WO2014054132A1 - プロペラファン - Google Patents

プロペラファン Download PDF

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Publication number
WO2014054132A1
WO2014054132A1 PCT/JP2012/075656 JP2012075656W WO2014054132A1 WO 2014054132 A1 WO2014054132 A1 WO 2014054132A1 JP 2012075656 W JP2012075656 W JP 2012075656W WO 2014054132 A1 WO2014054132 A1 WO 2014054132A1
Authority
WO
WIPO (PCT)
Prior art keywords
propeller fan
secondary flow
flow control
blades
virtual line
Prior art date
Application number
PCT/JP2012/075656
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
惇司 河野
敬英 田所
Original Assignee
三菱電機株式会社
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 三菱電機株式会社 filed Critical 三菱電機株式会社
Priority to US14/423,495 priority Critical patent/US20150204345A1/en
Priority to JP2014539524A priority patent/JP5984162B2/ja
Priority to EP12886000.4A priority patent/EP2905474B1/de
Priority to PCT/JP2012/075656 priority patent/WO2014054132A1/ja
Priority to CN201280076216.5A priority patent/CN104685218B/zh
Publication of WO2014054132A1 publication Critical patent/WO2014054132A1/ja

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • F04D29/684—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid injection
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/329—Details of the hub
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • F04D29/682—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid extraction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/002—Axial flow fans

Definitions

  • the present invention relates to a propeller fan, a blower, and an outdoor unit.
  • the propeller fan generally has a cylindrical boss connected to a drive source and a plurality of blades extending radially from the outer peripheral surface of the boss. Further, in Patent Document 1, the position at which the warp ratio is maximum in each blade is set to a position closer to the blade root than the outer periphery of the blade, and further, from the maximum position of the warp ratio to the blade root. A configuration in which the warp ratio is gradually reduced is disclosed. With this configuration, the generation of vortices is suppressed in the vicinity of the blade root portion without causing a large amount of work.
  • JP 2012-052443 A (mainly FIG. 1)
  • the airflow between the blades flows along the blades by balancing the Coriolis force acting in the direction opposite to the rotation direction of the propeller fan and the pressure gradient of the adjacent blade surfaces.
  • the presence of the above pressure gradient extends to the outer peripheral surface of the boss, whereas the relative velocity of the air current is small in the boundary layer of the outer peripheral surface of the boss, so that the Coriolis force is reduced. Therefore, in the vicinity of the outer peripheral surface of the boss, the balance is lost, and a secondary flow toward the adjacent blade is generated due to the influence of the pressure gradient. And when this secondary flow collides with a wing
  • the vortex generated at the connecting portion between the blade and the boss can be suppressed by gradually decreasing the warpage ratio from the maximum position of the warpage ratio to the root of the blade.
  • the work of the wing in the vicinity of the connection part becomes small.
  • the present invention has been made in view of the above, and suppresses vortices generated at the connection between the blade and the boss without depending on the setting of the warp ratio of the blade near the blade root, thereby reducing the noise of the fan.
  • An object of the present invention is to provide a propeller fan capable of achieving the above.
  • the propeller fan of the present invention for achieving the above-described object is a propeller fan including a boss portion having a cylindrical wall and a plurality of blades extending radially from the outer peripheral surface of the cylindrical wall of the boss portion.
  • a secondary flow control slit is provided between a pair of adjacent blades on the outer peripheral surface, and each of the plurality of secondary flow control slits penetrates the cylindrical wall and the inside of the boss portion. It communicates with the outside of the boss, the downstream end of the cylindrical wall is closed, the upstream end of the cylindrical wall is open, and each of the plurality of secondary flow control slits is a side surface.
  • a blower device of the present invention includes the above-described propeller fan of the present invention, a drive source that applies driving force to the propeller fan, and a casing that houses the propeller fan and the drive source.
  • the outdoor unit of the present invention for achieving the same object includes a heat exchanger, the above-described propeller fan of the present invention, a drive source for applying a driving force to the propeller fan, the propeller fan, and the drive source. And a casing for housing the heat exchanger.
  • the vortex generated at the connection portion between the blade and the boss can be suppressed without depending on the setting of the warp ratio of the blade near the blade root, and the noise of the fan can be reduced.
  • FIG. 1 is a side view of a propeller fan according to a first embodiment. It is a figure explaining the airflow on the boss
  • FIG. It is a figure explaining the airflow which passes the slit of the boss
  • FIG. It is a figure explaining the installation position of the slit of a boss outer peripheral surface regarding Embodiment 2 of this invention. It is a figure explaining the installation position of the slit of a boss outer peripheral surface regarding Embodiment 3 of this invention.
  • FIG. 4 It is a figure explaining the installation position of the slit of a boss outer peripheral surface regarding Embodiment 4 of this invention. It is a figure explaining the shape of the slit of a boss outer peripheral surface regarding Embodiment 5 of this invention. It is a figure explaining the shape of the slit of a boss outer peripheral surface regarding Embodiment 6 of this invention. It is a figure explaining the airflow which passes between the blades which concern on the propeller fan as a comparative example. It is a perspective view when the outdoor unit which concerns on Embodiment 7 of this invention is seen from the blower outlet side. It is a figure for demonstrating the structure of an outdoor unit from the upper surface side regarding this Embodiment 7. FIG. It is a figure which shows the state which removed the fan grille regarding this Embodiment 7. FIG. It is a figure which shows an internal structure regarding this Embodiment 7, further removing a front panel etc. FIG.
  • FIG. 1 is a perspective view showing a propeller fan according to Embodiment 1 of the present invention from the downstream side. 2, 3 and 4 are a side view of the propeller fan, a diagram for explaining the airflow on the outer peripheral surface of the boss, and a diagram for explaining the airflow passing through the slit, respectively.
  • the propeller fan 1 includes a boss portion 3 and a plurality of wings 5.
  • the boss 3 has a cylindrical tube wall 3a.
  • An output shaft of a driving source such as a motor is connected to the central portion 3b of the boss portion 3, and the propeller fan 1 is rotated by the driving force of the driving source.
  • 1 indicates the rotation direction of the propeller fan 1
  • the reference RA in FIG. 2 indicates the rotation axis of the propeller fan 1
  • the reference US conceptually indicates the upstream airflow
  • DS conceptually shows the downstream airflow.
  • the downstream end of the cylindrical wall 3a of the boss portion 3 is closed by the lid plate portion 3c.
  • the upstream end of the boss portion 3 in the cylindrical wall 3a is open, whereby the inside of the boss portion 3 communicates with the outside of the boss portion 3.
  • the plurality of blades 5 extend radially from the outer peripheral surface 3d of the cylindrical wall 3a of the boss 3.
  • the plurality of blades 5 are provided with the same shape and the same interval.
  • Each of the blades 5 has an outer peripheral edge 5a, a blade root portion 5b, a leading edge 5c, a trailing edge 5d, a positive pressure surface 5e, and a negative pressure surface 5f.
  • the outer peripheral edge 5a is an edge part on the radially outer side of the blade 5, and is an edge part extending in the circumferential direction.
  • the blade root portion 5 b is a portion connected to the outer peripheral surface 3 d of the boss portion 3 in the blade 5.
  • the front edge 5 c is an edge portion that connects the front end of the outer peripheral edge 5 a and the front end of the blade root portion 5 b, and is an edge portion on the front side in the rotational direction of the propeller fan 1.
  • the rear edge 5d is an edge portion that connects the rear end of the outer peripheral edge 5a and the rear end of the blade root portion 5b, and is an edge portion on the rear side in the rotation direction of the propeller fan 1.
  • both the front edge 5c and the rear edge 5d are curved so as to be positioned forward in the rotational direction as going outward in the radial direction.
  • Both the positive pressure surface 5e and the negative pressure surface 5f are blade surfaces defined by an outer peripheral edge 5a, a blade root portion 5b, a leading edge 5c, and a trailing edge 5d in plan view.
  • the positive pressure surface 5e and the negative pressure surface 5f are located in a front-back relationship with each other.
  • the positive pressure surface 5e is a blade surface on the downstream side of the airflow generated by the rotation of the propeller fan 1
  • the negative pressure surface 5f is a blade surface on the upstream side of the airflow. In the illustrated configuration, the positive pressure surface 5e is concave toward the downstream side, and the negative pressure surface 5f is convex toward the upstream side.
  • a secondary flow control slit 7 is provided between a pair of adjacent blades 5 on the outer peripheral surface 3d of the boss 3. As best shown in FIG. 4, each of the plurality of secondary flow control slits 7 on the entire outer peripheral surface 3 d of the boss portion 3 penetrates the cylindrical wall 3 a of the boss portion 3, and the inside of the boss portion 3. The outside of the boss 3 is communicated with.
  • each of the plurality of secondary flow control slits 7 extends obliquely with respect to the rotation axis RA of the propeller fan in a side view, and the blades of the plurality of blades 5.
  • the base portion 5b extends in the same direction as the forming direction.
  • each of the secondary flow control slits 7 extends linearly in a side view, and is inclined so as to be located on the upstream side of the airflow toward the front side in the rotation direction of the propeller fan.
  • the air blowing operation in the propeller fan according to the first embodiment will be described.
  • the flow in the propeller fan as a comparative example having no features of the present invention will be described.
  • the airflow flowing into the propeller fan from the upstream side flows downstream along the blade 55 as indicated by an arrow F3.
  • the airflow flowing into the propeller fan from the upstream side from the vicinity of the front edge 55c of the pressure surface 55e of the blade 55 to the suction surface 55f of the adjacent blade 55, as indicated by an arrow F4. After heading, it vortexes and flows downstream.
  • the airflow between the blades balances the Coriolis force acting in the direction opposite to the rotation direction and the pressure gradient from the pressure surface 55e of the blade 55 to the suction surface 55f of the adjacent blade 55.
  • a flow along the wing 55 is formed.
  • the presence of the above-described pressure gradient extends to the outer peripheral surface of the boss portion 53, whereas the relative velocity of the air current is small in the boundary layer of the outer peripheral surface of the boss portion 53, so the Coriolis force is reduced.
  • the upstream end surface of the boss portion 3 is opened, the inside of the boss portion 3 communicates with the upstream side of the propeller fan 1, and the gap between the blades is formed on the outer peripheral surface of the boss portion 3.
  • a secondary flow control slit 7 is provided to connect the inside and outside of the boss 3 so as to cross. Therefore, when the pressure between the blades is higher than the pressure inside the boss portion 3, the secondary flow is on the outer peripheral surface 3 d of the boss portion 3 as shown by the solid arrow F ⁇ b> 1 in FIGS. 3 and 4. It is sucked into the boss 3 through the secondary flow control slit 7.
  • the secondary flow is separated from the boundary layer on the outer peripheral surface 3d of the boss portion 3 by this air flow, the air flow flowing to the negative pressure surface 5f can be suppressed, and the turbulence of the air flow due to the generation of vortices can be suppressed.
  • the secondary flow control slit 7 is inclined in the same direction as the blade 5 with respect to the rotation axis RA of the propeller fan, the secondary flow control slit 7 is provided for the air flow parallel to the blade 5.
  • the action to be applied can be reduced, and further, the above-described vortex generation suppressing effect can be increased by making a right angle to the secondary flow.
  • the vortex generated at the connecting portion between the blade and the boss can be suppressed by the secondary flow control slit, and the noise of the fan can be reduced. Moreover, since it does not depend on the setting of the warp ratio of the blades near the blade root part, it is possible to suppress the generation of vortices while effectively working even near the blade root part.
  • FIG. 5 is a diagram for explaining the installation positions of the slits on the outer peripheral surface of the boss in the second embodiment of the present invention.
  • FIG. 5 shows a state in which the outer peripheral surface 3d of the boss part 3 is partially expanded.
  • the blade root part 5b of the pair of blades 5 and the secondary flow control slit located between them. 107 is shown.
  • a virtual line VL1 connecting a plurality of leading edges 5c at the position of the blade root part 5b and a virtual line VL2 connecting a plurality of trailing edges 5d at the position of the blade root part 5b are considered.
  • the secondary flow control slit 107 is provided in a range between the virtual line VL1 and the virtual line VL2. Other features of the secondary flow control slit 107 may be the same as those of the secondary flow control slit 7 of the first embodiment.
  • the vortex generated at the connecting portion between the blade and the boss can be suppressed, and the noise of the fan can be reduced.
  • the secondary flow control slit is limitedly provided in a range where the pressure gradient between the blades is large and the secondary flow is likely to occur, so that the generation of vortices is suppressed while reducing the influence on the main flow. it can.
  • FIG. 6 is a view for explaining the installation positions of the slits on the outer peripheral surface of the boss in the third embodiment of the present invention, and is a view similar to FIG.
  • a virtual line VL ⁇ b> 3 extending further in the middle position in the circumferential direction of a pair of adjacent blades (blade root portion 5 b) is considered.
  • the virtual line VL3 is a line obtained by connecting the circumferential midpoints of a pair of camber lines (blade thickness center lines) CL in a pair of adjacent wings from a pair of leading edges to a pair of trailing edges. It is.
  • the secondary flow control slit 207 extends in a range between the imaginary line VL1 and the imaginary line VL2, and is a front side region in the rotation direction RD of the propeller fan from the imaginary line VL3. Is placed inside.
  • Other features of the secondary flow control slit 207 may be the same as those of the secondary flow control slit 7 of the first embodiment.
  • the secondary flow control slit 207 is disposed at a position close to the suction surface 5f where the secondary flow is strongest (that is, a position closer to the suction surface 5f than the positive pressure surface 5e). The effect for suppressing the secondary flow is remarkably obtained.
  • FIG. 7 is a diagram for explaining the installation positions of the slits on the outer peripheral surface of the boss in the fourth embodiment of the present invention, and is a diagram in the same manner as FIG. In FIG. 7, in addition to virtual lines VL1, VL2, and VL3 similar to those in FIG. 6, virtual lines VL4 and VL5 are further considered.
  • the imaginary line VL4 is a line located at an equal distance from the pair of imaginary lines VL1 and VL2 in FIG. 7, in other words, the rotation axis direction of the propeller fan at the pair of imaginary lines VL1 and VL2. It is a line extending in the middle position. 7, the intersection of the camber line (blade thickness center line) CL and the virtual line VL4 in the front blade 5 in the rotation direction RD of the propeller fan in the corresponding pair of blades 5 is defined as P.
  • a line segment connecting the leading edge 5c of the corresponding rear wing 5 and the intersection P of the corresponding front wing 5 is considered as a virtual line VL5.
  • the secondary flow control slit 307 extends in a range between the imaginary line VL1 and the imaginary line VL2, and is ahead of the imaginary line VL3 in the rotation direction RD of the propeller fan. And in the rear side region in the rotation direction RD of the propeller fan with respect to the virtual line VL5.
  • the secondary flow control slit 307 is the virtual line VL2, the virtual line VL3, the virtual line VL5, and the propeller fan rotation direction RD of the corresponding pair of blades 5 as seen in FIG. It arrange
  • Other features of the secondary flow control slit 207 may be the same as those of the secondary flow control slit 7 of the first embodiment.
  • the same advantages as in the third embodiment can be obtained. Further, the secondary flow is very likely to occur from the vicinity of the front edge of the boss connecting portion in the rear wing to the middle point or the rear edge of the front edge and the rear edge of the adjacent front wing, In the fourth embodiment, there is an advantage that the action by the secondary flow control slit can be obtained more intensively in the region where the secondary flow is very likely to occur.
  • FIG. 8 is a diagram for explaining the installation positions of the slits on the outer peripheral surface of the boss in the fifth embodiment of the present invention, and is a diagram in the same manner as FIG.
  • the secondary flow control slit 407 in the fifth embodiment extends in parallel with the warp of the blade 5.
  • the secondary flow control slit 407 in FIG. 8 is a more limited example in the fifth embodiment, but the arrangement form of the secondary flow control slit in the fourth embodiment (in FIG. (The intersection is not shown), and is further curved so as to be parallel to the warp of the blade 5.
  • the secondary flow control slit relating to the fifth embodiment extends in parallel with the warpage of the blade in the secondary flow control slit of any of the first to fourth embodiments described above. It is not necessarily limited to the state shown in FIG.
  • the secondary flow control slit is parallel to the main flow of the airflow between the blades, so that it is given to the main flow. The influence can be reduced.
  • FIG. 9 is a diagram for explaining the installation positions of the slits on the outer peripheral surface of the boss in the sixth embodiment of the present invention, and is a diagram in the same manner as FIG.
  • the secondary flow control slit 507 in the sixth embodiment has a width of L / 10 or less (slit extending direction) with respect to the inter-blade distance L in the circumferential direction of the corresponding pair of blades 5. In the direction perpendicular to the direction).
  • the other configuration of the secondary flow control slit 507 is the same as that of any of the secondary flow control slits of the first to fifth embodiments described above.
  • FIG. FIG. 11 is a perspective view of the outdoor unit (blower) according to the seventh embodiment when viewed from the outlet side
  • FIG. 12 is a diagram for explaining the configuration of the outdoor unit from the upper surface side.
  • FIG. 13 shows a state in which the fan grill is removed
  • FIG. 14 is a diagram showing the internal configuration by further removing the front panel and the like.
  • the outdoor unit body (casing) 51 is configured as a housing having a pair of left and right side surfaces 51a, 51c, a front surface 51b, a back surface 51d, an upper surface 51e, and a bottom surface 51f.
  • the side surface 51a and the back surface 51d have an opening for sucking air from the outside (see arrow A in FIG. 12).
  • the blower outlet 53 is formed in the front panel 52 as an opening part for blowing air outside (refer arrow A of FIG. 12).
  • the blower outlet 53 is covered with a fan grille 54, thereby preventing contact between an object or the like and the propeller fan 1 for safety.
  • the propeller fan 1 is installed in the outdoor unit main body 51.
  • the propeller fan 1 is the propeller fan according to any one of the first to sixth embodiments described above.
  • the propeller fan 1 is connected to a fan motor (drive source) 61 on the back surface 51 d side via a rotary shaft 62, and is driven to rotate by the fan motor 61.
  • the interior of the outdoor unit main body 51 is divided into a blower chamber 56 in which the propeller fan 1 is housed and installed, and a machine room 57 in which the compressor 64 and the like are installed, by a partition plate (wall body) 51g. .
  • a heat exchanger 68 is provided so as to extend in a substantially L shape in plan view.
  • a bell mouth 63 is disposed on the outer side in the radial direction of the propeller fan 1 disposed in the blower chamber 56.
  • the bell mouth 63 is located outside the outer peripheral end of the blade 5 and has an annular shape along the rotation direction of the propeller fan 1.
  • a partition plate 51g is located on one side of the bell mouth 63 (rightward in the drawing of FIG. 12), and on the other side (opposite direction) (leftward in the drawing of FIG. 12).
  • a part of the heat exchanger 68 is located.
  • the front end of the bell mouth 63 is connected to the front panel 52 of the outdoor unit so as to surround the outer periphery of the outlet 53.
  • the bell mouth 63 may be configured integrally with the front panel 52 or may be prepared as a separate body.
  • a flow path between the suction side and the blow-out side of the bell mouth 63 is configured as an air path near the blow-out port 53. That is, the air passage near the blowout port 3 is separated from the other space in the blower chamber 56 by the bell mouth 63.
  • the heat exchanger 68 provided on the suction side of the propeller fan 1 includes a plurality of fins arranged side by side so that the plate-like surfaces are parallel to each other, and a heat transfer tube penetrating each fin in the direction of arrangement. I have.
  • a refrigerant circulating through the refrigerant circuit flows in the heat transfer tube.
  • the heat transfer tube extends in an L shape over the side surface 51a and the back surface 51d of the outdoor unit main body 51, and a plurality of stages of the heat transfer tubes meander while passing through the fins as shown in FIG. Configured to do.
  • the heat exchanger 68 is connected to the compressor 64 via a pipe 65 and the like, and further connected to an indoor heat exchanger, an expansion valve, etc. (not shown) to constitute a refrigerant circuit of the air conditioner. Further, a substrate box 66 is disposed in the machine room 7, and equipment mounted in the outdoor unit is controlled by a control board 67 provided in the substrate box 66.
  • this Embodiment 7 demonstrated the outdoor unit of the air conditioning apparatus as an example of the outdoor unit including the air blower, the present invention is not limited to this, and is implemented as, for example, an outdoor unit such as a water heater. Further, it can be widely applied as a device for blowing air, and can also be applied to devices and facilities other than outdoor units.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PCT/JP2012/075656 2012-10-03 2012-10-03 プロペラファン WO2014054132A1 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US14/423,495 US20150204345A1 (en) 2012-10-03 2012-10-03 Propeller fan
JP2014539524A JP5984162B2 (ja) 2012-10-03 2012-10-03 プロペラファン、送風装置、および室外機
EP12886000.4A EP2905474B1 (de) 2012-10-03 2012-10-03 Propellerlüfter
PCT/JP2012/075656 WO2014054132A1 (ja) 2012-10-03 2012-10-03 プロペラファン
CN201280076216.5A CN104685218B (zh) 2012-10-03 2012-10-03 螺旋桨式风扇

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2012/075656 WO2014054132A1 (ja) 2012-10-03 2012-10-03 プロペラファン

Publications (1)

Publication Number Publication Date
WO2014054132A1 true WO2014054132A1 (ja) 2014-04-10

Family

ID=50434493

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2012/075656 WO2014054132A1 (ja) 2012-10-03 2012-10-03 プロペラファン

Country Status (5)

Country Link
US (1) US20150204345A1 (de)
EP (1) EP2905474B1 (de)
JP (1) JP5984162B2 (de)
CN (1) CN104685218B (de)
WO (1) WO2014054132A1 (de)

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EP3667098B1 (de) * 2017-08-09 2022-08-03 Mitsubishi Electric Corporation Propellergebläse, gebläse und kältekreislaufvorrichtung
USD910834S1 (en) * 2018-12-05 2021-02-16 Asia Vital Components Co., Ltd. Impeller for a fan
CN111692128B (zh) * 2020-05-21 2021-12-10 西安交通大学 一种跨音压气机组合机匣处理结构

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EP2905474A4 (de) 2016-07-06
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CN104685218B (zh) 2018-03-16
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EP2905474B1 (de) 2019-08-28
US20150204345A1 (en) 2015-07-23

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