WO2003051559A1 - Fan blade and method for producing the same - Google Patents

Fan blade and method for producing the same Download PDF

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Publication number
WO2003051559A1
WO2003051559A1 PCT/FI2001/001111 FI0101111W WO03051559A1 WO 2003051559 A1 WO2003051559 A1 WO 2003051559A1 FI 0101111 W FI0101111 W FI 0101111W WO 03051559 A1 WO03051559 A1 WO 03051559A1
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WO
WIPO (PCT)
Prior art keywords
blade
leading edge
mould
blades
casting
Prior art date
Application number
PCT/FI2001/001111
Other languages
French (fr)
Inventor
Markku Kemppainen
Arvo Huisko
Original Assignee
Fortum Oyj
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 Fortum Oyj filed Critical Fortum Oyj
Priority to AU2002219257A priority Critical patent/AU2002219257A1/en
Priority to PCT/FI2001/001111 priority patent/WO2003051559A1/en
Publication of WO2003051559A1 publication Critical patent/WO2003051559A1/en
Priority to FI20040845A priority patent/FI116890B/en

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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
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/0081Casting in, on, or around objects which form part of the product pretreatment of the insert, e.g. for enhancing the bonding between insert and surrounding cast metal
    • 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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/388Blades characterised by construction
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/21Manufacture essentially without removing material by casting
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/12Light metals
    • F05D2300/121Aluminium
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6032Metal matrix composites [MMC]

Definitions

  • the invention relates to a fan blade according to the preamble of claim 1 for use under erosive conditions, said blade being characterized by light weight and improved erosion resistance also at elevated temperatures up to approx. 220 °C.
  • the invention also relates to a method for producing the fan blade.
  • Fan blades of the type concerned in the present invention are used in industrial fans operating under heavily erosive conditions either at ambient temperature or in atmospheres of elevated temperatures .
  • Flue gas fans of peat- or coal-fired power plants represent a typical application.
  • the flue gases exit the power plant boiler at a temperature of 120 °C to 150 °C with a high content of flyash, whose particulate matter is both erosive and corrosive.
  • Other demanding applications comprise dryer fans in paper machines, ventilation blowers in mines, vacuum cleaning system blowers for dusty industrial processes and air-conditioning blowers for industrial buildings .
  • the lightest possible materials such as alloys of aluminium are favored in the fan constructions. Due to their low specific weight vs. strength, also different kinds of polymers are attractive, but the low erosion resistance and poor strength at elevated temperatures limit their use under erosive conditions and elevated temperatures. Also the erosion resistance of aluminum alloys as well as their strength at elevated temperatures remain less than desirable. Moreover, the fatigue resistance and stiffness properties of aluminium alloys are relatively low. Therefore, steel is frequently used as a fan construction material in applications subject to erosion and elevated temperatures. However, steel is hampered by its high density. Fans made from steel components are massive requiring heavy-duty bearings and support structures.
  • the fan blades are bombarded by flyash particles carried along with the flue gas.
  • the fan blade comprises the blade section proper and a stem keyed for mounting on the blade wheel hub, whereby for improved wear resistance a hard-chromium plated lining strip of austenitic stainless steel is flush-mounted and fixed with screws in a recess, which is made to the leading edges of the blade section.
  • the hard-chromium plating on the protective wear strip has a thickness of 0.5 mm.
  • the strength of metal alloys can be improved by comple- menting their base metal matrix with reinforcing filler materials.
  • Such reinforcing fillers conventionally comprise ceramic materials that retain their solid-state composition at the casting temperature of the base metal, whereby the group of typical filler materials includes silicon carbide, aluminium oxide, boron carbide and carbon in different forms. and.shapes. Also glass and steel are used to some extent .
  • the base metal matrix thus reinforced generally is a light metal alloy such as the alloys of Al, Mg and Ti .
  • metal-matrix particulate composite is an aluminium alloy filled with silicon carbide or aluminium oxide particles whose volume in the casting melt is 5 - 30 vol.-% with a particle size of 5 - 40 ⁇ m, obviously other material combinations can be used.
  • Filler reinforced metals or metal alloys can be made into objects in a plurality of different ways, the most common production methods being casting and various pulverized metal processing methods. While casting is the production method of best cost-efficiency, casting a reinforced material is much more complicated than that of nonfilled metal alloys.
  • ceramic particles are used as the reinforcing filler material in castings, but fibers and pulverized material may in special cases be used as dispersed filler.
  • the reinforcing filler particles must be dispersed homogeneously or in a desired manner in the object being manufactured, and between the matrix metal and the filler material must be formed a strong bond free from brittle phases such as compounds or oxides of the matrix metal .
  • the filler particles must be coated or heat-treated.
  • the bonding strength between these two can be improved during casting by applying an external pressure, which obviously complicates the design of the manufacturing process and leads into clumsy casting arrangements.
  • a fan blade made of aluminium composite material by casting comprises a wear strip made of strip metal and cast integrally into the blade proper.
  • the wear strip of the fan blade is fabricated by bending a curved section conformant to the shape, .of..the blade leading edge .. To .the inside of the curved section is attached by welding a drilled bonding plate which ensures a integral bond during casting and serves as a backing rail during resurfacing welding of the wear strip.
  • the problem with this structure is that the inner volume of the strip is limited by the edges of the strip and the bonding blade so that the cast composite material that flows very difficultly may not fill the volume within the edges of the strip totally.
  • the strip is colder than the cast material whereby the material may solidify within the wear strip too fast and prevent the flow of the cast material .
  • the wear strip is heated with a blow torch in order to prevent above mentioned problems, but because of the structure of the wear strip and the cooling of the strip before casting the weight difference caused by pores within the wear strip between different blades is still too high. If there is a weight difference between the blades they must, be placed on the blower so that the weights of different blades balance each other or balancing weights must be used. In either case the blades must be accurately weighed and the mounting of the blades is difficult. Because of balancing' procedure of the blower the replacement of the blades is difficult and possible unbalance that is left causes vibration problems of the structures leading to the need of further maintenance and monitoring of the apparatuses .
  • the goal of the invention is accomplished through producing the blade by casting from an aluminium alloy filled with reinforcing particles.
  • the leading edge of the blade is made of steel and integrally bonded to the blade during casting, which gives the blade a still further improved wear resistance and a small weight variation.
  • the steel leading edge is heated at least prior to casting with electric current after the mould is closed.
  • the blade according to the invention is characterized by what is stated in the characterizing part of claim 1.
  • the method for manufacturing the blade is characterized by what is stated in the characterizing part of claim 6.
  • the invention offers significant benefits.
  • a blade according to the invention wherein the leading edge is integrally cast on the blade and protrudes within the blade stem key has a strength and stiffness better compared with forged aluminium blades and clearly superior compared with conventional cast aluminium blades.
  • the leading edge protrudes also from the distal end of the blade so that the leading edge extends over the whole length of the blade .
  • a backplate of the leading edge extends over almost half of the width of the blade.
  • the leading edge may be readily resurfaced by welding, which under certain circumstances can be an important benefit. For instance, under the operating conditions of a peat-fired power plant, the leading edge is eroded faster than the blade section itself.
  • the construction of the leading edge permits resurfacing welding of the wear strip,..thus making it possible .to recondition blades having intact blade sections but eroded leading edges for reuse. In the example case of a peat-fired power plant, such resurfacing welding may give the fan blades a service life better than three years.
  • the structural material of the blades can be recycled. The material may be melted and recast into a blade section in the same fashion as aluminum alloys are recycled. Thus, the material is fully recyclable.
  • the blades according to the present invention have a high quality combined with an advantageous production cost.
  • the steel leading edge provides a possibility to manufacture blades that have a minimum form and weight variation.
  • the blades are further ground by a diamond grinder in order to further minimize the weight variation and to give the blade a smooth surface. Smoothing the surface improves further the abrasion resistance by removing protrusions and dents from the blade. If a abrading particles hit such a dent or protrusion, they start to wear a groove over the blade. Grooving of the blade may cause imbalance or disturbance of the flow and force to fix or change the blade.
  • the greatest advantage of the invention is that the balancing of the blower and mounting of the blades is easier since the variation of the weight of the blades is small, normally less than 3% of the total weight of a blade of a certain size. Also the tolerances of the blade can be tighter whereby the performance of the single blade does not vary, whereby the operating balance of the blower is further improved. As is well known the static and dynamic balance has great effect on the durability and operational life of machinery.
  • the mounting of the blades becomes also easier since it is not necessary to weight each blade before mounting an calculate its position on the blower hub diameter in relation of the other blades having a different varying weight. In order to further decrease the weight variation, the blades are weighed after casting and sorted in weight classes.
  • the blades are ground by a diamond grinder according to weighing results, the heaviest blades being worked on the most and the lightest the lest, naturally.
  • the finished blades may further be sorted in weight classes in order to aid the mounting of the blades. If the weight class of the blades is marked at the factory, it is not any more necessary to weigh the blades when mounting, which speeds up the mounting greatly.
  • Figure 1 is a view of one embodiment of a blower blade according to the invention.
  • Figure 2 is a diagram of a mould for manufacturing of the blades according to the invention including a cast blade
  • the weight variation is a weight difference of the lightest and the heaviest blade of the same size and configuration.
  • This variation may be 3% or smaller of the calculated design weight or alternatively 3% of the mean weight of the blades of a same size and configuration.
  • Preferably the weight variation is 2% at the highest.
  • the variation is examined "as cast", that is after casting of the blades before machining of the blades but after removing material left in pouring basin and casting passage ways.
  • the fan blade is made by casting from a reinforced particle filled aluminum alloy. That part of the blade section 2 on which the erosive particles impinge perpendicularly is protected by a steel plate leading edge part 1. In those cases where the angle of attack on the blade is invariably oblique (0° - 15°) or the amount of erosive particles is insignificant, no wear protecting steel part is required.
  • the steel plate construction 1 is bonded to the leading edge of the blade by integral casting and is extended to reach into the blade mounting key 3 moulded to the blade stem and the distal end of the blade correspondingly.
  • the mounting key is shown here diagrammatically only.
  • the steel leading edge 1 is attached to the blade section during the casting operation by integral cast bonding techniques.
  • the reinforcing filler of the blade composite material comprises silicon carbide particles with a particle diameter of 9 - 20 ⁇ m typical. Also other reinforcing materials and filler particle sizes are feasible. Typically, the proportion of the filler material is from 5 to 20 vol.-% depending on the application and degree of erosiveness under the operating conditions.
  • the matrix component of the composite material typically is a cast- able aluminium alloy such as AlSi9Mg0.6. Also other cast- able aluminium alloys can be used.
  • a suitable composite material for the fan blades of the above-described peat- fired power plant is the aluminium-matrix-based composite comprised of AlSi9Mg0.6 with 10 vol.-% of SiC (9.3 ⁇ m particle size) as the filler.
  • the protective wear strip or plate of the blade is made from Avesta 2205 duplex steel, for example. Other grades of steel suitable for this purpose are widely available and the choice can be made according to the availability and conditions in the environment where the blade is used.
  • the steel plate leading edge 1 is integrally cast so as to extend into the blade stem key 3 thus imparting extra strength to the area where the blade section 2 joins with the blade stem key 3.
  • the leading edge protrudes also from the distal end of the blade so that the leading edge extends over the whole length of the blade.
  • a backplate of the leading edge extends over almost half of the width of the blade.
  • the front edge of the steel leading edge 1 is additionally provided with a fixing lug 4 at which the steel leading edge 1 is fixed in place during casting by means of a pin inserted through the lug 4.
  • Other shapes of blades equipped with a steel leading edge 1 or pad must have an appropriately modified design of geometry.
  • the length of the blades made by this method is typically 100 - 1400 mm.
  • the leading edge 1 consists of three pieces: a backplate
  • the leading part 6 forms the profile of the front edge of the blade and is formed accordingly.
  • the leading part has an U-form cross section.
  • the backplate 5 is attached on the convex side of the leading part 6 and extends almost at the bottom of the groove formed inside the leading part 6. In the bottom of the groove of the leading part is a filler wire 7 and the edge of the backplate 5 rests on the wire 7.
  • the leading part 6, the edge of the backplate 5 and the filler wire 7 are joined together by a discontinuous welding 8. Of coarse, continuous welding may also be used but then heavy heat transfer may cause deformations more easily..
  • the backplate 5 is joined with the leading part 6 also at the edge of the convex side of the leading part
  • the backplate is bent first towards the center of the leading edge 1 and then directly away therefrom.
  • the protruding part of the backplate 5 comprises holes 9 for attachment to the blade section 2.
  • the holes 9 are advantageously made by punching, but drilling or other working methods may be used.
  • the part of the backplate 5 located inside the leading part 6 comprises a row of triangular tongues 10 pointing towards the blade section 2. These tongues 10 are formed by punching and bending from the material of the backplate 5.
  • the tongues 10 also serve for attachment of the leading edge 1 to the blade section 2.
  • the backplate 5 and the leading part 6 have a material thickness of 2 mm, for example and the diameter of the filler wire 7 is 4 mm. The dimensioning of the materials is of course dependent on the dimensions of the blade.
  • the filler wire 7 right under the front edge of the leading part 6 enabled successful repair welding of the leading edge 1 by guaranteeing that there is enough material for the welding material to attach to.
  • the convex side of the blade wears more rapidly, whereby this side is reinforced by two overlapping metal layers. This enables repair welding of this area also.
  • the backplate 5 extends over almost the half of the width and the whole length of the blade and reinforces thus the whole blade.
  • the cast blade is shown in its casting mould.
  • the casting mould comprises conventional upper 15 and lower 11 parts wherein a cavity for the blade 2 is formed. Further, on the side of the leading edge 1 of the blade there is a space for a steel leading edge 1 and a space for an electric resistor 13 which can be connected to a electric power source through leads 14
  • the casting proceeds as follows.
  • the steel leading edge 1 is placed in its place in the lower part 11 of the mould and attached firmly on the mould trough a pin pushed through a hole 12 on the fixing lug 4 and pins pushed through holes on the end of the steel leading edge 1.
  • the electric resistor 13 is placed into the space provided therefor and the ends of the leads 14 are placed outside the mould. After these measures glue is spread on the lower part 11 of the mould and the mould is closed by placing the upper part 15 on the lower part 11. Now the cast steel leading edge 1 and the electric resistor 13 are kept tightly between the halves 11, 15 of the mould and electric current can be connected to the electric resistor 13 for heating the steel leading edge 1 and the mould for casting.
  • the heating of the steel leading edge is essential for successful casting for two reasons. First, it evaporates all moisture from the leading edge 1 and from the mould material, which might cause pores in the cast metal.
  • the heating prevents the cast metal to solidify too early whereby the metal flows freely into the inner volume of the leading edge 1 and the cast metal fills this volume thoroughly.
  • the heating removes free gases from the mould.
  • the temperature of the steel leading edge 1 should be about 70 - 200 °C, advantageously 130 °C, at the beginning of the filling of the mould depending on the cast material and dimensions of the blade and leading edge. However, other temperatures may be useful in some occasion.
  • the heating of the cast steel leading edge may be terminated before beginning the filling of the mould but it must be taken care that the leading edge 1 is at desired elevated temperature when the casting starts.
  • the filling of the mould is performed in usual manner preferably using an automated tilting device that keeps the .filling speed of the mould in optimum. The heating can be continued during the filling of the mould and the solidifying of the cast composite metal.
  • the power of the 170 W and eight moulds may be connected to a power source simultaneously. Heating period is 5 hours during which the temperature of the leading edge and the mould reaches 130 °C. This temperature ensures removal of free gases from the mould, which then ensures a product free of pores . By this method the weight variation of the blades can be kept within 2% advantageously.
  • blades having a very low porosity and therefore small weight variation can be manufactured.
  • the weight variation of the blades can be kept as small as 3% of the calculated or medium weight and in some conditions even as small as 2%.
  • Such a small weight variation removes the need of the balancing of the blowers or makes the balancing very easy when the blades are chanced.
  • feeder heads and barbs are removed and the castings weighed. Then the castings are sorted into groups and ground by a diamond grinder into desired weight. The grinding also finishes the surface of the blades. Finished blades are then sorted into at least three weight categories in order to aid balancing of a fan during installation.
  • the present invention may have alternative embodiments.
  • the steel leading edge can be heated by induction or connecting electric current directly on the cast steel leading edge .
  • these methods require more sophisticated electric power sources to control the temperature of the steel leading edge.
  • the important feature of the electrical heating is that it makes it possible to heat the leading edge while it is within the mould thus preventing the cooling of the part before casting, which is evident if the part is heated in oven or by a blow torch before closing the mould.
  • the shape of the blade is made to fit the operating environment and fan type using the same design rules as for any other blade, with the exception that the improved strength imparted by the novel material permits the use of smaller material thicknesses where desirable.
  • the leading edge part can be surfaced for higher wear resistance by hard-chromium plating, for instance.
  • Suitable steel grades for use in the leading edge part are, e.g., ferritic, austenitic and duplex steels.
  • the wear-subjected section of the blade need to be made from a composite material filled with reinforcing particles, whereby the blade stem, for instance, can be made from an alloy of aluminium or steel if so desired, because the blade stem jointed to the blade wheel hub has a substantially smaller tangential speed than the blade section thus undergoing less wear.
  • the castable material is advantageously selected from the group of composites commercially available from known manufacturers. Aluminium-matrix based composites are made at least by Duralcan, USA, and Hydro Aluminium, Norway. In the casting method itself, the appropriate design of the melt passageway is particularly crucial as was noted previously.
  • the melt passageway shall be formed so that any possible bends caused by the pattern in the melt passageway are streamlined. For this purpose, the use of a manifold-type passageway may be necessary, whereby the number of parallel paths should, however, preferably be minimized.
  • the fan blades according to the invention are used in industrial fans operating under heavily erosive condi- tions either at ambient temperature or in atmospheres of elevated temperatures. Flue gas fans of peat- or coal- fired power plants represent a typical application. The flue gases exit the power plant boiler at a temperature of 120°C to 150°C with a high content of flyash, whose particulate matter is both erosive and corrosive.
  • the fan blades according to the invention are most suitable for use in fans operated under a wide range of demanding conditions. While these fans are desiredly characterized by light weight, high wear resistance, tolerance to elevated temperatures and a certain degree of corrosion resistance, also other types of applications can be contemplated for the present invention.

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  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
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Abstract

The present invention relates to a fan blade intended for use under erosive conditions and characterized by a light weight and high tolerance to erosion even at elevated temperatures up to approx. 220 °C. The invention is based on fabricating the blade (2) by casting from an aluminium-matrix composite alloy material filled with reinforcing particles. A steel wear pad (1) serving to further improve the wear resistance, strength and stiffness of the blade is bonded by integral casting to the leading edge of the blade (2). The innovation to manufacture the blade by using electrical heating for the steel wear pad and the mould enable to cast products free of defects, homogenous and equal of weights.

Description

Fan blade and method for producing the same
The invention relates to a fan blade according to the preamble of claim 1 for use under erosive conditions, said blade being characterized by light weight and improved erosion resistance also at elevated temperatures up to approx. 220 °C. The invention also relates to a method for producing the fan blade.
Fan blades of the type concerned in the present invention are used in industrial fans operating under heavily erosive conditions either at ambient temperature or in atmospheres of elevated temperatures . Flue gas fans of peat- or coal-fired power plants represent a typical application. The flue gases exit the power plant boiler at a temperature of 120 °C to 150 °C with a high content of flyash, whose particulate matter is both erosive and corrosive. Other demanding applications comprise dryer fans in paper machines, ventilation blowers in mines, vacuum cleaning system blowers for dusty industrial processes and air-conditioning blowers for industrial buildings .
Fans are often used under conditions which are strongly erosive to the structures of the fans, whereby the fan blades must be changed as often as several times a year due to erosion or other damage. Such fan blade replacement entails extra costs caused by both the replacement operations themselves and the necessary shutdown times. These costs may rise to a substantial level. Particularly high costs may be incurred in power plants . In United States, the annual costs attributed to damage caused by erosion to the fans of coal-fired power plants have been estimated at USD 12 million (M. Menguturk & E.F. Sverdrup, Fan Erosion Control. Forschung im Ingenieur- wesen 52(1986)1, pp. 9-12. Due to the high rotational speeds involved, the structures of the fans are designed for minimum weight. Hence, the lightest possible materials such as alloys of aluminium are favored in the fan constructions. Due to their low specific weight vs. strength, also different kinds of polymers are attractive, but the low erosion resistance and poor strength at elevated temperatures limit their use under erosive conditions and elevated temperatures. Also the erosion resistance of aluminum alloys as well as their strength at elevated temperatures remain less than desirable. Moreover, the fatigue resistance and stiffness properties of aluminium alloys are relatively low. Therefore, steel is frequently used as a fan construction material in applications subject to erosion and elevated temperatures. However, steel is hampered by its high density. Fans made from steel components are massive requiring heavy-duty bearings and support structures.
Exemplifying the function and service life of aluminium alloy fan blades, reference is made to a peat-fired power plant in Joensuu, Finland, previously owned by Fortum Power and Heat Oy. The flue gas fans (axial-type fans) of the power plant have blade rotors with a diameter of approx. 2000 mm and their speed of rotation is from 1000 to 1500 rpm. Due to the large dimensions and high speed of rotation, the fan components must have a low mass, and therefore, their blades are made by casting and forging from a special lightweight aluminium alloy (containing 2-3 % Zn, 1-1.5 % Mg, trace amounts of Ti, Cu, Si, Cr and Fe, the remainder being Al) . Rotating at a high speed, the fan blades are bombarded by flyash particles carried along with the flue gas. The fan blade comprises the blade section proper and a stem keyed for mounting on the blade wheel hub, whereby for improved wear resistance a hard-chromium plated lining strip of austenitic stainless steel is flush-mounted and fixed with screws in a recess, which is made to the leading edges of the blade section. The hard-chromium plating on the protective wear strip has a thickness of 0.5 mm.
In this specific application, erosion caused by flyash particulate matter is so severe that the blades must be replaced once or twice a year. During these operating intervals, both the edge lining strip and the blade proper are worn into a condition beyond duty and repair. The trailing edge of the blade proper is worn totally through at the end of the service cycle and the hard- chromium plated surface of the lining strip is eroded down to deep net-like cracking pattern. In addition to erosive wear, the rotor blades may suffer a sudden damage by breaking off at the area where the blade section joins with the blade stem key. To improve their erosion resistance, thermal spray coating like HVOF -coating of the blades by aluminium oxide, tungsten carbide or chromium carbide has been attempted. However, such spray-coatings have not given an improved erosion tolerance to the blades. Despite their limited service life, however, such blades find continuous use in the absence of more favourable alternatives.
The strength of metal alloys can be improved by comple- menting their base metal matrix with reinforcing filler materials. Such reinforcing fillers conventionally comprise ceramic materials that retain their solid-state composition at the casting temperature of the base metal, whereby the group of typical filler materials includes silicon carbide, aluminium oxide, boron carbide and carbon in different forms. and.shapes. Also glass and steel are used to some extent . The base metal matrix thus reinforced generally is a light metal alloy such as the alloys of Al, Mg and Ti . While the most commonly used metal-matrix particulate composite is an aluminium alloy filled with silicon carbide or aluminium oxide particles whose volume in the casting melt is 5 - 30 vol.-% with a particle size of 5 - 40 μm, obviously other material combinations can be used.
Filler reinforced metals or metal alloys can be made into objects in a plurality of different ways, the most common production methods being casting and various pulverized metal processing methods. While casting is the production method of best cost-efficiency, casting a reinforced material is much more complicated than that of nonfilled metal alloys. Typically, ceramic particles are used as the reinforcing filler material in castings, but fibers and pulverized material may in special cases be used as dispersed filler. The reinforcing filler particles must be dispersed homogeneously or in a desired manner in the object being manufactured, and between the matrix metal and the filler material must be formed a strong bond free from brittle phases such as compounds or oxides of the matrix metal . To obtain such a strong bond between the filler particles and the matrix metal, the filler particles must be coated or heat-treated. The bonding strength between these two can be improved during casting by applying an external pressure, which obviously complicates the design of the manufacturing process and leads into clumsy casting arrangements.
In the publication WO 96/38247 it is described a fan blade made of aluminium composite material by casting. The blade comprises a wear strip made of strip metal and cast integrally into the blade proper. The wear strip of the fan blade is fabricated by bending a curved section conformant to the shape, .of..the blade leading edge .. To .the inside of the curved section is attached by welding a drilled bonding plate which ensures a integral bond during casting and serves as a backing rail during resurfacing welding of the wear strip. The problem with this structure is that the inner volume of the strip is limited by the edges of the strip and the bonding blade so that the cast composite material that flows very difficultly may not fill the volume within the edges of the strip totally. On the other hand the strip is colder than the cast material whereby the material may solidify within the wear strip too fast and prevent the flow of the cast material . These reasons lead to pores in the blade within the wear strip.
Even though the pores may not essentially decrease the strength of the blade, the weight of the blade and the position of the center of gravity of the blade does change because of the pores. This leads to serious balancing problems in fast rotating large diameter blowers. According to the WO 96/38247 the wear strip is heated with a blow torch in order to prevent above mentioned problems, but because of the structure of the wear strip and the cooling of the strip before casting the weight difference caused by pores within the wear strip between different blades is still too high. If there is a weight difference between the blades they must, be placed on the blower so that the weights of different blades balance each other or balancing weights must be used. In either case the blades must be accurately weighed and the mounting of the blades is difficult. Because of balancing' procedure of the blower the replacement of the blades is difficult and possible unbalance that is left causes vibration problems of the structures leading to the need of further maintenance and monitoring of the apparatuses .
It is an object of the present invention. to achieve, a..fan blade and a method for manufacturing the same made from a metal-matrix particulate composite material, said blade having a wear resistance under erosive and high- temperature conditions that is essentially better than is achievable by means of conventional designs and having a very small weight variation readily after casting. The goal of the invention is accomplished through producing the blade by casting from an aluminium alloy filled with reinforcing particles. The leading edge of the blade is made of steel and integrally bonded to the blade during casting, which gives the blade a still further improved wear resistance and a small weight variation. The steel leading edge is heated at least prior to casting with electric current after the mould is closed.
More specifically, the blade according to the invention is characterized by what is stated in the characterizing part of claim 1.
The method for manufacturing the blade is characterized by what is stated in the characterizing part of claim 6.
The invention offers significant benefits.
In conventional tests performed in a laboratory- controlled environment, it has been found that the addition of reinforcing ceramic filler particles in a metal alloy in general does not significantly improve the wear resistance of the object under erosive conditions. Unexpectedly, however, it has been found that fan blades operating under erosive conditions can be given an essentially elevated wear resistance through manufacturing the blades from a metal-matrix particulate composite material. Plausibly, a precondition for an improved wear resistance, is that the angle of.. incidence of the erosive particulate matter hitting the blade must be properly arranged particularly in the area of the trailing edge of the blade and the blade surface itself. Besides the improved wear resistance, the blade according to the invention offers elevated operating temperature at approx. 220 EC max. continuous duty, which is essentially higher than that of a forged aluminium alloy blade.
The steel plate construction in the leading edge of the fan blade gives the blade a good bending strength. The bonding of the plate construction to the blade edge by means of integral casting strengthens and stiffens both the leading edge of the fan blade and the joining area of the blade section with the blade stem key, which is socketed on the blade wheel hub. By contrast, a wear strip separately mounted to the blade edge by screws does not impart a greater strength to the blade structure . A blade according to the invention wherein the leading edge is integrally cast on the blade and protrudes within the blade stem key has a strength and stiffness better compared with forged aluminium blades and clearly superior compared with conventional cast aluminium blades. The leading edge protrudes also from the distal end of the blade so that the leading edge extends over the whole length of the blade . A backplate of the leading edge extends over almost half of the width of the blade. These features guarantee that the blade does not shatter totally if hit by any large objects accidentally entering the fan.
The leading edge may be readily resurfaced by welding, which under certain circumstances can be an important benefit. For instance, under the operating conditions of a peat-fired power plant, the leading edge is eroded faster than the blade section itself. The construction of the leading edge permits resurfacing welding of the wear strip,..thus making it possible .to recondition blades having intact blade sections but eroded leading edges for reuse. In the example case of a peat-fired power plant, such resurfacing welding may give the fan blades a service life better than three years. Moreover, the structural material of the blades can be recycled. The material may be melted and recast into a blade section in the same fashion as aluminum alloys are recycled. Thus, the material is fully recyclable.
The blades according to the present invention have a high quality combined with an advantageous production cost. The steel leading edge provides a possibility to manufacture blades that have a minimum form and weight variation. The blades are further ground by a diamond grinder in order to further minimize the weight variation and to give the blade a smooth surface. Smoothing the surface improves further the abrasion resistance by removing protrusions and dents from the blade. If a abrading particles hit such a dent or protrusion, they start to wear a groove over the blade. Grooving of the blade may cause imbalance or disturbance of the flow and force to fix or change the blade.
The greatest advantage of the invention is that the balancing of the blower and mounting of the blades is easier since the variation of the weight of the blades is small, normally less than 3% of the total weight of a blade of a certain size. Also the tolerances of the blade can be tighter whereby the performance of the single blade does not vary, whereby the operating balance of the blower is further improved. As is well known the static and dynamic balance has great effect on the durability and operational life of machinery. The mounting of the blades becomes also easier since it is not necessary to weight each blade before mounting an calculate its position on the blower hub diameter in relation of the other blades having a different varying weight. In order to further decrease the weight variation, the blades are weighed after casting and sorted in weight classes. Thereafter the blades are ground by a diamond grinder according to weighing results, the heaviest blades being worked on the most and the lightest the lest, naturally. The finished blades may further be sorted in weight classes in order to aid the mounting of the blades. If the weight class of the blades is marked at the factory, it is not any more necessary to weigh the blades when mounting, which speeds up the mounting greatly.
In the following the invention is described in greater detail by making reference to the appended drawings in which
Figure 1 is a view of one embodiment of a blower blade according to the invention;
Figure 2 is a diagram of a mould for manufacturing of the blades according to the invention including a cast blade; and
In the following the weight variation is a weight difference of the lightest and the heaviest blade of the same size and configuration. This variation may be 3% or smaller of the calculated design weight or alternatively 3% of the mean weight of the blades of a same size and configuration. Preferably the weight variation is 2% at the highest. The variation is examined "as cast", that is after casting of the blades before machining of the blades but after removing material left in pouring basin and casting passage ways.
Next, the manufacture by casting of a blade according to the invention for a flue gas fan is described as an exemplifying embodiment. Only the features characterizing the invention are discussed, in..detail and.a more thorough description of casting of this kind of blades is in the WO 96/38247.
According to the embodiment described below, the fan blade is made by casting from a reinforced particle filled aluminum alloy. That part of the blade section 2 on which the erosive particles impinge perpendicularly is protected by a steel plate leading edge part 1. In those cases where the angle of attack on the blade is invariably oblique (0° - 15°) or the amount of erosive particles is insignificant, no wear protecting steel part is required. The steel plate construction 1 is bonded to the leading edge of the blade by integral casting and is extended to reach into the blade mounting key 3 moulded to the blade stem and the distal end of the blade correspondingly. The mounting key is shown here diagrammatically only. Thus, the steel leading edge 1 is attached to the blade section during the casting operation by integral cast bonding techniques.
The reinforcing filler of the blade composite material comprises silicon carbide particles with a particle diameter of 9 - 20 μm typical. Also other reinforcing materials and filler particle sizes are feasible. Typically, the proportion of the filler material is from 5 to 20 vol.-% depending on the application and degree of erosiveness under the operating conditions. The matrix component of the composite material typically is a cast- able aluminium alloy such as AlSi9Mg0.6. Also other cast- able aluminium alloys can be used. A suitable composite material for the fan blades of the above-described peat- fired power plant is the aluminium-matrix-based composite comprised of AlSi9Mg0.6 with 10 vol.-% of SiC (9.3 μm particle size) as the filler.
The protective wear strip or plate of the blade is made from Avesta 2205 duplex steel, for example. Other grades of steel suitable for this purpose are widely available and the choice can be made according to the availability and conditions in the environment where the blade is used. The steel plate leading edge 1 is integrally cast so as to extend into the blade stem key 3 thus imparting extra strength to the area where the blade section 2 joins with the blade stem key 3. The leading edge protrudes also from the distal end of the blade so that the leading edge extends over the whole length of the blade. A backplate of the leading edge extends over almost half of the width of the blade. These features guarantee that the blade does not shatter totally if hit by any large objects accidentally entering the fan. The front edge of the steel leading edge 1 is additionally provided with a fixing lug 4 at which the steel leading edge 1 is fixed in place during casting by means of a pin inserted through the lug 4.' Other shapes of blades equipped with a steel leading edge 1 or pad must have an appropriately modified design of geometry. The length of the blades made by this method is typically 100 - 1400 mm.
The leading edge 1 consists of three pieces: a backplate
5, a leading part 6 and a filler wire 7. The leading part 6 forms the profile of the front edge of the blade and is formed accordingly. The leading part has an U-form cross section. The backplate 5 is attached on the convex side of the leading part 6 and extends almost at the bottom of the groove formed inside the leading part 6. In the bottom of the groove of the leading part is a filler wire 7 and the edge of the backplate 5 rests on the wire 7. The leading part 6, the edge of the backplate 5 and the filler wire 7 are joined together by a discontinuous welding 8. Of coarse, continuous welding may also be used but then heavy heat transfer may cause deformations more easily.. The backplate 5 is joined with the leading part 6 also at the edge of the convex side of the leading part
6. The backplate is bent first towards the center of the leading edge 1 and then directly away therefrom. Thus the part of the backplate 5 protruding from the leading part extends in the middle of the blade section 2. The protruding part of the backplate 5 comprises holes 9 for attachment to the blade section 2. The holes 9 are advantageously made by punching, but drilling or other working methods may be used. The part of the backplate 5 located inside the leading part 6 comprises a row of triangular tongues 10 pointing towards the blade section 2. These tongues 10 are formed by punching and bending from the material of the backplate 5. The tongues 10 also serve for attachment of the leading edge 1 to the blade section 2. The backplate 5 and the leading part 6 have a material thickness of 2 mm, for example and the diameter of the filler wire 7 is 4 mm. The dimensioning of the materials is of course dependent on the dimensions of the blade.
The filler wire 7 right under the front edge of the leading part 6 enabled successful repair welding of the leading edge 1 by guaranteeing that there is enough material for the welding material to attach to. The convex side of the blade wears more rapidly, whereby this side is reinforced by two overlapping metal layers. This enables repair welding of this area also. The backplate 5 extends over almost the half of the width and the whole length of the blade and reinforces thus the whole blade.
In figure 2 the cast blade is shown in its casting mould. The casting mould comprises conventional upper 15 and lower 11 parts wherein a cavity for the blade 2 is formed. Further, on the side of the leading edge 1 of the blade there is a space for a steel leading edge 1 and a space for an electric resistor 13 which can be connected to a electric power source through leads 14
The casting proceeds as follows. The steel leading edge 1 is placed in its place in the lower part 11 of the mould and attached firmly on the mould trough a pin pushed through a hole 12 on the fixing lug 4 and pins pushed through holes on the end of the steel leading edge 1. The electric resistor 13 is placed into the space provided therefor and the ends of the leads 14 are placed outside the mould. After these measures glue is spread on the lower part 11 of the mould and the mould is closed by placing the upper part 15 on the lower part 11. Now the cast steel leading edge 1 and the electric resistor 13 are kept tightly between the halves 11, 15 of the mould and electric current can be connected to the electric resistor 13 for heating the steel leading edge 1 and the mould for casting.
The heating of the steel leading edge is essential for successful casting for two reasons. First, it evaporates all moisture from the leading edge 1 and from the mould material, which might cause pores in the cast metal.
Secondly, the heating prevents the cast metal to solidify too early whereby the metal flows freely into the inner volume of the leading edge 1 and the cast metal fills this volume thoroughly. Third, the heating removes free gases from the mould. The temperature of the steel leading edge 1 should be about 70 - 200 °C, advantageously 130 °C, at the beginning of the filling of the mould depending on the cast material and dimensions of the blade and leading edge. However, other temperatures may be useful in some occasion. The heating of the cast steel leading edge may be terminated before beginning the filling of the mould but it must be taken care that the leading edge 1 is at desired elevated temperature when the casting starts. The filling of the mould is performed in usual manner preferably using an automated tilting device that keeps the .filling speed of the mould in optimum. The heating can be continued during the filling of the mould and the solidifying of the cast composite metal.
The power of the 170 W and eight moulds may be connected to a power source simultaneously. Heating period is 5 hours during which the temperature of the leading edge and the mould reaches 130 °C. This temperature ensures removal of free gases from the mould, which then ensures a product free of pores . By this method the weight variation of the blades can be kept within 2% advantageously.
By using a steel plate leading edge 1 and preheating of the leading edge when it is within the mould in order to keep it and the mould in elevated temperature at least until the filling of the mould begins, blades having a very low porosity and therefore small weight variation can be manufactured. By this method, the weight variation of the blades can be kept as small as 3% of the calculated or medium weight and in some conditions even as small as 2%. Such a small weight variation removes the need of the balancing of the blowers or makes the balancing very easy when the blades are chanced.
After the blades have been cast and removed from the moulds, feeder heads and barbs are removed and the castings weighed. Then the castings are sorted into groups and ground by a diamond grinder into desired weight. The grinding also finishes the surface of the blades. Finished blades are then sorted into at least three weight categories in order to aid balancing of a fan during installation.
Besides those described above, the present invention may have alternative embodiments.
The steel leading edge can be heated by induction or connecting electric current directly on the cast steel leading edge . However these methods require more sophisticated electric power sources to control the temperature of the steel leading edge. The important feature of the electrical heating is that it makes it possible to heat the leading edge while it is within the mould thus preventing the cooling of the part before casting, which is evident if the part is heated in oven or by a blow torch before closing the mould.
Obviously, the shape of the blade is made to fit the operating environment and fan type using the same design rules as for any other blade, with the exception that the improved strength imparted by the novel material permits the use of smaller material thicknesses where desirable. The leading edge part can be surfaced for higher wear resistance by hard-chromium plating, for instance. Suitable steel grades for use in the leading edge part are, e.g., ferritic, austenitic and duplex steels. In principle, only the wear-subjected section of the blade need to be made from a composite material filled with reinforcing particles, whereby the blade stem, for instance, can be made from an alloy of aluminium or steel if so desired, because the blade stem jointed to the blade wheel hub has a substantially smaller tangential speed than the blade section thus undergoing less wear.
The castable material is advantageously selected from the group of composites commercially available from known manufacturers. Aluminium-matrix based composites are made at least by Duralcan, USA, and Hydro Aluminium, Norway. In the casting method itself, the appropriate design of the melt passageway is particularly crucial as was noted previously. The melt passageway shall be formed so that any possible bends caused by the pattern in the melt passageway are streamlined. For this purpose, the use of a manifold-type passageway may be necessary, whereby the number of parallel paths should, however, preferably be minimized.
The fan blades according to the invention are used in industrial fans operating under heavily erosive condi- tions either at ambient temperature or in atmospheres of elevated temperatures. Flue gas fans of peat- or coal- fired power plants represent a typical application. The flue gases exit the power plant boiler at a temperature of 120°C to 150°C with a high content of flyash, whose particulate matter is both erosive and corrosive. Here, the fan blades according to the invention are most suitable for use in fans operated under a wide range of demanding conditions. While these fans are desiredly characterized by light weight, high wear resistance, tolerance to elevated temperatures and a certain degree of corrosion resistance, also other types of applications can be contemplated for the present invention.

Claims

Claims :
1. A fan blade for use under erosive conditions, the blade comprising a blade section (2) made by casting from a metal-matrix composite material containing reinforcing particles, a steel leading edge (1) bonded to the blade section by integral casting and fixing elements (3) at one end of the blade section for attaching the blade to a blade wheel hub of a fan, c h a r a c t e r i z e d in that the leading edge (1) comprises a leading part (6) having a cross section in form of U, the legs of the U- shape forming a convex part and a concave part of the edge of the blade, a filler wire (7) in the bottom of the leading part (6) and a backplate (5) attached under the convex leg of the leading edge (6) and extending over the whole length of the blade and towards the blade section (2) .
2. A blade as defined in claim 1, c h a r a c t e r - i z e d in that the parts of the leading part (1) are welded together.
3. A blade as defined in claim 1 or 2, c h a r a c t e r i z e d in that the metal-matrix composite materi- al of the blade is comprised of aluminum, alloying components and a reinforcing filler selected from the group of silicon carbide, aluminum oxide and other ceramic particles .
4. A blade as defined in claim 1 or 2, c h a r a c t e r i z e d in that the weight variation.of .the blades of same size and construction is 3%, advantageously 2% and most advantageously 1% at highest
5. A blade as defined in claim 2, c h a r a c t e r i z e d in that the part of the backplate (5) located inside the leading part (6) comprises a row of triangular tongues (10) pointing towards the blade section (2) .
6. A method for producing a fan blade, comprising,
- placing a steel leading edge (1) within a mould (11, 15) , and
- filling the mould (11, 15) with a metal matrix composite material containing reinforcing particles, in order to form the blade (1, 2, 3) and to attach the leading edge (1) to the blade,
c h a r a c t e r i z e d by heating the leading edge (1) electrically within said mould (11, 15) at least before filling said mould (11, 15) with said metal matrix composite material simultaneously heating the mould (11, 15.
7. A method according to the claim 6, c h a r a c t e r - i z e d in that the leading edge (1) is heated to a temperature of 70 - 200 °C, advantageously 130 °C before beginning of the filling of the mould.
8. A method according to the claim 6 or 7, c h a r a c t e r i z e d in that the leading edge (1) is heated by an electric resistor (13 ) placed within the mould (11, 15) .
9. A method according to the claim 6 or 7, c h a r a c t e r i z e d in that the leading edge (1) is heated through electric induction.
10. A method according to the claim 6 or 7, c h a r a c t e r i z e d in that the wear pad is heated by connecting electric current directly to the leading edge (1) .
11. A method according to the claim 6, c h a r a c t e r i z e d by heating the leading edge (1) for at least 5 hours .
PCT/FI2001/001111 2001-12-17 2001-12-17 Fan blade and method for producing the same WO2003051559A1 (en)

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AU2002219257A AU2002219257A1 (en) 2001-12-17 2001-12-17 Fan blade and method for producing the same
PCT/FI2001/001111 WO2003051559A1 (en) 2001-12-17 2001-12-17 Fan blade and method for producing the same
FI20040845A FI116890B (en) 2001-12-17 2004-06-17 Fan blade for industrial fan used in erosive conditions, such as in peat-fired or coal-fired power plants, has steel leading edge comprising leading part, filler wire, and back plate

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2345754A1 (en) * 2008-10-22 2010-09-30 Productos No Ferricos De Mungia, S.L. Alabe armado (Machine-translation by Google Translate, not legally binding)
FR2991612A1 (en) * 2012-06-11 2013-12-13 Snecma PROCESS FOR THE FOUNDED PRODUCTION OF A PIECE COMPRISING AN EFFICIENT PORTION
CN104889703A (en) * 2007-12-31 2015-09-09 涡轮发动机零部件科技公司 Method of Manufacturing a Turbine Fan Blade
US9945389B2 (en) 2014-05-05 2018-04-17 Horton, Inc. Composite fan
CN110328462A (en) * 2019-07-01 2019-10-15 安徽安风风机有限公司 High intensity transition method at volute tongue chamfering

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4241110A (en) * 1978-07-20 1980-12-23 Mitsubishi Jukogyo Kabushiki Kaisha Method of manufacturing rotor blade
WO1996038247A1 (en) * 1995-06-02 1996-12-05 Imatran Voima Oy Blower blade

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4241110A (en) * 1978-07-20 1980-12-23 Mitsubishi Jukogyo Kabushiki Kaisha Method of manufacturing rotor blade
WO1996038247A1 (en) * 1995-06-02 1996-12-05 Imatran Voima Oy Blower blade

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104889703A (en) * 2007-12-31 2015-09-09 涡轮发动机零部件科技公司 Method of Manufacturing a Turbine Fan Blade
CN104889703B (en) * 2007-12-31 2017-07-11 涡轮发动机零部件科技公司 The method for manufacturing turbine fan blade
ES2345754A1 (en) * 2008-10-22 2010-09-30 Productos No Ferricos De Mungia, S.L. Alabe armado (Machine-translation by Google Translate, not legally binding)
FR2991612A1 (en) * 2012-06-11 2013-12-13 Snecma PROCESS FOR THE FOUNDED PRODUCTION OF A PIECE COMPRISING AN EFFICIENT PORTION
US9962763B2 (en) 2012-06-11 2018-05-08 Snecma Casting method for obtaining a part including a tapering portion
US9945389B2 (en) 2014-05-05 2018-04-17 Horton, Inc. Composite fan
US10415587B2 (en) 2014-05-05 2019-09-17 Horton, Inc. Composite fan and method of manufacture
US10914314B2 (en) 2014-05-05 2021-02-09 Horton, Inc. Modular fan assembly
CN110328462A (en) * 2019-07-01 2019-10-15 安徽安风风机有限公司 High intensity transition method at volute tongue chamfering

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