EP1798375B1 - Profil d'aube pour aubes statoriques variables - Google Patents

Profil d'aube pour aubes statoriques variables Download PDF

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Publication number
EP1798375B1
EP1798375B1 EP06024318A EP06024318A EP1798375B1 EP 1798375 B1 EP1798375 B1 EP 1798375B1 EP 06024318 A EP06024318 A EP 06024318A EP 06024318 A EP06024318 A EP 06024318A EP 1798375 B1 EP1798375 B1 EP 1798375B1
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European Patent Office
Prior art keywords
zone
stator
profile
line
blade
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Not-in-force
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EP06024318A
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German (de)
English (en)
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EP1798375A3 (fr
EP1798375A2 (fr
Inventor
Volker Gümmer
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Rolls Royce Deutschland Ltd and Co KG
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Rolls Royce Deutschland Ltd and Co KG
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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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/56Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • 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
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • 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
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • F04D29/544Blade shapes
    • 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
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/301Cross-sectional characteristics
    • 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
    • F05D2250/00Geometry
    • 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
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/14Two-dimensional elliptical
    • 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
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • F05D2250/74Shape given by a set or table of xyz-coordinates
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/02Formulas of curves

Definitions

  • the present invention relates to variable stator blades of fluid flow machines such as fans, compressors, pumps, and fans in the axial, semi-axial, or even radial form.
  • the working medium can be gaseous or liquid.
  • the invention relates to at least one adjustable stator blade, possibly also an adjustable Vorleitrad, a fluid flow machine.
  • the blading in question is within a housing, which limits the flow of at least one rotor and a stator with a fluid to the outside.
  • a rotor comprises a plurality of rotor blades attached to a rotating shaft and supplies energy to the working fluid
  • a stator consists of a plurality of stator blades usually mounted in the housing.
  • the aerodynamic load capacity and the efficiency of fluid flow machines is limited in particular by the growth and separation of boundary layers in the region of the radial gap between the blading and the housing or hub, which is structurally necessary at the annular channel edge.
  • Rotary adjustable stators in particular, which are characterized by the necessary free cuts in front of and behind the rotary spindle, have a pronounced radial gap and cause considerable flow losses.
  • turntables as large as possible are usually provided at the inner and outer ends of the adjusting stators in order to keep the extent of the cutouts in the flow direction small.
  • the turntables are arranged so that they are located in the critically classified profile leading edge zone of the blade edge cuts.
  • the Fig. 1 Fig. 2 shows a schematic representation of two prior art blade configurations in the meridian plane given by the radial direction r and the axial direction x.
  • the presentation is limited to a mounted in hub as housing variable stator, a storage solely in housing or hub with a full radial gap at the other end of the blade but in some cases also occurs.
  • the blade On the left side of the picture, a conventional variable stator without variation of the skeleton line type is shown.
  • the blade consists of only one block (ZO) in which the type of skeleton line is given according to uniform rules.
  • ZO the type of skeleton line is given according to uniform rules.
  • This category includes the so-called CDA (controlled diffusion aerofoils) US4431376 , From an aerodynamic point of view, the CDA aims for a moderate profile frontload.
  • the present invention relates to stators, which are rotatably mounted on at least one blade end and can be adjusted via a spindle about a fixed axis of rotation. As in all representations shown here, the inflow of the relevant row of blades takes place, as indicated by the thick arrow, from left to right.
  • the present invention has for its object to provide an adjustable stator blade of the type mentioned, which achieves a very effective influencing the edge flow through targeted and problematic, block-wise definition of the profile skeleton lines along the blade height while avoiding the prior art.
  • the Fig.2 gives a precise definition of meridian flow lines and streamline profile sections.
  • the middle meridional flow line is formed by the geometric center of the ring channel. If one establishes a normal at each location of the middle streamline, one obtains the course of the ring channel width W along the flow path and, on the other hand, a number of normals with whose help further meridional streamlines result with the same relative subdivision in the direction of the channel height.
  • the intersection of a meridional streamline with a blade results in a streamline profile intersection.
  • the 3a shows the invention adjustable stator blade with storage in the housing and hub "SGN" in the determined by the axial coordinate x and the radial coordinate r meridian.
  • the blade edge zones Z1 and Z2, the transition zones T1 and T2 and the blade center zone Z0 are particularly marked and in each case by meridional flow lines as defined in FIG Fig.2 limited.
  • Each of the five bucket zones is assigned a subset WZ1, WT1, WZ0, WT2, WZ2, which is measured in the direction of the channel width W.
  • the Fig. 4 shows the definition of the height aspect ratio, which is decisive for the determination of the respective zone widths.
  • the middle streamline first gives the position for the determination of the total blade height H when halving the distance between the leading and trailing edges (point G).
  • the height H is determined along a straight line at point G perpendicular to the middle streamline.
  • five flow lines are specified at 10%, 30%, 50%, 70% and 90% of the channel width W (SL10, SL30, SL50, SL70, SL90), along which the respective chord length L is to be determined.
  • the definition of L is shown for any meridian flow area (um level) in the upper left half of the picture.
  • the chord length resulting at xy% of the channel width is here and in the formulas of Figure 4 denoted by LSLxy.
  • the Figure 5 shows the definition of the rotational axis position, which is co-determining for the present invention according to profile skeleton line type PR.
  • the picture shows a schematic of the streamline section through the adjustable stator blade at 5% and 95% channel width, respectively. Shown is the puncture point of the axis of rotation in the plane of the streamline section, point D. This point does not necessarily have to lie within the profile, as shown here.
  • the entire chord length is L. Determined by the perpendicular Lot of the point D on the chord, one obtains the measured distance d of the axis of rotation in the same direction from the front edge.
  • the respective skeleton line type is determined in relative representation with the help of the related inclination angle ⁇ * and the related run length s *, see 6a ,
  • the image shows a streamline profile cut of the blade on a meridian flow surface (um-plane).
  • the inclination angle ⁇ P and the run length sP covered up to this point are determined in all points of the skeleton line.
  • the inclination angles at leading and trailing edges ⁇ 1 and ⁇ 2 as well as the total running length of the skeleton line S are used. The following applies: ⁇ * ⁇ ⁇ 1 - ⁇ P / ⁇ ⁇ 1 - ⁇ ⁇ 2 and s * sP / S ,
  • the Figure 6b shows in the known relative representation the definition of the skeleton line type "PM". Skeleton lines according to the invention are located above a boundary line. Skeleton lines in the exclusion area below and on the boundary line are not according to the invention.
  • a skeleton line distribution which can be provided according to the invention for the block in the center of the blade is shown.
  • Skeleton line courses according to the invention are located below the continuous upper limit line and run over the lower limit line given in a specific interval. Skeleton lines in the exclusion area above and on the upper boundary line are not according to the invention. Skeleton line courses below or on the lower boundary line are also not according to the invention.
  • an edge flow control is achieved, which can increase the efficiency of each stage by about 1% with the same stability.
  • a reduction in the number of blades of up to 20% is possible.
  • the inventive concept is applicable to different types of turbomachines and, depending on the degree of utilization of the concept, leads to reductions in costs and weight for the turbomachine of 2% to 10%.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Claims (2)

  1. Stator réglable d'une turbomachine, avec une ligne moyenne de profil qui s'étend le long d'une ligne d'écoulement méridienne, sachant que le stator peut pivoter autour d'un axe de rotation, et est subdivisé dans le sens radial en au moins trois zones (Z0, Z1, Z2), que les zones (Z1, Z2) sont des zones marginales d'aube et la zone (Z0) est une zone centrale d'aube, et que dans chacune des trois zones, les lignes moyennes de profil de chaque zone (Z0, Z1, Z2) s'étendant des bords intérieurs aux bords extérieurs dans le sens radial sont formées de manière à satisfaire les équations suivantes : α * = α 1 - α P α 1 - α 2
    Figure imgb0031
    s * = s P S
    Figure imgb0032

    dans lesquelles:
    - P est un point quelconque de la ligne moyenne de profil,
    - α1 est l'angle d'inclinaison sur le bord d'attaque du stator,
    - α2 est l'angle d'inclinaison sur le bord de fuite du stator,
    - α* est l'angle adimensionnel, spécifique, de la cambrure totale,
    - s* est la longueur adimensionnelle, spécifique,
    - αP est l'angle de la tangente à un point quelconque P de la ligne moyenne de profil par rapport à la ligne d'écoulement méridienne centrale,
    - SP est la longueur de la ligne moyenne de profil à un point quelconque P, et
    - S est la longueur totale de la ligne moyenne de profil,
    caractérisé en ce que dans une représentation par un diagramme, dans lequel l'angle adimensionnel spécifique α* est représenté en fonction de la longueur adimensionnelle spécifique s*, la ligne moyenne de profil est formée dans une zone marginale d'aube (Z1, Z2) du stator à son extrémité fixe (Z1, Z2), le tracé de la ligne moyenne de profil étant représenté sous la forme α* comme fonction de s*, en dessous d'une ligne limite représentée dans le diagramme, laquelle ligne limite est obtenue conformément à l'équation suivante : α * d * , s * = α * d * = 0 , 5 + α * d * = 0 , 3 - α * d * = 0 , 5 * 0 , 5 - d * / 0 , 2 ,
    Figure imgb0033

    dans laquelle: α * d * = 0 , 3 = - 15 , 1441661664 s * 6 + 52 , 8168915277 s * 5 - 67 , 2135203453 s * 4 + 35 , 9670881201 s * 3 - 6 , 8146566070 s * 2 + 1 , 3350483823 s * + 0 , 0535731815
    Figure imgb0034

    et α * d * = 0 , 5 = 3 , 6478453237 s * 6 - 5 , 6044881912 s * 5 - 5 , 3211690262 s * 4 + 11 , 7583720270 s * 3 - 4 , 3361971934 s * 2 + 0 , 8062070974 s * + 0 , 0502599068 ,
    Figure imgb0035

    sachant qu'un axe de rotation relatif du stator est situé sur une perpendiculaire à la corde de profil dans le plan de la section respective de la ligne d'écoulement, et qu'une distance d entre l'axe de rotation D et le bord d'attaque du stator est définie par la perpendiculaire à la corde de profil, sachant que la position relative de l'axe de rotation d* est définie par d* = d/L, avec L = longueur totale de la corde du profil de l'aube à extrémité fixe et d = distance entre l'axe de rotation D et le bord d'attaque du stator dans le sens de la corde de profil, sachant qu'un rapport de la hauteur à la largeur (HSV) se détermine selon l'équation suivante: HSV = 5 H / L SL 10 + L SL 30 + L SL 50 + L SL 70 + L SL 90 ,
    Figure imgb0036

    dans laquelle:
    - H est la hauteur le long d'une ligne droite située dans le plan méridien défini par le sens radial r et le sens axial x et qui, à un point G, est perpendiculaire à une ligne d'écoulement médiane formant le centre géométrique de la voie d'écoulement dans laquelle est placé le stator,
    - L est la longueur de la corde du profil, et
    - les différentes longueurs L des cordes de profil pour cinq lignes d'écoulement correspondent à 10 %, 30 %, 50 %, 70 % et 90 % d'une largeur W de canal annulaire d'une voie d'écoulement dans laquelle est placé le stator,
    sachant que des largeurs de zone sont déterminées en fonction du rapport de la hauteur à la largeur (HSV) sous forme relative, rapportée à une largeur de canal annulaire de la voie d'écoulement (W), conformément à la consigne de calcul suivante : WZ 1 / W = WZ 2 / W = 0 , 06 HSV 0 , 65 / HSV
    Figure imgb0037
    WT 1 / W = WT 2 / W = 0 , 30 HSV 0 , 80 / HSV
    Figure imgb0038
    WZ 0 / W = 1 - WZ 1 / W - WT 1 / W - WZT 2 / W - WZ 2 / W ,
    Figure imgb0039

    dans laquelle:
    - W est la largeur du canal annulaire de la voie d'écoulement,
    - WZ1 est la largeur partielle de canal dans une zone Z1,
    - WZ2 est la largeur partielle de canal dans une zone Z2,
    - WZ0 est la largeur partielle de canal dans une zone centrale Z0,
    - WT1 est la largeur partielle de canal dans une zone transitoire entre la zone Z1 et la zone Z0, et
    - WT2 est la largeur partielle de canal dans une zone transitoire entre la zone Z0 et Z2.
  2. Stator selon la revendication n° 1, caractérisé en ce que dans une représentation du tracé de la ligne moyenne sous la forme α* comme fonction de s*, la ligne moyenne de profil dans une zone du stator située dans la zone centrale d'aube (Z0) est formée au-dessus d'une ligne limite qui est obtenue conformément à l'équation suivante : α * = - 3 , 8512520965 s * 6 + 14 , 6764714420 s * 5 - 21 , 6808727924 s * 4 + 16 , 3850592743 s * 3 - 6 , 9703863077 s * 2 + 2 , 4431236235 s * - 0 , 0060854622
    Figure imgb0040
EP06024318A 2005-12-19 2006-11-23 Profil d'aube pour aubes statoriques variables Not-in-force EP1798375B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005060699A DE102005060699A1 (de) 2005-12-19 2005-12-19 Strömungsarbeitsmaschine mit Verstellstator

Publications (3)

Publication Number Publication Date
EP1798375A2 EP1798375A2 (fr) 2007-06-20
EP1798375A3 EP1798375A3 (fr) 2008-10-29
EP1798375B1 true EP1798375B1 (fr) 2011-03-02

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EP06024318A Not-in-force EP1798375B1 (fr) 2005-12-19 2006-11-23 Profil d'aube pour aubes statoriques variables

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US (1) US7416382B2 (fr)
EP (1) EP1798375B1 (fr)
DE (2) DE102005060699A1 (fr)

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JP6694950B2 (ja) * 2016-03-30 2020-05-20 三菱重工エンジン&ターボチャージャ株式会社 可変容量型ターボチャージャ
DE102016115868A1 (de) * 2016-08-26 2018-03-01 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit hohem Ausnutzungsgrad
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Also Published As

Publication number Publication date
EP1798375A3 (fr) 2008-10-29
EP1798375A2 (fr) 2007-06-20
US7416382B2 (en) 2008-08-26
DE502006008986D1 (de) 2011-04-14
DE102005060699A1 (de) 2007-06-21
US20070140837A1 (en) 2007-06-21

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