EP1382856B1

Movatterモバイル変換

Info

Publication number: EP1382856B1
Application number: EP20010274219
Authority: EP
Inventors: Zhiming Daikin Industries Ltd. ZHENG; Jiro Daikin Industries Ltd. YAMAMOTO
Original assignee: Daikin Industries Ltd
Current assignee: Daikin Industries Ltd
Priority date: 2001-04-26
Filing date: 2001-12-25
Publication date: 2006-03-22
Anticipated expiration: 2021-12-25
Also published as: EP1382856A1; EP1382856A4; CN1201090C; DE60118103D1; ES2263554T3; AU2002217482B2; DE60118103T2; CN1449472A; HK1061707A1; WO2002090777A1; TW524928B

Abstract

A blower, comprising an impeller having a plurality of blades (3) installed on the outer periphery of a hub (2), wherein the specific areas (Q) of the blades (3) extending, in a specified width, in a vane span direction along the trailing edges (3b) of the blades (3) are bent to a negative pressure surface (3f) side, whereby the separation of air flow becomes hard to occur on the negative pressure surface (3f) of the blades (3) to suppress the disturbance of a wake (A0), the stream of the air flow discharged rearward from the trailing edges (3b) becomes smooth on the pressure surface (3e) side to reduce the disturbance, and thus the width of the wake (A0) is reduced to improve the aerodynamic characteristics of the blades.

Description

TECHNICAL FIELD

The present invention relates to a blower characterized in its blade structure and an air conditioner having the blower.

BACKGROUND ART

Fig. 17 shows a conventional common axial blower Z₀ similar to the ones discloses inJP 2 085 898 U and US 6 164 919 A. This axial blower Z₀ is constituted such that animpeller 21 formed by radially disposing a plurality of

blades

23, 23, ... around the outer periphery of ahub 22 is driven to rotate by amotor 24, and that abell mouth 25 is disposed in such a manner as to surround theimpeller 21. Furthermore, eachblade 23 of theimpeller 21 is a sweapt-forward blade obtained by proceeding its leadingedge 23a frontward in the rotation direction, and is also a thick blade wing having a cross section of a streamline shape that is attached to thehub 22 at a predetermined blade angle, as shown in Figs. 18 and 19.

Furthermore, as shown in Fig. 19, theblade 23 has a curved form with an appropriate "camber" or a curve in its chord direction. The concave side surface of the blade is a face, orpressure surface 23c, and its convex side surface is a suction surface, ornegative pressure surface 23d. When theimpeller 21 rotates, as shown in Fig. 20, an airflow that flows in from the leadingedge 23a side of theblade 23 collides with the leadingedge 23a, is divided to flow separately along thepressure surface 23c and along thenegative pressure surface 23d, and then discharged from thetrailing edge 23b side to the rear. At this time, the airflow is raised in pressure by a lift action at thepressure surface 23c and discharged or blown off toward a direction of arrow A.

Meanwhile, it is usual in the conventional axial blower Z₀ that the "camber" of theblade 23 is continuous from the leadingedge 23a to thetrailing edge 23b in one direction as shown in Fig. 19. This is based on a design idea emphasizing a static pressure characteristic of the blower that, since a lift action occurs due to this "camber" and the pressure of the airflow is raised, making the range of "camber" as large as possible is effective to obtain a higher static pressure.

However, when the "camber" of theblade 23 is continuous from the leadingedge 23a to thetrailing edge 23b as described above, a problem arises that the width of a rear stream A₀ discharged from thetrailing edge 23b of theblade 23 rearwards is increased, and the aerodynamic characteristics of theblade 23 are deteriorated, thereby lowering the air discharge efficiency as described below.

That is, since the convex shape is continuous at thenegative pressure surface 23d of theblade 23, and hence a boundary layer is gradually developed on thenegative pressure surface 23d from the leadingedge 23a towards thetrailing edge 23b. Thus, of the airflows flowing on thenegative pressure surface 23d side, an airflow A₂ that proceeds along thenegative pressure surface 23d is separated off the blade in the vicinity of thetrailing edge 23b. As a result, the rear stream A₀ discharged to the rear side of thetrailing edge 23b becomes an unstable and turbulent flow. Meanwhile, regarding thepressure surface 23c side of theblade 23, the angle difference between the airflow discharge direction at thetrailing edge 23b (that is, a direction of a tangent line to the curved surface in the vicinity of thetrailing edge 23b) and the rotation direction of theblade 23 is large. Thus, of the airflows flowing on thepressure surface 23c side, an airflow A₁ that flows along thepressure surface 23c and is discharged from thetrailing edge 23b rearwards, receives a deflecting action to flow along the blade rotation direction immediately after blown off from thetrailing edge 23b. Consequently, the flow becomes unstable, and turbulence easily occurs. When this flow is merged with the rear stream A₀, the turbulence of the rear stream A₀ is promoted, and the width of the stream in the blade thickness direction, that is, the rear stream width S is increased.

As a result, the aerodynamic resistance of eachblade 23 is increased, which in turn invites deterioration of the air discharge efficiency of the blower as a whole, and accordingly power consumption of themotor 24 is increased by the degree of this deterioration of the air discharge efficiency.

The problem of the increase in power consumption of the blower is relatively easily recognized when the blower is used alone. However, if a blower is incorporated in equipment such as, for example, an air conditioner, power consumption of the blower is very low in comparison with power consumption of other component members such as, for example, a compressor. Accordingly, when power consumption of the whole air conditioner is examined in view of energy saving property, attention has been paid to the compressor with high power consumption, but the power consumption of the blower has rarely been considered as a problem.

However, against the background of the recent further increase in social needs for environment protection and energy saving, the blower is also required to have an energy saving property, and in order to achieve this requirement, development of a technique for increasing efficiency of the blower is being required.

A blower according to the preamble ofclaim 1 is known from JP 2 085 898 U and US 6,164,919 A.

DISCLOSURE OF THE INVENTION

Accordingly, an object of the present invention is to provide a blower in which high efficiency is achieved by improving a blade structure, and an air conditioner equipped with this blower.

In order to achieve this object, the present invention provides a blower having the features ofclaim 1.

With the above constitution, the following effects can be obtained.

(a) On the negative pressure surface side of the blade, a range of a convex surface that promotes development of a boundary layer is reduced, so that airflow separation hardly occurs and turbulence of the rear stream is suppressed by the degree of reduction of the range of the convex surface. Meanwhile, on the pressure surface side of the blade, the angle difference of the airflow discharge (blowoff) direction at the trailing edge and the blade rotating direction is reduced, so that the airflow discharged from the trailing edge to the rear becomes smooth and turbulence is reduced by the degree of reduction of that angle difference. Furthermore, as a synergetic effect of these, the stream width of the rear stream discharged from the trailing edge of the blade is reduced as much as possible, and the aerodynamic characteristics of the blades are improved by the degree of this reduction of the rear stream width. As a result, efficiency of the blower is improved and power consumption is reduced by the degree of the improvement of efficiency, thereby improving energy saving property of the blower.
(b) Since only the specific region on the trailing edge side of the blade is bent towards the negative pressure surface (suction surface) side, reduction of the lifting action of the pressure surface (acting face) can be as small as possible. As a result, while reduction of the static pressure characteristic is suppressed as much as possible, the effects described in the above item (a) are secured. Thus, it is possible to obtain higher efficiency and energy saving property of the blower at the same time.

The above effects are similarly obtained when the blade has a nearly or substantially even blade thickness from the leading edge to the trailing edge as well as when the blade has a streamline-shaped cross section.

Furthermore, according to the present invention, in an air conditioner having a heat exchanger and a blower, a blower having the above constitution is employed as the blower.

This air conditioner is imparted with both higher efficiency and energy saving property by including the blower having the above constitution.

BRIEF DESCRIPTION OF THE DRAWINGS

Fig. 1 is a cross sectional view showing an essential part of an axial blower according to a first embodiment of the invention;
Fig. 2 is a front view showing an impeller shown in Fig. 1;
Fig. 3 is a cross sectional view along line III-III in Fig. 2;
Fig. 4 is an explanatory view showing how an airflow flows on blade surfaces;
Fig. 5 is a cross sectional view showing an essential part of a mixed flow blower according to a second embodiment of the invention;
Fig. 6 is a front view showing an impeller shown in Fig. 5;
Fig. 7 is a cross sectional view along line VII-VII in Fig. 6;
Fig. 8 is a front view showing an outdoor unit of an air conditioner equipped with an axial blower;
Fig. 9 is a cross sectional view along line IX-IX in Fig. 8;
Fig. 10 is a cross sectional view along line X-X in Fig. 8;
Fig. 11 is a cross sectional view showing a blade according to another embodiment;
Fig. 12 is a cross sectional view showing a blade according to yet another embodiment;
Fig. 13 is a cross sectional view showing a blade according to yet another embodiment (not part of the invention);
Fig. 14 is a graph showing an "air quantity-static pressure" characteristic of the blower;
Fig. 15 is a graph showing an "air quantity-total pressure efficiency" characteristic of the blower;
Fig. 16 is a graph showing an "air quantity-shaft power" characteristic of the blower;
Fig. 17 is a cross sectional view showing an essential part of a conventional axial blower;
Fig. 18 is a front view showing an impeller shown in Fig. 17;
Fig. 19 is a cross sectional view along line XIX-XIX in Fig. 18; and
Fig. 20 is an explanatory view showing a state of an airflow that flows on the blade.

BEST MODE FOR CARRYING OUT THE INVENTION

Hereafter, embodiments of the present invention will be described with reference to Figs. 1-13 and Figs. 14-16. It is noted that like component parts are designated by like reference numerals in Figs. 1-13.

(First embodiment)

Fig. 1 shows an axial blower Z₁ according to a first embodiment of the invention. This axial blower Z₁ is a so-called "propeller fan", and is constituted such that animpeller 1 formed by radially mounting a plurality of (three in this embodiment)

blades

3, 3, 3 onto the outer periphery of ahub 2 at a predetermined blade angle can be driven to rotate by amotor 4, and abell mouth 5 is disposed in such a manner as to surround thisimpeller 1.

Eachblade 3 of theimpeller 1 is a "sweapt-forward blade", whoseleading edge 3a extends towards the front side in the rotation direction as shown in Figs. 2 and 3. Theblade 3 is also a so-called "airfoil wing", which has a relatively large blade thickness, with this thickness gradually reduced from ablade leading edge 3a towards ablade trailing edge 3b, and has a predetermined "camber" in the chord direction. A concave side surface of the blade is a pressure surface, or actingface 3e, and its convex side surface is a negative pressure surface, orsuction surface 3f.

Furthermore, the most characteristic of thisblade 3 is that a region extending in a predetermined width along the trailingedge 3b in the wingspan direction of the blade 3 (a region closer to the trailingedge 3b than line L in Figs. 1-3) is designated as a specific region Q, and that the blade is bent towards thenegative pressure surface 3f side in this specific region Q. Therefore, in theblade 3 of this embodiment, a portion closer to theleading edge 3a and a portion closer to the trailingedge 3b relative to the line L serving as a boundary between the two portions have respective "cambers" in reverse directions. Such an arrangement of the "cambers" is novel and totally different from the one where a "camber" continues in only one direction from theleading edge 23a through the trailingedge 23b as in theconventional blade 23 shown in Fig. 19.

The following unique effects are obtained from the axial blower Z₁ having theimpeller 1 with theblades 3 having such a novel constitution.

That is, as shown in Fig. 4, when theimpeller 1 rotates, there take place an airflow A₁ and an airflow A₂, which flow from theleading edge 3a side towards the trailingedge 3b side along thepressure surface 3e and thenegative pressure surface 3f, respectively, of theblade 3. Furthermore, of these airflows A₁, A₂, the airflow A₂, which flows along thenegative pressure surface 3f, tends to be separated off the blade in the vicinity of the trailingedge 3b and generates a rear stream A₀ which is an unstable and turbulent flow. Meanwhile, the airflow A₁, which flows along thepressure surface 3e, is discharged rearwards from the trailingedge 3b and then merged with the rear stream A₀.

In such circumstances, in the axial blower Z₁ of this embodiment, since the specific region Q provided on the trailingedge 3b side of theblade 3 is bent towards thenegative pressure surface 3f side as described above, thenegative pressure surface 3f has a reduced airflow A₂ separation area on the trailingedge 3b side, and the flow of the rear stream A₀ is suppressed accordingly by the amount of reduction of the airflow A₂ separation area. Meanwhile, on thepressure surface 3e side, since the specific region Q is bent towards thenegative pressure surface 3f sides, the discharge direction of the airflow A₁ to the rear at the trailingedge 3b becomes closer to the rotation direction of theblade 3, and the angular difference between these directions is reduced. Accordingly, the discharge of the airflow A₁ becomes smoother, so that even if this flow is merged with the rear stream A₀, increase of the turbulence in the rear stream A₀ is suppressed and stabilization of the rear stream A₀ is promoted accordingly. Thus, an increase of the rear stream width S is suppressed.

As a result, the aerodynamic characteristics of theblades 3 are improved by the degree of suppression of the increase of the rear stream width S, and the efficiency of the axial blower Z₁ is improved. By the degree of this efficiency improvement, the power consumption is reduced and the energy saving property is also improved.

Furthermore, as described above, since the axial blower Z₁ of this embodiment is constituted such that only the specific region Q on the trailingedge 3b side of theblade 3 is bent towards thenegative pressure surface 23d side, reduction of the lifting action of thepressure surface 3e due to the presence of the specific region Q is suppressed as much as possible, and the static pressure characteristic is favorably maintained.

Thus, in the axial blower Z₁ of this embodiment, higher efficiency and energy saving property are simultaneously achievable by an extremely simple and inexpensive constitution that the specific region Q on the trailingedge 3b side of theblade 3 is bent towards thenegative pressure surface 3f side.

Figs. 14-16 show results of various performance tests to confirm each of the above effects in the axial blower Z₁ of this embodiment.

Fig. 14 is an "air quantity - static pressure" characteristic graph. A curve La1 shows a characteristic of the axial blower Z₁ of the above embodiment. A curve Lb1 shows a characteristic of an axial blower having a conventional structure. This "air quantity - static pressure" characteristic graph in Fig. 14 shows that the static pressure performance of the axial blower Z₁ of this embodiment is lower than that of the conventional blower to some extent because, in the axial blower Z₁ of the embodiment, an effective area of the actingface 3e, that is, the area of a portion involved in the air pressure raising action is reduced by bending the specific region Q portion on the trailingedge 3b side of theblade 3 towards thenegative pressure surface 3f side.

Fig. 15 is an "air quantity - total pressure efficiency" characteristic graph. A curve La2 shows a characteristic of the axial blower Z₁ of this embodiment. A curve Lb2 shows a characteristic of an axial blower with a conventional structure. It is apparent from this "air quantity - total pressure efficiency" characteristic graph in Fig. 15 that the axial blower Z₁ of the embodiment has higher total pressure efficiency than that of the conventional axial blower.

Fig. 16 is an "air quantity - shaft power" characteristic diagram. A curve La3 shows a characteristic of the axial blower Z₁ of the above embodiment. A curve Lb3 shows a characteristic of an axial blower having a conventional structure. It is apparent from this "air quantity - shaft power" characteristic graph in Fig. 16 that the shaft power of the axial blower Z₁ of the embodiment is significantly lower than the shaft power of the conventional axial blower.

As is apparent from the above, in the axial blower Z₁ of this embodiment, the static pressure performance is maintained high although slightly lower than that of the conventional blower. Meanwhile, regarding, both the total pressure efficiency and the shaft power, the axial blower Z₁ of this embodiment is more excellent than the blower of the conventional structure, and particularly in the shaft power the embodiment is much superior. Therefore, when these performances are compared and considered, it can be said that the axial blower Z₁ of this embodiment is highly efficient and excellent in energy saving property in total in comparison with the blower of the conventional structure.

(Second embodiment)

Fig. 5 shows a mixed flow blower Z₂ according to a second embodiment of the invention. This axial blower Z₂ is constituted such that animpeller 1 formed by radially mounting a plurality of (four in this embodiment)

blades

3, 3, 3 onto the outer periphery of ahub 2 in the shape of a truncated cone at a predetermined blade angle can be driven to rotate by amotor 4, and abell mouth 5 is disposed in such a manner as to surround thisimpeller 1.

Eachblade 3 of theimpeller 1 is a "sweapt-forward blade", whoseleading edge 3a extends towards the front side in the rotation direction as shown in Figs. 6 and 7. Theblade 3 is also a so-called "airfoil wing", which has a relatively large blade thickness, with this thickness gradually reduced from aleading edge 3a towards a trailingedge 3b, and has a predetermined "camber" in the chord direction, as shown in Fig. 3. A concave side surface of the blade is a pressure surface, or actingface 3e, and its convex side surface is a negative pressure surface, orsuction surface 3f.

Furthermore, the most characteristic of thisblade 3 is that, when a region extending in a predetermined width along the trailingedge 3b in the wingspan direction of the blade 3 (a region closer to the trailingedge 3b than line L in Figs. 5-7) is assumed as a specific region Q, the blade is bent towards thenegative pressure surface 3f side in this specific region Q. Therefore, in theblade 3 of this embodiment, a portion closer to theleading edge 3a and a portion closer to the trailingedge 3b with the region line L as a boundary have respective "cambers" in reverse directions. Such an arrangement of the "cambers" is novel and totally different from the structure of the conventional blade 23 (see Fig. 19).

The mixed flow blower Z₂ having theimpeller 1 with theblades 3 of such a novel constitution has the same effects as the first embodiment axial blower Z₁, except that the direction of flow of the air as discharged (blown off) is different between these blowers. Therefore, the above-description on the effects of the first embodiment is incorporated by reference as the effects of the second embodiment and further description is omitted.

(Third embodiment)

Figs. 8-10 show an outdoor unit Y of an air conditioner equipped with the axial blower Z₁ according to the first embodiment. In this outdoor unit Y, a rectangular box-like casing 10 is partitioned by apartition wall 11. One side of the wall is used aheat exchange chamber 12, and the other side is used as amachine chamber 13. The axial blower Z₁ and aheat exchanger 6 are disposed in theheat exchange chamber 12, and acompressor 7 is disposed in themachine chamber 13. Furthermore, anoutlet port 9 faced by the axial blower Z₁ is equipped with agrill 8.

In this outdoor unit Y, when the axial blower Z₁ is driven and theimpeller 1 rotates, an airflow is generated that passes from the outdoor through theheat exchanger 6 and theimpeller 1 and is discharged through theoutlet port 9 to the outdoor, and heat exchange is allowed between the airflow and a refrigerant circulated in theheat exchanger 6.

Since the outdoor unit Y of this embodiment is equipped with, as an air supply means to theheat exchanger 6, the axial blower Z₁ according to the first embodiment, which is highly efficient and excellent in energy saving property with low power consumption, it is an ideal outdoor unit having both high heat exchange efficiency and energy saving property.

(Modified Examples)

In the axial blower Z₁ of the first embodiment, a thick "airfoil wing" as shown in Fig. 3 is adopted as theblade 3. Furthermore, in the mixed flow blower Z₂ of the second embodiment, a thin "airfoil wing" as shown in Fig. 7 is adopted as theblade 3. However, theblade 3 of the present invention is not limited to these forms, but various forms such as those shown in Figs. 11-13 can be adopted.

Theblade 3 shown in Fig. 11 is an airfoil wing having a special form wherein a portion closer to itsleading edge 3a is made locally thick, and the other portions are made thin.

Theblade 3 shown in Fig. 12 is an airfoil wing having a special form, wherein a relatively large portion closer to itsleading edge 3a is made thick, and the blade thickness is gradually reduced from this thick portion towards the trailingedge 3b.

Theblade 3 shown in Fig. 13 (not part of the invention) is a plate wing formed by bending a thin plate having a certain thickness with a predetermined "camber".

In any of these modified examples of theblade 3, the same effects as those of the blowers Z₁, Z₂ according to the first and second embodiments are obtained by.bending a predetermined region on the trailingedge 3b side (that is, the specific region Q) towards thenegative pressure surface 3f side.