas turbines Expired DE834408C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEM7614A DE834408C (en) 1950-11-23 1950-11-23 Prestressed axial blade root attachment for steam and gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEM7614A DE834408C (en) 1950-11-23 1950-11-23 Prestressed axial blade root attachment for steam and gas turbines

Publications (1)

Publication Number Publication Date
DE834408C true DE834408C (en) 1952-03-20

Family

ID=7293817

Family Applications (1)

Application Number Title Priority Date Filing Date
DEM7614A Expired DE834408C (en) 1950-11-23 1950-11-23 Prestressed axial blade root attachment for steam and gas turbines

Country Status (1)

Country Link
DE (1) DE834408C (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2843356A (en) * 1954-04-05 1958-07-15 Gen Electric Turbo-machine rotor assembly
US2930581A (en) * 1953-12-30 1960-03-29 Gen Electric Damping turbine buckets
US3076634A (en) * 1959-06-12 1963-02-05 Ass Elect Ind Locking means for compressor and turbine blades
US3216699A (en) * 1963-10-24 1965-11-09 Gen Electric Airfoil member assembly
US3378230A (en) * 1966-12-16 1968-04-16 Gen Electric Mounting of blades in turbomachine rotors
WO1995030070A1 (en) * 1994-04-29 1995-11-09 United Technologies Corporation Ramped dovetail rails for rotor blade assembly
EP1892380A1 (en) * 2006-08-25 2008-02-27 Siemens Aktiengesellschaft Turbine blade retention system
EP1905957A1 (en) * 2006-09-27 2008-04-02 Siemens Aktiengesellschaft Locking device of a turbine blade
EP2090750A1 (en) * 2008-02-14 2009-08-19 Siemens Aktiengesellschaft Turbomachine rotor, rotor blade for such a turbomachine rotor, supporting strip for such a rotor blade in the turbomachine rotor and corresponding assembling method
WO2018075217A1 (en) * 2016-10-17 2018-04-26 General Electric Company System for composite marine propellers

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE652188C (en) * 1937-10-27 Wilhelm Wenzel Dipl Ing Blade attachment for steam or gas turbines

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE652188C (en) * 1937-10-27 Wilhelm Wenzel Dipl Ing Blade attachment for steam or gas turbines

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930581A (en) * 1953-12-30 1960-03-29 Gen Electric Damping turbine buckets
US2843356A (en) * 1954-04-05 1958-07-15 Gen Electric Turbo-machine rotor assembly
US3076634A (en) * 1959-06-12 1963-02-05 Ass Elect Ind Locking means for compressor and turbine blades
US3216699A (en) * 1963-10-24 1965-11-09 Gen Electric Airfoil member assembly
US3378230A (en) * 1966-12-16 1968-04-16 Gen Electric Mounting of blades in turbomachine rotors
WO1995030070A1 (en) * 1994-04-29 1995-11-09 United Technologies Corporation Ramped dovetail rails for rotor blade assembly
US8192167B2 (en) 2006-08-25 2012-06-05 Siemens Aktiengesellschaft Blade fastening means of a turbine
WO2008022890A1 (en) * 2006-08-25 2008-02-28 Siemens Aktiengesellschaft Blade fastening means of a turbine
JP2010501765A (en) * 2006-08-25 2010-01-21 シーメンス アクチエンゲゼルシヤフト Turbine blade fixing device
EP1892380A1 (en) * 2006-08-25 2008-02-27 Siemens Aktiengesellschaft Turbine blade retention system
CN101506475B (en) * 2006-08-25 2013-01-23 西门子公司 Blade fastening means of a turbine
EP1905957A1 (en) * 2006-09-27 2008-04-02 Siemens Aktiengesellschaft Locking device of a turbine blade
WO2008037661A1 (en) * 2006-09-27 2008-04-03 Siemens Aktiengesellschaft Securing apparatus of a turbine blade
EP2090750A1 (en) * 2008-02-14 2009-08-19 Siemens Aktiengesellschaft Turbomachine rotor, rotor blade for such a turbomachine rotor, supporting strip for such a rotor blade in the turbomachine rotor and corresponding assembling method
US8512001B2 (en) 2008-02-14 2013-08-20 Siemens Aktiengesellschaft Turbomachine rotor comprising a pretensioning device for pretensioning a rotor blade
WO2018075217A1 (en) * 2016-10-17 2018-04-26 General Electric Company System for composite marine propellers

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