TW202009954A - Static electrical machine having outwardly-extended heat dissipation fins and/or heat dissipation hole on the frame device of iron core - Google Patents

Abstract

The present invention discloses a Static electrical machine having outwardly-extended heat dissipation fins and/or heat dissipation hole on the frame device of iron core, in which a frame device is formed with an outwardly-extended heat dissipation fin structure and/or formed with heat dissipation holes at locations defined at adjacent surfaces between the frame device and an iron core with magnetic loops, so that the heat dissipation holes can be served to enlarge the heat dissipation area of the iron core with the magnetic loops disposed in a static electric machine and directly exposed to an ambient gaseous or liquid environment, and the outwardly-extended heat dissipation fins can be served to enlarge the heat dissipation area to the exterior, thereby allowing the heat dissipation performance of the iron core with the magnetic loops, clamped and fastened by the frame device, to the ambient gaseous or liquid environment to be further enhanced,regardless of the ambient gaseous or liquid fluid is flowing or still.

Description

The iron core outer frame device has a static electrical machine (Static electrical machine) with outwardly extending radiating wings and/or radiating holes

The present invention is directed to a winding structure composed of a coil winding, an insulated wire frame (BOBBIN), conductive pins, and wires, and a static motor such as a transformer and an inductor, which is composed of a magnetic circuit iron core and is placed in a gaseous or liquid working environment , Electromagnets, electromagnetic effect linear displacement actuators, or linear back-to-reset movement energy can be converted into power generation electrical energy devices and other electromagnetic effect application devices, an innovative invention "iron core outer frame device with outwardly extending cooling wings and/or cooling holes "Static electrical machine" to improve its heat dissipation performance; for the aforementioned various electromagnetic effect application devices, the magnetic circuit iron core is usually fixed by an outer frame device made of thermally conductive material, which is convenient for assembly or disassembly. The outer frame device installed on the outer core of the magnetic circuit core inevitably forms a shield on the external heat dissipation surface of the magnetic circuit core, so the formed multi-layer structure causes a greater heat transfer thermal resistance, which hinders the external transmission and heat dissipation of the magnetic circuit core and deteriorates Its heat dissipation performance; the present invention "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" is not a rotary motor used for generating revolving energy, but specifically for The structural innovation of the outer frame device of the magnetic circuit iron core applied to the electromagnetic effect application device sandwiched between the stationary motors, the application discloses that the "iron core outer frame device has a static motor with outwardly extending cooling wings and/or cooling holes ( "Static electrical machine)" outer frame device is made of a heat dissipation hole with outwardly extending heat dissipation wing structure and/or provided on the surface of the outer frame device and the magnetic circuit iron core. The heat dissipation hole makes the magnetic circuit iron core of the static motor It can increase the area of direct heat dissipation of the surrounding gaseous or liquid environment, and the outwardly extending heat dissipation wings increase the external heat dissipation surface area, so that when the surrounding gaseous or liquid fluid is flowing or static, it can further enhance the magnetic The heat dissipation performance of the road core to the surrounding gaseous or liquid environment.

Traditionally, it has a winding structure composed of coil windings, insulated wire frames (BOBBIN), conductive pins, and wires for passing current, and an electromagnetic effect application device composed of a magnetic circuit core for passing magnetic flux, such as a static motor. Electromagnetic effect application devices such as transformers, inductors, electromagnetic effect actuators, electromagnets, or bit movement energy forwarding electrical energy output are usually fixed by outer frame devices made of thermally conductive materials. The advantage is that they can effectively fix electromagnetic applications The magnetic circuit core of the device and the protection of its winding structure consisting of coil winding, insulated wire frame (BOBBIN), conductive pins, and wires are missing because the outer frame device greatly shields part of the core's external heat dissipation surface. The deterioration of external heat dissipation performance of the electromagnetic application device is its lack.

As is well known, a static motor is different from a rotary motor. Because the rotary motor itself does not have a rotary function, the cooling fan is driven by the rotating part of the rotary motor to assist in cooling. Therefore, the temperature rise is the natural enemy of the static motor. Efficiency, so providing good heat dissipation performance is an important part of the structure of static motors. Based on the consideration of space occupation, weight and cost, the heat dissipation performance of the low cost and small volume that helps the static motor to radiate, conduct and convection is One of the topics; traditional winding structure consisting of coil windings, insulated bobbin (BOBBIN) and conductive pins and wires for passing current, and electromagnetic effect application device composed of magnetic circuit core for passing magnetic flux, for example Electrostatic effect application devices such as static motors such as transformers, inductors, electromagnetic effect actuators, electromagnets, or bit movement energy forwarding electrical energy output are usually fixed by outer frame devices made of thermally conductive materials. The advantages are: Effectively fix the magnetic circuit iron core of the electromagnetic application device and protect its winding structure composed of coil windings, insulated wire frames (BOBBIN), conductive pins, and wires. The lack of it is because the outer frame device greatly shields part of the iron core from external heat radiation The external heat dissipation performance of the electromagnetic application device is degraded due to its lack; the "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" of the present invention is not provided for generating Rotary motor with revolving energy is a structural innovation for the outer frame device of the magnetic circuit core around the magnetic circuit application device specially designed for the electromagnetic effect sandwiched on the stationary motor. The application discloses that the "iron core outer frame device has outward cooling "Static electrical machine" with wings and/or heat dissipation holes" The outer frame device is a heat dissipation hole made with an outwardly extending heat dissipation wing structure and/or provided on the surface of the outer frame device and the magnetic circuit iron core, The heat dissipation holes enable the magnetic core of the static motor to increase the area of direct heat radiation to the surrounding gaseous or liquid environment, and the outwardly extending heat dissipation wings increase the external heat dissipation surface area, so that the surrounding gaseous or liquid fluid is flowing or static At the same time, all further improve the heat dissipation performance of the magnetic circuit iron core clamped by it to the surrounding gaseous or liquid environment.

101‧‧‧Horizontal (X-X) bridge cooling wing

102‧‧‧longitudinal (Y-Y) bridge cooling wing

103‧‧‧Bending the heat dissipation wings from the outer edge

104‧‧‧Horizontal (X-X) half-bridge heat sink

105‧‧‧ Longitudinal (Y-Y) half-bridge heat sink

106‧‧‧ Oblique bridge cooling wing

107‧‧‧V-shaped bridge cooling wing

111‧‧‧Horizontal (X-X) co-structured heat dissipation holes

112‧‧‧longitudinal (Y-Y) heat dissipation holes

116‧‧‧Diagonal co-structured heat dissipation holes

117‧‧‧V-shaped co-structured cooling holes

120‧‧‧Drain hole

130‧‧‧Ventilation holes

200‧‧‧Outer frame device

300‧‧‧Magnetic core

400‧‧‧winding structure

E‧‧‧Upper side of outer frame device

A, B, C, D

F‧‧‧Left side of outer frame device

G‧‧‧Right side of outer frame device

Rear side of I, J, K, L‧‧‧frame device

H‧‧‧Bottom side of outer frame device

FIG. 1 shows one of the positions on the upper side (E) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes.

Fig. 2 is a diagram showing the position of the front side (A, B, C, D) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes of two.

FIG. 3 shows the third position view of the left side surface (F) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes.

FIG. 4 shows the fourth position view of the right side surface (G) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes.

FIG. 5 is a view showing the position of the rear side (I, J, K, L) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes Fifth.

FIG. 6 shows the sixth position view of the bottom side (H) of the outer frame device (200) of the magnetic circuit iron core (300) of the stationary motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes.

FIG. 7 shows one of the embodiments of the present invention. The outer frame device (200) is provided with at least one lateral (XX) bridge-type heat dissipation fin (101) and an adjacent lateral (XX) co-structured heat dissipation hole (111). view.

FIG. 8 is a top view of FIG. 7.

Fig. 9 is a side view of Fig. 7.

FIG. 10 shows the second embodiment of the present invention. The outer frame device (200) is provided with at least one longitudinal (YY) bridge fin (102) and adjacent longitudinal (YY) co-structured heat dissipation holes (112) view.

FIG. 11 is a top view of FIG. 10.

Fig. 12 is a side view of Fig. 10.

FIG. 13 shows the third embodiment of the present invention. The outer frame device (200) is provided with a plurality of lateral (XX) bridge heat dissipation wings (101) and adjacent lateral (XX) co-construction heat dissipation holes (111) view.

Fig. 14 is a top view of Fig. 13.

Fig. 15 is a side view of Fig. 13.

FIG. 16 shows the fourth embodiment of the present invention. The outer frame device (200) is provided with a plurality of longitudinal (YY) bridge heat dissipation wings (102) and adjacent longitudinal (YY) co-construction heat dissipation holes (112) view.

FIG. 17 is a top view of FIG. 16.

Fig. 18 is a side view of Fig. 16.

FIG. 19 shows a fifth embodiment of the present invention. The outer frame device (200) has lateral (XX) bridge-type heat dissipation wings (101) and adjacent lateral (XX) co-structured heat dissipation holes (111). (XX) Front view of the bridge-type heat dissipation fin (101) with at least one drain hole (120).

FIG. 20 is a top view of FIG. 19.

21 is a side view of FIG. 19.

22 shows the sixth embodiment of the present invention, the outer frame device (200) has a longitudinal (YY) bridge-type heat dissipation fin (102) and an adjacent longitudinal (YY) heat dissipation hole (112), and its longitudinal (YY) Front view of the bridge fins (102) with at least one drain hole (120).

Fig. 23 is a top view of Fig. 22.

Fig. 24 is a side view of Fig. 22.

Fig. 25 shows the seventh embodiment of the present invention. The outer frame device (200) is a front view of at least one oblique bridge fin (106) and adjacent oblique co-structured heat dissipation holes (116).

FIG. 26 is a top view of FIG. 25.

FIG. 27 is a side view of FIG. 25.

FIG. 28 shows an eighth embodiment of the present invention. The outer frame device (200) is a front view of at least one V-shaped bridge heat dissipation fin (107) and an adjacent V-shaped structured heat dissipation hole (117).

FIG. 29 is a top view of FIG. 28.

30 is a side view of FIG. 28.

FIG. 31 shows the ninth embodiment of the present invention. The outer frame device (200) is a plurality of lateral (XX) half-bridge heat dissipation wings (104) and adjacent lateral (XX) co-structured heat dissipation holes (111) Front view.

FIG. 32 is a top view of FIG. 31.

FIG. 33 is a side view of FIG. 31.

Fig. 34 shows the tenth embodiment of the present invention, the outer frame device (200) is a plurality of longitudinal (YY) half-bridge heat dissipation wings (105) and adjacent longitudinal (YY) co-structured heat dissipation holes (112) Front view.

FIG. 35 is a top view of FIG. 34.

Fig. 36 is a side view of Fig. 34.

FIG. 37 shows that the outer frame device (200) of the present invention is provided with a plurality of lateral (XX) half-bridge heat dissipation wings (104) and adjacent lateral (XX) co-structured heat dissipation holes (111) arranged on the same side Schematic diagram of an embodiment.

FIG. 38 shows that the outer frame device (200) of the present invention has a plurality of lateral (XX) half-bridge heat dissipation wings (104) staggered on different sides and adjacent lateral (XX) co-structured heat dissipation holes (111) ) Of the embodiment schematic.

FIG. 39 shows an eleventh embodiment of the present invention. The outer frame device (200) is provided with at least one lateral (XX) half-bridge heat sink (104) arranged in multiple rows on the same side and the adjacent lateral (XX) ) Front view of the co-construction heat dissipation hole (111).

FIG. 40 is a top view of FIG. 39.

FIG. 41 is a side view of FIG. 39.

FIG. 42 shows the twelfth embodiment of the present invention. The outer frame device (200) is provided with at least one horizontal (XX) half-bridge heat dissipating wing (104) arranged in multiple rows on different sides and adjacent horizontal (XX) ) Front view of the co-construction heat dissipation hole (111).

FIG. 43 is a top view of FIG. 42.

FIG. 44 is a side view of FIG. 42.

FIG. 45 shows the thirteenth embodiment of the present invention, the outer frame device (200) and at least one of the outer edges of the surface of the iron core of the stationary motor, with the cooling fins (103) bent outward from the outer edge Example front view.

FIG. 46 is a top view of FIG. 45.

Fig. 47 is a side view of Fig. 45.

Fig. 48 shows the fourteenth embodiment of the present invention, the outer frame device (200) and at least one of the outer edges of the surface of the iron core of the stationary motor, and the heat dissipation wings (103) bent outward from the outer edge and Front view of an embodiment with a multi-fold structure.

FIG. 49 is a top view of FIG. 48.

FIG. 50 is a side view of FIG. 48.

FIG. 51 shows the fifteenth embodiment of the present invention, the outer frame device (200) has longitudinal (YY) bridge-type heat dissipation wings (102) and adjacent longitudinal (YY) co-construction heat dissipation holes (112), and its The outer frame device (200) and at least one of the outer edges of the fitting surface of the iron core of the stationary motor have a front view of an embodiment in which the heat dissipation wings (103) are bent outward from the outer edge and have a multi-folded structure.

FIG. 52 is a top view of FIG. 51.

Fig. 53 is a side view of Fig. 51.

FIG. 54 shows a sixteenth embodiment of the present invention, the outer frame device (200) has longitudinal (YY) bridge-type heat dissipation wings (102) and adjacent longitudinal (YY) co-construction heat dissipation holes (112), and its The longitudinal (YY) bridge-type heat dissipation wing (102) has at least one drain hole (120), and at least one of its outer frame device (200) and at least one of the outer edges of the fitting surface of the static motor iron core, with the outer edge facing The front view of the embodiment of the heat-radiating wing (103) bent outwards and having a multi-folded structure.

FIG. 55 is a top view of FIG. 54.

Fig. 56 is a side view of Fig. 54.

Fig. 57 shows at least one of the bonding surfaces of the outer frame device (200) of the static motor iron core and the magnetic circuit core (300) of the present invention, with a square shape for the magnetic circuit core (300) to directly radiate outward Front view of the embodiment of the heat dissipation hole (130).

FIG. 58 is a top view of FIG. 57.

FIG. 59 is a side view of FIG. 57.

Fig. 60 shows the horizontal (XX) of various heat dissipation holes of the outer frame device (200) of the stationary motor iron core of the present invention and the magnetic circuit iron core (300) for the magnetic circuit iron core (300) to directly radiate to the outside Figures showing the shape of the heat dissipation holes (111), longitudinal (YY) co-configuration heat dissipation holes (112), diagonal co-configuration heat dissipation holes (116), V-shaped co-structure heat dissipation holes (117), and heat dissipation holes (130).

FIG. 61 shows the seventeenth embodiment of the present invention. The outer frame device (200) is a lateral (XX) bridge-type heat dissipation fin (101) and an adjacent lateral (XX) co-structured heat dissipation hole (111). The horizontal (XX) bridge type heat dissipation wing (101) has at least one drain hole (120), and the outer frame device (200) and the magnetic circuit iron core (300) fit the mask for the magnetic circuit iron core (300) to directly dissipate heat Front view of the heat dissipation hole (130).

FIG. 62 is a top view of FIG. 61.

Fig. 63 is a side view of Fig. 61.

Fig. 64 shows an eighteenth embodiment of the present invention. The outer frame device (200) is a longitudinal (YY) bridge-type heat dissipation fin (102) and an adjacent longitudinal (YY) co-structured heat dissipation hole (112). The longitudinal (YY) bridge-type heat dissipation wing (102) has at least one drain hole (120), and its outer frame device (200) and the magnetic circuit core (300) are attached to the mask for the magnetic circuit core (300) to directly dissipate heat Front view of the heat dissipation hole (130).

FIG. 65 is a top view of FIG. 64.

Fig. 66 is a side view of Fig. 64.

Fig. 67 shows the nineteenth embodiment of the present invention, and the outer frame device (200) is a at least one transverse (XX) half-bridge heat dissipation wing (104) and an adjacent transverse (XX) radiating hole (111) ), the outer frame device (200) and the magnetic circuit core (300) are attached to the front surface of the heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat to the outside.

FIG. 68 is a top view of FIG. 67.

Fig. 69 is a side view of Fig. 67.

Fig. 70 shows the twentieth embodiment of the present invention, the outer frame device (200) is a at least one longitudinal (YY) half-bridge heat sink (105) and adjacent longitudinal (YY) co-structured heat dissipation holes (112) ), the outer frame device (200) and the magnetic circuit core (300) are attached to the front view of the rectangular slot-shaped heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat outward.

FIG. 71 is a top view of FIG. 70.

72 is a side view of FIG. 70.

Traditionally, it has a winding structure composed of coil windings, insulated wire frames (BOBBIN), conductive pins, and wires for passing current, and an electromagnetic effect application device composed of a magnetic circuit core for passing magnetic flux, such as a static motor. Electromagnetic effect application devices such as transformers, inductors, electromagnetic effect actuators, electromagnets, or bit movement energy forwarding electrical energy output are usually fixed by outer frame devices made of thermally conductive materials. The advantage is that they can effectively fix electromagnetic applications The magnetic circuit core of the device and the protection of its winding structure consisting of coil winding, insulated wire frame (BOBBIN), conductive pins, and wires are missing because the outer frame device greatly shields part of the core's external heat dissipation surface. The deterioration of external heat dissipation performance of the electromagnetic application device is its lack.

The present invention is directed to a winding structure composed of a coil winding, an insulated wire frame (BOBBIN), conductive pins, and wires, and a static motor such as a transformer and an inductor, which is composed of a magnetic circuit iron core and is placed in a gaseous or liquid working environment , Electromagnets, electromagnetic effect linear displacement actuators, or linear back-to-return movement energy can be converted into power generation electrical energy devices and other electromagnetic effect application devices, an innovative invention "iron core outer frame device with outwardly extending cooling wings and/or cooling holes "Static electrical machine" to improve its heat dissipation performance; for the aforementioned various electromagnetic effect application devices, the magnetic circuit iron core is usually fixed by an outer frame device made of thermally conductive material, which is convenient for assembly or disassembly. The outer frame device installed on the outer core of the magnetic circuit core inevitably forms a shield on the external heat dissipation surface of the magnetic circuit core, so the formed multi-layer structure causes a greater heat transfer thermal resistance, which hinders the external transmission and heat dissipation of the magnetic circuit core and deteriorates Its heat dissipation performance.

The present invention “the static electrical machine with iron core outer frame device with outwardly extending radiating fins and/or radiating holes” does not supply a rotary motor for generating revolving energy, but is specifically designed for a stationary clamp Of the electromagnetic effect application device of the built-in motor. The structural innovation of the outer frame device of the magnetic circuit iron core is disclosed in the application. "The outer frame device of the iron core has a static electrical machine (Static electrical machine) with outwardly extending heat dissipation wings and/or heat dissipation holes. ”The outer frame device is made with outwardly extending heat dissipation wing structure and/or a heat dissipation hole provided on the surface of the outer frame device and the magnetic circuit iron core. The heat dissipation hole allows the magnetic circuit iron core of the stationary motor to increase its The area of the surrounding gaseous or liquid environment directly exposed to heat dissipation, and the outwardly extending heat dissipation wings increase the external heat dissipation surface area, so that when the surrounding gaseous or liquid fluid is flowing or static, it further enhances the clamped magnetic circuit iron core pair The heat dissipation performance of the surrounding gaseous or liquid environment.

The subject disclosed in this case refers to an application device for electromagnetic effects, such as transformers, inductors, electromagnetic effect actuators, electromagnets, or mobile energy forwarding electrical energy output, which is sandwiched between stationary motors. The three-dimensional polygonal magnetic circuit core (300) structure formed by laminating the magnetic core (300), or various three-dimensional shapes composed of sintered bulk magnetic powder cores.

The following is an example of the outer frame device (200) used for the stationary motor iron core composed of an approximately square cube or rectangular cube magnetic circuit core (300) with the most common peripherals having six surfaces and the most widely used. The location of the heat dissipation holes provided for the outwardly extending heat dissipation wing structure and/or the attachment surface of the outer frame device (200) and the magnetic circuit core (300) is described as follows: FIG. 1 shows the static type of the invention On the outer frame device (200) of the magnetic circuit iron core (300) of the motor

The side (E) is one of the positions of the heat dissipation wings and/or heat dissipation holes.

Fig. 2 is a diagram showing the position of the front side (A, B, C, D) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes of two.

FIG. 3 shows the third position view of the left side surface (F) of the outer frame device (200) of the magnetic circuit core (300) of the stationary motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes.

FIG. 4 shows the fourth position view of the right side surface (G) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes.

FIG. 5 is a view showing the position of the rear side (I, J, K, L) of the outer frame device (200) of the magnetic circuit core (300) of the static motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes Fifth.

FIG. 6 shows the sixth position view of the bottom side (H) of the outer frame device (200) of the magnetic circuit iron core (300) of the stationary motor of the present invention for providing outwardly extending heat dissipation wings and/or heat dissipation holes.

As shown in FIGS. 1 to 6, when the present invention is applied to the above-mentioned magnetic circuit core (300) sandwiched between an approximately square cube or a rectangular cube, it is specifically provided with outwardly extending heat dissipation wings and/or heat dissipation holes (130) ), the outer frame device (200) is sandwiched between the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the magnetic circuit core (300) structure at least A, B, C, D , E, F, G, H, I, J, K, L at least one of the positions; when the outer frame device (200) is used to form the external locking function of the stationary motor, the bottom is for combining with the fixed When it is covered by the fixed surface, it can be elastically considered whether to provide outwardly extending heat dissipation wings and/or heat dissipation holes (130), and at least one of the remaining surfaces of the outer frame device (200) is provided with outward heat dissipation Wings and/or heat dissipation holes (130).

When the static motor is placed in the air, at least one of the surfaces of the outer frame device (200) for clamping the magnetic circuit core (300) of the static motor and at least one of the surfaces of the outer shell device is provided with outwardly extending cooling wings and/or Heat sink (130).

The above "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" consists of:-Winding structure (400): including coil windings and insulated wire racks (BOBBIN) structure, externally conductive pins or wires, for installation on the magnetic circuit core (300); - magnetic circuit core (300): made of magnetically conductive material, including sheets The magnetically permeable materials are superimposed, or are made of bulk magnetically permeable materials, or are made of sintered magnetically conductive powder materials to form the magnetic circuit iron core (300) of the stationary motor for the winding structure (400); --Outer frame device (200): Outer frame device (200) made of thermally conductive material with outwardly extending heat dissipation wings and/or heat dissipation holes for clamping to the magnetic circuit core (300); The structure is composed of static motors such as transformers, inductors, electromagnets, electromagnetic-effect linear displacement actuators, or linear-to-reset movement energy-generating electrical energy conversion devices and other electromagnetic effect application devices, which are characterized by being clamped to a static motor The outer frame device (200) of the magnetic circuit core (300) is made of a thermally conductive material with an outwardly extending heat dissipation wing structure to increase the external heat dissipation surface area and/or has the outer frame device (200) and the magnetic circuit core ( 300) The heat dissipation holes on the mating surface for the magnetic circuit core (300) of the static motor to increase the area of direct heat radiation to the surrounding gaseous or liquid environment. When the surrounding gaseous or liquid fluid is flowing or static , Can improve the heat dissipation performance of the magnetic circuit iron core (300) clamped to the surrounding gas or liquid environment; as mentioned above, the application "iron core outer frame device has outwardly extending heat dissipation wings and/or heat dissipation "Static electrical machine", the outer frame device (200) has outwardly extending heat dissipation wings and/or heat dissipation holes for the magnetic circuit core (300) to directly dissipate heat to form a lifting magnetic circuit core (300) An optimized structure for the heat transfer performance of the surrounding gaseous or liquid environment, in which the outer frame device (200) has outwardly extending heat dissipation wings and/or heat dissipation holes for the magnetic circuit iron core to directly dissipate heat. More than one type: (1) horizontal (XX) bridge-type cooling fins (101); (2) longitudinal (YY) bridge-type cooling fins (102); (3) bending the cooling fins (103) outward from the outer edge; 4) Lateral (XX) half-bridge heat sink (104); (5) Longitudinal (YY) half-bridge heat sink (105); (6) Oblique bridge heat sink (106); (7) V-shaped bridge Type heat dissipation wing (107); (8) horizontal (XX) co-configuration heat dissipation hole (111); (9) longitudinal (YY) co-configuration heat dissipation hole (112); (10) oblique co-configuration heat dissipation hole (116); (11) V-shaped co-structured heat dissipation holes (117); and (12) The bonding surface of the outer frame device (200) and the magnetic circuit core (300) is provided for the magnetic circuit core (300) to directly dissipate heat Hole (1 30).

This "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" can be used for various outward heat dissipation wings and/or disclosed above according to application requirements The heat dissipation holes for the magnetic circuit core to directly dissipate heat are made into a selected combination of structures. The following examples are used to illustrate, the examples are only for assistance, not for limitation; Figure 7 shows the implementation of the invention In one example, the outer frame device (200) is a front view of at least one lateral (XX) bridge-type heat dissipation fin (101) and adjacent lateral (XX) co-structured heat dissipation holes (111).

FIG. 8 is a top view of FIG. 7.

Fig. 9 is a side view of Fig. 7.

As shown in Figures 7-9, the outer frame device (200) of the stationary motor iron core formed by the magnetic circuit core (300) of an approximately square cube or rectangular cube is used as an example. At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) at least one horizontal (XX) bridge cooling fin (101) and the adjacent lateral (XX) configuration Heat dissipation holes (111) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 10 shows the second embodiment of the present invention. The outer frame device (200) is provided with at least one longitudinal (YY) bridge fin (102) and adjacent longitudinal (YY) co-structured heat dissipation holes (112) view.

FIG. 11 is a top view of FIG. 10.

Fig. 12 is a side view of Fig. 10.

As shown in FIGS. 10-12, the outer frame device (200) of a stationary motor iron core formed by a magnetic core (300) that is approximately a square cube or a rectangular cube is used as an example. At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) at least one longitudinal (YY) bridge fin (102) and the adjacent longitudinal (YY) configuration Heat dissipation holes (112) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 13 shows the third embodiment of the present invention. The outer frame device (200) is provided with a plurality of lateral (XX) bridge heat dissipation wings (101) and adjacent lateral (XX) co-construction heat dissipation holes (111) view.

Fig. 14 is a top view of Fig. 13.

Fig. 15 is a side view of Fig. 13.

As shown in FIGS. 13-15, it is an example of an outer frame device (200) applied to the periphery of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) is composed of a plurality of lateral (XX) bridge heat dissipation wings (101) and adjacent lateral (XX) Heat dissipation holes (111) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 16 shows the fourth embodiment of the present invention. The outer frame device (200) is provided with a plurality of longitudinal (YY) bridge heat dissipation wings (102) and adjacent longitudinal (YY) co-construction heat dissipation holes (112) view.

FIG. 17 is a top view of FIG. 16.

Fig. 18 is a side view of Fig. 16.

As shown in Figures 16 to 18, it is an example of an outer frame device (200) applied to the periphery of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) is constructed with a plurality of longitudinal (YY) bridge fins (102) and adjacent longitudinal (YY) Heat dissipation holes (112) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 19 shows a fifth embodiment of the present invention. The outer frame device (200) has lateral (XX) bridge-type heat dissipation wings (101) and adjacent lateral (XX) co-structured heat dissipation holes (111). (XX) Front view of the bridge-type heat dissipation fin (101) with at least one drain hole (120).

FIG. 20 is a top view of FIG. 19.

21 is a side view of FIG. 19.

As shown in Figs. 19-21, the outer frame device (200) of the stationary motor iron core formed by the magnetic core (300) of an approximately square cube or rectangular cube is used as an example. At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) is a horizontal (XX) bridge-type cooling wing (101) and an adjacent lateral (XX) joint cooling hole (111), and its lateral (XX) bridge fins (101) have at least one drain hole (120) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

22 shows the sixth embodiment of the present invention, the outer frame device (200) has a longitudinal (YY) bridge-type heat dissipation fin (102) and an adjacent longitudinal (YY) heat dissipation hole (112), and its longitudinal (YY) Front view of the bridge fins (102) with at least one drain hole (120).

Fig. 23 is a top view of Fig. 22.

Fig. 24 is a side view of Fig. 22.

As shown in FIGS. 22 to 24, the outer frame device (200) of the stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example, and its characteristics are: At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) is a longitudinal (YY) bridge fin (102) and an adjacent longitudinal (YY) joint cooling hole (112), and its longitudinal (YY) bridge fins (102) have at least one drain hole (120) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

The aforementioned bridge-type heat dissipation wing may further be composed of a diagonal or V-shaped bridge heat dissipation wing structure and a co-structured heat dissipation hole, which are described as follows: FIG. 25 shows the seventh embodiment of the present invention, and its outer frame device (200 ) Is a front view of at least one oblique bridge-type heat dissipation fin (106) and adjacent oblique co-configuration heat dissipation holes (116).

FIG. 26 is a top view of FIG. 25.

FIG. 27 is a side view of FIG. 25.

As shown in FIGS. 25 to 27, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example. At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200), at least one oblique bridge heat dissipation wing (106), and the adjacent oblique co-structured heat dissipation holes (116) ) To improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 28 shows an eighth embodiment of the present invention. The outer frame device (200) is a front view of at least one V-shaped bridge heat dissipation fin (107) and an adjacent V-shaped structured heat dissipation hole (117).

FIG. 29 is a top view of FIG. 28.

30 is a side view of FIG. 28.

As shown in FIGS. 28 to 30, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example, and its characteristics are: At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200), at least one V-shaped bridge fin (107) and the adjacent V-shaped radiating holes (117) ) To improve the heat dissipation performance of the surrounding gaseous or liquid environment.

This "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" can be further composed of half-bridge heat dissipation wings and conformal heat dissipation hole structures; As follows: FIG. 31 shows the ninth embodiment of the present invention, and its outer frame device (200) is a plurality of lateral (XX) half-bridge heat dissipation wings (104) and adjacent lateral (XX) co-structured heat dissipation holes ( 111) Front view.

FIG. 32 is a top view of FIG. 31.

FIG. 33 is a side view of FIG. 31.

As shown in FIGS. 31 to 33, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example, and its characteristics are: At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) includes a plurality of lateral (XX) half-bridge heat dissipation wings (104) and adjacent lateral (XX) Construct heat dissipation holes (111) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

Fig. 34 shows the tenth embodiment of the present invention, the outer frame device (200) is a plurality of longitudinal (YY) half-bridge heat dissipation wings (105) and adjacent longitudinal (YY) co-structured heat dissipation holes (112) Front view.

FIG. 35 is a top view of FIG. 34.

Fig. 36 is a side view of Fig. 34.

As shown in FIGS. 34 to 36, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example, and its characteristics are: At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) includes a plurality of longitudinal (YY) half-bridge cooling wings (105) and adjacent longitudinal (YY) Construct heat dissipation holes (112) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

The static electric machine (Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes) described in the aforementioned FIGS. 31 to 36, the arrangement of the half bridge heat dissipation wings includes the same side The arrangement or staggered arrangement on different sides; here is an example as follows: FIG. 37 shows the outer frame device (200) of the present invention is provided with a plurality of lateral (XX) half-bridge cooling fins (104) and phases arranged on the same side A schematic diagram of an embodiment of adjacent lateral (XX) co-construction heat dissipation holes (111).

As shown in FIG. 37, the outer frame device (200) applied to the periphery of the stationary motor core formed by the magnetic circuit core (300) of an approximately square cube or rectangular cube is used as an example. 200) At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side has a plurality of lateral (XX) half-bridge heat dissipation wings (104) and adjacent lateral (XX) heat dissipation The holes (111) and the adjacent horizontal (XX) half-bridge heat dissipation wings (104) are arranged on the same side to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 38 shows that the outer frame device (200) of the present invention has a plurality of lateral (XX) half-bridge heat dissipation wings (104) staggered on different sides and adjacent lateral (XX) co-structured heat dissipation holes (111) ) Of the embodiment schematic.

As shown in FIG. 38, the outer frame device (200) applied to the periphery of the stationary motor iron core composed of an approximately square cube or rectangular cube magnetic circuit core (300) is taken as an example. 200) At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side has a plurality of lateral (XX) half-bridge heat dissipation wings (104) and adjacent lateral (XX) heat dissipation holes (111), each adjacent horizontal (XX) half-bridge heat dissipation wing (104) is staggered on different sides to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 39 shows an eleventh embodiment of the present invention. The outer frame device (200) is provided with at least one lateral (XX) half-bridge heat sink (104) arranged in multiple rows on the same side and the adjacent lateral (XX) ) Front view of the co-construction heat dissipation hole (111).

FIG. 40 is a top view of FIG. 39.

FIG. 41 is a side view of FIG. 39.

As shown in FIGS. 39 to 41, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit iron core (300) is used as an example. At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) and at least one horizontal (XX) half-bridge heat dissipation wing (104) and phases arranged in multiple rows on the same side The adjacent lateral (XX) co-constructed heat dissipation holes (111) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 42 shows the twelfth embodiment of the present invention. The outer frame device (200) is provided with at least one horizontal (XX) half-bridge heat dissipating wing (104) arranged in multiple rows on different sides and adjacent horizontal (XX) ) Front view of the co-construction heat dissipation hole (111).

FIG. 43 is a top view of FIG. 42.

FIG. 44 is a side view of FIG. 42.

As shown in FIGS. 42-44, it is an example of an outer frame device (200) applied to the periphery of a stationary motor iron core composed of an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) and at least one horizontal (XX) half-bridge heat dissipation wing (104) and phases arranged in multiple rows on different sides The adjacent lateral (XX) co-constructed heat dissipation holes (111) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

This item "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" is further characterized in that at least one of its outer frame device (200) and the static motor iron core One of the outer edges of the fitting surface, with the heat dissipation wings (103) bent outward from the outer edge; the following is an example: Figure 45 shows the thirteenth embodiment of the present invention, the outer frame device (200) and the static At least one of the outer edges of the fitting surface of the motor iron core has a front view of an embodiment in which the cooling fin (103) is bent outward from the outer edge.

FIG. 46 is a top view of FIG. 45.

Fig. 47 is a side view of Fig. 45.

As shown in FIGS. 45 to 47, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example, and its characteristics are: At least one of the upper side, the front side, the left side, the right side, the rear side, the bottom side and the outer edge of the surface of the static motor iron core fitting surface of the frame device (200), with the heat dissipation flexing outward from the outer edge ( 103), to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

Fig. 48 shows the fourteenth embodiment of the present invention, the outer frame device (200) and at least one of the outer edges of the surface of the iron core of the stationary motor, and the heat dissipation wings (103) bent outward from the outer edge and Front view of an embodiment with a multi-fold structure.

FIG. 49 is a top view of FIG. 48.

FIG. 50 is a side view of FIG. 48.

As shown in FIGS. 48 to 50, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example, and its characteristics are: At least one of the upper side, the front side, the left side, the right side, the rear side, the bottom side and the outer edge of the surface of the static motor iron core fitting surface of the frame device (200), with the heat dissipation flexing outward from the outer edge ( 103) And it has a multi-fold structure to further increase its heat dissipation area to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 51 shows the fifteenth embodiment of the present invention, the outer frame device (200) has longitudinal (YY) bridge-type heat dissipation wings (102) and adjacent longitudinal (YY) co-construction heat dissipation holes (112), and its The outer frame device (200) and at least one of the outer edges of the fitting surface of the iron core of the stationary motor have a front view of an embodiment in which the heat dissipation wings (103) are bent outward from the outer edge and have a multi-folded structure.

FIG. 52 is a top view of FIG. 51.

Fig. 53 is a side view of Fig. 51.

As shown in FIGS. 51-53, it is an example of an outer frame device (200) applied to the periphery of a stationary motor iron core composed of an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) is a longitudinal (YY) bridge fin (102) and an adjacent longitudinal (YY) joint cooling hole (112), and at least one of the upper side, the front side, the left side, the right side, the rear side, the bottom side and the outer surface of the outer surface of the outer frame device (200) and the static motor core contact surface, with the outer edge Bending the heat dissipation wing (103) outward and presenting a multi-fold structure to further increase its heat dissipation area to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 54 shows a sixteenth embodiment of the present invention, the outer frame device (200) has longitudinal (YY) bridge-type heat dissipation wings (102) and adjacent longitudinal (YY) co-construction heat dissipation holes (112), and its The longitudinal (YY) bridge-type heat dissipation wing (102) has at least one drain hole (120), and at least one of its outer frame device (200) and at least one of the outer edges of the fitting surface of the static motor iron core, with the outer edge facing The front view of the embodiment of the heat-radiating wing (103) bent outwards and having a multi-folded structure.

FIG. 55 is a top view of FIG. 54.

Fig. 56 is a side view of Fig. 54.

As shown in FIGS. 54-56, it is an example of an outer frame device (200) applied to the periphery of a stationary motor iron core composed of an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the frame device (200) is a longitudinal (YY) bridge fin (102) and an adjacent longitudinal (YY) joint cooling hole (112), and its longitudinal (YY) bridge fins (102) have at least one drain hole (120), and the upper side, front side, left side, right side, rear side of its outer frame device (200) 、At least one of the outer edge of the bottom side and the surface of the iron core of the stationary motor, which has a heat dissipation wing (103) bent outward from the outer edge and has a multi-fold structure to further increase its heat dissipation area to enhance its surroundings The heat dissipation performance of gaseous or liquid environment.

This item "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" in addition to the horizontal (XX) bridge heat dissipation wings (101) or horizontal (XX) half bridge type Radiating fins (104) and adjacent lateral (XX) framing holes (111), longitudinal (YY) bridge cooling fins (102) or longitudinal (YY) half-bridge cooling fins (105) and adjacent longitudinal (YY) Co-structured heat dissipation holes (112), diagonal bridge fins (106) and adjacent diagonal co-structured heat dissipation holes (116), V-shaped bridge fins (107) and adjacent V-shaped heat dissipation The structure of the heat dissipation hole (117) constitutes the function for the magnetic circuit core (300) to directly dissipate heat. The further feature is that it can be installed in the outer frame device (200) of the static motor core and the magnetic circuit core (300). At least one of them fits the mask square or rectangular type heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat; the following examples are illustrated: Figure 57 shows the core of the static motor of the present invention At least one of the bonding surfaces of the frame device (200) and the magnetic circuit core (300) has a front view of an embodiment of a heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat outward.

FIG. 58 is a top view of FIG. 57.

FIG. 59 is a side view of FIG. 57.

As shown in FIGS. 57 to 59, the outer frame device (200) of a stationary motor iron core formed by a magnetic circuit core (300) composed of an approximately square cube or a rectangular cube is used as an example. Type motor iron core outer frame device (200) at least one of the upper side, front side, left side, right side, rear side, bottom side and the magnetic circuit core (300) bonding surface, with magnetic circuit The iron core (300) directly dissipates heat to form a square heat dissipation hole (130) to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

Fig. 60 shows the horizontal (XX) of various heat dissipation holes of the outer frame device (200) of the stationary motor iron core of the present invention and the magnetic circuit iron core (300) for the magnetic circuit iron core (300) to directly radiate to the outside Figures showing the shape of the heat dissipation holes (111), longitudinal (YY) co-configuration heat dissipation holes (112), diagonal co-configuration heat dissipation holes (116), V-shaped co-structure heat dissipation holes (117), and heat dissipation holes (130).

As shown in FIG. 60, the outer frame device (200) applied to the periphery of the stationary motor iron core formed by the magnetic circuit core (300) of an approximately square cube or rectangular cube is used as an example. The bonding surface of the core outer frame device (200) and at least one of the magnetic circuit cores (300) may be further formed by various arc-shaped heat dissipation holes and/or polygonal heat dissipation holes, as shown in FIG. 60 for example The various heat dissipation holes are horizontal (XX) co-configuration heat dissipation holes (111), vertical (YY) co-configuration heat dissipation holes (112), oblique co-configuration heat dissipation holes (116), V-shaped co-configuration heat dissipation holes (117), heat dissipation holes (130) The shape includes a hole shape or a slot-shaped hole shape; for example: (a) circular heat dissipation holes; (b) oval heat dissipation holes; (c) semicircular heat dissipation holes; (d) triangular heat dissipation holes; ( e) Four-corner heat dissipation holes; (f) Pentagonal heat dissipation holes; (g) Hexagonal heat dissipation holes; (h) Seven-corner heat dissipation holes; (i) Octagonal heat dissipation holes; (j) Diamond-shaped heat dissipation holes; (k) Oblique Heat dissipation holes; (l) V-shaped heat dissipation holes; (m) star-shaped heat dissipation holes; (n) rectangular elliptical slot-shaped heat dissipation holes with convex arcs on both sides; (o) rectangular slot-shaped hole Heat dissipation holes; (p) At least one side has a tooth-shaped heat dissipation hole and other geometric shape hole structures, and is composed of at least one of them; the above examples (a) ~ (p) shape is not limited, only For example.

The application "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" is characterized in that the outer frame device (200) has outwardly extending heat dissipation wings and/or The heat dissipation holes for the magnetic circuit core (300) to directly dissipate heat form an optimized structure for improving the heat transmission performance of the magnetic circuit core (300) to the surrounding gaseous or liquid environment, in which the outer frame device (200) has outwardly extending The heat dissipation wing and/or the heat dissipation hole for direct heat dissipation of the magnetic circuit core contains one or more of the following: (1) horizontal (XX) bridge type heat dissipation wings (101); (2) longitudinal (YY) bridge type heat dissipation wings ( 102); (3) Bending the heat dissipation wings (103) from the outer edge; (4) Transverse (XX) half-bridge heat dissipation wings (104); (5) Longitudinal (YY) half-bridge heat dissipation wings (105) ; (6) diagonal bridge fins (106); (7) V-shaped bridge fins (107); (8) lateral (XX) co-constructed cooling holes (111); (9) longitudinal (YY) total Structured heat dissipation holes (112); (10) Oblique co-structured heat dissipation holes (116); (11) V-shaped co-structured heat dissipation holes (117); and (12) Outer frame device (200) and magnetic circuit core (300) ) Is provided with a heat dissipation hole (130) for the magnetic circuit iron core (300) to directly dissipate heat.

This "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" can be further installed on the magnetic iron of the static motor by one or more of the above heat dissipation structures as required At least one of the upper side, the front side, the left side, the right side, the rear side, and the bottom side of the outer frame device (200) of the core (300) and the number required for the installation, here are the following embodiments To illustrate, the embodiments are for illustration rather than to limit the structure type and number of outwardly extending heat dissipation wings and/or the shape and number of heat dissipation holes.

FIG. 61 shows the seventeenth embodiment of the present invention. The outer frame device (200) is a lateral (XX) bridge-type heat dissipation fin (101) and an adjacent lateral (XX) co-structured heat dissipation hole (111). The horizontal (XX) bridge type heat dissipation wing (101) has at least one drain hole (120), and the outer frame device (200) and the magnetic circuit iron core (300) fit the mask for the magnetic circuit iron core (300) to directly dissipate heat Front view of the heat dissipation hole (130).

FIG. 62 is a top view of FIG. 61.

Fig. 63 is a side view of Fig. 61.

As shown in FIGS. 61 to 63, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example, and its characteristics are: The frame device (200) is a lateral (XX) bridge type heat dissipation wing (101) and an adjacent lateral (XX) co-structured heat dissipation hole (111), and the lateral (XX) bridge type heat dissipation wing (101) has at least one vent The flow hole (120), the outer frame device (200) and the magnetic circuit core (300) are attached to the mask, and the heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat to improve the gas or liquid around it The heat dissipation performance of the environment.

Fig. 64 shows an eighteenth embodiment of the present invention. The outer frame device (200) is a longitudinal (YY) bridge-type heat dissipation fin (102) and an adjacent longitudinal (YY) co-structured heat dissipation hole (112). The longitudinal (YY) bridge-type heat dissipation wing (102) has at least one drain hole (120), and its outer frame device (200) and the magnetic circuit core (300) are attached to the mask for the magnetic circuit core (300) to directly dissipate heat Front view of the heat dissipation hole (130).

FIG. 65 is a top view of FIG. 64.

Fig. 66 is a side view of Fig. 64.

As shown in FIGS. 64 to 66, the outer frame device (200) of the stationary motor iron core formed by the magnetic core (300) of an approximately square cube or rectangular cube is used as an example. The outer frame device (200) is a longitudinal (YY) bridge type heat dissipation wing (102) and an adjacent longitudinal (YY) structured heat dissipation hole (112), and the longitudinal (YY) bridge type heat dissipation wing (102) has at least one The drain hole (120), the outer frame device (200) and the magnetic circuit core (300) are attached to the heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat, so as to enhance the gas state or The heat dissipation performance of the liquid environment.

Fig. 67 shows the nineteenth embodiment of the present invention, and the outer frame device (200) is a at least one transverse (XX) half-bridge heat dissipation wing (104) and an adjacent transverse (XX) radiating hole (111) ), the outer frame device (200) and the magnetic circuit core (300) are attached to the front surface of the heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat to the outside.

FIG. 68 is a top view of FIG. 67.

Fig. 69 is a side view of Fig. 67.

As shown in FIGS. 67 to 69, the outer frame device (200) of a stationary motor iron core formed by an approximately square cube or rectangular cube magnetic circuit core (300) is used as an example. The frame device (200) has at least one lateral (XX) half-bridge heat dissipation wing (104) and adjacent lateral (XX) co-structured heat dissipation holes (111), and its outer frame device (200) and magnetic circuit core ( 300) A cooling hole (130) that fits the mask for the magnetic circuit core (300) to directly dissipate heat to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

Fig. 70 shows the twentieth embodiment of the present invention, the outer frame device (200) is a at least one longitudinal (YY) half-bridge heat sink (105) and adjacent longitudinal (YY) co-structured heat dissipation holes (112) ), the outer frame device (200) and the magnetic circuit core (300) are attached to the front view of the rectangular slot-shaped heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat outward.

FIG. 71 is a top view of FIG. 70.

72 is a side view of FIG. 70.

As shown in FIGS. 70-72, the outer frame device (200) of the stationary motor iron core formed by the magnetic circuit core (300) of an approximately square cube or rectangular cube is used as an example. The frame device (200) is a heat dissipation hole (112) with at least one longitudinal (YY) half-bridge heat dissipation fin (105) and an adjacent longitudinal (YY) structure, and the outer frame device (200) and the magnetic circuit iron core (200) 300) A rectangular slot-shaped heat dissipation hole (130) for the magnetic circuit iron core (300) to directly dissipate heat to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

Application "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes" Applications include heat dissipation heat dissipation wings and/or heat dissipation holes made of thermally conductive material Outer frame device for clamping the winding structure composed of coil winding, insulated wire frame (BOBBIN) and conductive pins and wires and the static motor composed of magnetic circuit iron core for gas or liquid working environment The magnetic circuit iron core of the electromagnetic effect application device such as transformers, inductors, electromagnets, electromagnetic effect linear displacement actuators, or linearly moving the reset energy into electrical energy generation devices, etc., which constitute the iron core outer frame device has an outward extension The static motor of the heat dissipation wing and/or heat dissipation hole can increase the heat dissipation surface area of the surrounding gaseous or liquid environment to further improve the heat dissipation performance.

Based on the disclosure of the above application, the "outer frame device with iron core outer frame has a static electrical machine with outwardly extending heat dissipation wings and/or heat dissipation holes", the outer frame device is made into an outwardly extending heat dissipation wing structure, and/or phase The co-constructed heat dissipation holes and/or heat dissipation holes adjacent to the surface of the outer frame device and the magnetic circuit iron core can make the magnetic circuit iron core of the stationary motor increase the area of direct heat radiation to the surrounding gaseous or liquid environment. In addition, by increasing the external heat dissipation surface area by extending the heat dissipation wings, the heat dissipation performance of the clamped magnetic circuit core to the surrounding gaseous or liquid environment is further improved.

102‧‧‧longitudinal (Y-Y) bridge cooling wing

103‧‧‧Bending the heat dissipation wings from the outer edge

112‧‧‧longitudinal (Y-Y) heat dissipation holes

200‧‧‧Outer frame device

300‧‧‧Magnetic core

400‧‧‧winding structure

Claims (19)

A "Static electrical machine with iron core outer frame device with outwardly extending heat dissipation wings and/or heat dissipation holes", which is composed of:-Winding structure (400): including coil winding and insulated wire frame (BOBBIN) structure, externally conductive pins or wires, for installation on the magnetic circuit core (300); - magnetic circuit core (300): made of magnetically conductive material, including sheets The magnetically permeable materials are superimposed, or are made of bulk magnetically permeable materials, or are made of sintered magnetically conductive powder materials to form the magnetic circuit iron core (300) of the stationary motor for the winding structure (400); --Outer frame device (200): Outer frame device (200) made of thermally conductive material with outwardly extending heat dissipation wings and/or heat dissipation holes for clamping to the magnetic circuit core (300); The structure is composed of static motors such as transformers, inductors, electromagnets, electromagnetic effect linear displacement actuators, or linear-to-reset movement energy-generating electrical energy devices and other electromagnetic effect application devices, which are characterized by being clamped to a static motor The outer frame device (200) of the magnetic circuit core (300) is made of a thermally conductive material with an outwardly extending heat dissipation wing structure to increase the external heat dissipation surface area and/or has the outer frame device (200) and the magnetic circuit core ( 300) The heat dissipation holes on the mating surface for the magnetic circuit core (300) of the static motor to increase the area of direct heat radiation to the surrounding gaseous or liquid environment. When the surrounding gaseous or liquid fluid is flowing or static , Can improve the heat dissipation performance of the clamped magnetic circuit core (300) to the surrounding gaseous or liquid environment; the outer frame device (200) has outwardly extending heat dissipation wings and/or magnetic circuit core The heat dissipation holes for direct external heat dissipation include one or more of the following: (1) horizontal (XX) bridge-type heat dissipation wings (101); (2) longitudinal (YY) bridge-type heat dissipation wings (102); (3) from the outer edge Outer bending heat dissipation fins (103); (four) lateral (XX) half-bridge heat dissipation wings (104); (five) longitudinal (YY) half-bridge heat dissipation wings (105); (six) diagonal bridge heat dissipation wings (106); (VII) V-shaped bridge fins (107); (VIII) Transverse (XX) conformal heat dissipation holes (111); (IX) Vertical (YY) conformal heat dissipation holes (112); (X) Oblique co-configuration heat dissipation holes (116); (11) V-shaped co-configuration heat dissipation holes (117); and (12) The bonding surface of the outer frame device (200) and the magnetic circuit core (300) is provided for The magnetic circuit core (300) directly dissipates the heat dissipation holes (130). As described in the first patent application, the iron core outer frame device has a static electrical machine (Static electrical machine) with outwardly extending heat dissipation wings and/or heat dissipation holes, including a magnetic circuit for sandwiching between an approximately square cube or a rectangular cube When the iron core (300) is provided, the location for the outwardly extending heat dissipation wings and/or heat dissipation holes (130) is that the outer frame device (200) is sandwiched between the upper side of the magnetic circuit iron core (300) structure, The front side, the left side, the right side, the rear side, and the bottom side are at least one of A, B, C, D, E, F, G, H, I, J, K, and L. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A mask with at least one lateral (XX) bridge-type heat dissipation fin (101) and adjacent lateral (XX) heat dissipation holes (111) to enhance the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A mask with at least one longitudinal (YY) bridge-type heat dissipation fin (102) and adjacent longitudinal (YY) heat dissipation holes (112) to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A horizontal (XX) bridge fin (101) and the adjacent lateral (XX) framing holes (111), and its lateral (XX) bridge fins (101) have at least one drain hole (120) ) To improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A longitudinal (YY) bridge cooling fin (102) and the adjacent longitudinal (YY) radiating holes (112), and the longitudinal (YY) bridge cooling fin (102) has at least one drain hole (120) ) To improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A mask with at least one oblique bridge fin (106) and adjacent oblique composing heat dissipation holes (116) to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A mask with at least one V-shaped bridge heat sink (107) and adjacent V-shaped co-structured heat dissipation holes (117) to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) One side has a plurality of lateral (XX) half-bridge heat dissipation wings (104) and adjacent lateral (XX) co-structured heat dissipation holes (111), and each adjacent lateral (XX) half-bridge heat dissipation wing (104) is It is placed on the same side or different sides to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A mask has at least one horizontal (XX) half-bridge heat dissipation wing (104) and adjacent horizontal (XX) co-construction heat dissipation holes (111) arranged in multiple rows on the same side or different sides to enhance the gas or liquid around it The heat dissipation performance of the environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the stationary motor core formed by the core (300) is characterized by the upper side, front side, left side, right side, rear side, bottom side and the static side of the outer frame device (200) At least one of the outer edges of the fitting surface of the motor iron core has the heat dissipation wings (103) bent outward from the outer edge to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the stationary motor core formed by the core (300) is characterized by the upper side, front side, left side, right side, rear side, bottom side and the static side of the outer frame device (200) At least one of the outer edges of the motor iron core fitting surface has a heat dissipation wing (103) bent outward from the outer edge and has a multi-fold structure to further increase its heat dissipation area to enhance the surrounding gas or liquid environment Heat dissipation performance. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A longitudinal (YY) bridge-type cooling wing (102) and adjacent longitudinal (YY) co-constructed cooling holes (112), and the upper side, front side, left side, right side of the outer frame device (200), The rear side, the bottom side and the outer surface of the stationary motor core are at least one of the outer edges, with the outer edge of the cooling fin (103) and a multi-folded structure to further increase its heat dissipation area to improve the The heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that at least one of the upper side, front side, left side, right side, rear side and bottom side of the outer frame device (200) A longitudinal (YY) bridge cooling fin (102) and the adjacent longitudinal (YY) radiating holes (112), and the longitudinal (YY) bridge cooling fin (102) has at least one drain hole (120) ), and at least one of the upper side, the front side, the left side, the right side, the rear side, the bottom side of the outer frame device (200) and the outer edge of the static motor iron core fitting surface, with the outer edge outward Bending the heat dissipation wing (103) and having a multi-fold structure to further increase its heat dissipation area to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that the outer frame device (200) is a horizontal (XX) bridge type heat dissipation fin (101) and an adjacent horizontal (XX) )Constructing heat dissipation holes (111), its lateral (XX) bridge-type heat dissipation wings (101) have at least one drain hole (120), and its outer frame device (200) and magnetic circuit iron core (300) are attached to the mask for supply The magnetic circuit core (300) directly dissipates the heat dissipation holes (130) to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that the outer frame device (200) is a longitudinal (YY) bridge fin (102) and an adjacent longitudinal ( YY) Constitutive heat dissipation holes (112), the longitudinal (YY) bridge-type heat dissipation wings (102) have at least one drain hole (120), and the outer frame device (200) and the magnetic circuit iron core (300) fit the mask A heat dissipation hole (130) for the magnetic circuit core (300) to directly dissipate heat to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the static motor iron core formed by the core (300) is characterized in that the outer frame device (200) is provided with at least one lateral (XX) half-bridge heat dissipation wing (104) and adjacent The lateral (XX) co-construction heat dissipation holes (111), the outer frame device (200) and the magnetic circuit iron core (300) fit the mask to the heat dissipation holes (130) for the magnetic circuit iron core (300) to directly dissipate heat to improve The heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine with iron core outer frame device as described in items 1 and 2 of the patent scope with outwardly extending heat dissipation wings and/or heat dissipation holes, including magnetic circuit iron applied to approximately square cube or rectangular cube The outer frame device (200) of the outer periphery of the iron core of the stationary motor formed by the core (300) is characterized in that the outer frame device (200) is provided with at least one longitudinal (YY) half-bridge heat sink (105) and adjacent Longitudinal (YY) co-construction heat dissipation holes (112), the outer frame device (200) and the magnetic circuit core (300) are attached to the mask, and the rectangular slot-shaped heat dissipation for the magnetic circuit core (300) to directly dissipate heat Holes (130) to improve the heat dissipation performance of the surrounding gaseous or liquid environment. A static electrical machine with a fin and/or radiating holes extending outwards as described in the first and second paragraphs of the scope of the patent application includes a static electrical machine that includes a ferrule for clamping the magnetic circuit The device has an outwardly extending heat dissipation wing structure and/or a transformer, inductor, electromagnet, electromagnetic effect linear displacement actuator, or a linear displacement movement that has a heat dissipation hole provided on the surface of the outer frame device and the magnetic circuit iron core. It can be converted into a stationary motor composed of an electromagnetic effect application device such as a power generation device.

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