TWM586865U - Frame device of iron core of static electrical machine having outwardly-extended heat dissipation fins and/or heat dissipation hole - Google Patents

Abstract

The present utility discloses a frame device of iron core of static electrical machine having outwardly-extended heat dissipation fins and/or heat dissipation holes, 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.

Description

Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes

This new type is for stationary winding motors, such as transformers and inductors, which are composed of coil windings, insulated wireframes (BOBBIN), conductive pins and wires, and magnetic circuit cores for placement in gaseous or liquid working environments. , Electromagnets, electromagnetic effect linear displacement actuators, or linear reciprocating displacement energy can be converted into power generation electrical energy devices and other electromagnetic effect application devices, an innovative invention of a "static motor with outwardly extending cooling wings and / or cooling holes ( static electrical machine) ”to improve its heat dissipation performance; the magnetic circuit core of the aforementioned various electromagnetic effect application devices is usually fixed by a frame device made of thermally conductive materials, so as to facilitate assembly or disassembly. The outer frame device installed on the magnetic circuit core will inevitably form a shield on the surface of the magnetic circuit core for external heat dissipation. Therefore, the formed multilayer structure causes a large heat transmission thermal resistance, which prevents the magnetic circuit core from external heat transmission and heat dissipation and degrades. Its heat dissipation performance; The new "static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes" is not a rotary motor for generating turning energy, but is designed to be clamped to a stationary state. The electromagnetic effect application device of the electric motor is a structural innovation of the outer frame device of the magnetic circuit iron core. The application discloses "a static electrical machine iron frame device with outwardly extending cooling wings and / or cooling holes. "The outer frame device is made of heat dissipation holes with outwardly extending cooling wing structures and / or provided on the joint surface of the outer frame device and the magnetic circuit core. The heat dissipation holes enable the magnetic circuit core of the stationary motor to be increased. The area of the surrounding gaseous or liquid environment that directly exposes heat radiation, and the outwardly extending heat dissipation wings increase The external heat dissipation surface area further improves the heat dissipation performance of the clamped magnetic circuit core to the surrounding gaseous or liquid environment.

Traditionally, a winding structure composed of a coil winding, an insulated wire frame (BOBBIN) and conductive pins, and a wire for passing a current, and an electromagnetic effect application device composed of a magnetic circuit core for passing magnetic flux, such as a stationary motor such as Transformers, inductors, electromagnetic effect actuators, electromagnets, or mobile energy relay devices for electromagnetic effect applications are usually fixed with outer frame devices made of thermally conductive materials. The advantage is that they can effectively fix electromagnetic applications. The magnetic core of the device and the winding structure that protects it from coil windings, insulated wire frames (BOBBIN), conductive pins, and wires are missing because the outer frame device greatly shields part of the core's external heat dissipation surface, resulting in The deterioration of the external heat dissipation performance of the electromagnetic application device is missing.

As it is known that the stationary motor is different from the rotary motor, because it does not have a rotary function, it cannot drive the cooling fan to assist the cooling as the rotary motor itself. Therefore, the temperature rises to be the natural enemy of the stationary motor. Efficiency, so providing good heat dissipation performance is an important part of the structure of stationary motors. Based on the consideration of space, weight and cost, without the need to add additional cooling fans or liquid cooling devices, seek low cost, small size and One of the topics is to help the static heat dissipation performance of static motors to external radiation, conduction and convection; Traditionally, a winding structure composed of a coil winding, an insulated wire frame (BOBBIN) and conductive pins, and a wire for passing a current, and an electromagnetic effect application device composed of a magnetic circuit core for passing magnetic flux, such as a stationary motor such as Transformers, inductors, electromagnetic effect actuators, electromagnets, or mobile energy relay devices for electromagnetic effect applications are usually fixed with outer frame devices made of thermally conductive materials. The advantage is that they can effectively fix electromagnetic applications. The magnetic core of the device and its protection by the coil windings, insulated wire frame (BOBBIN) and guide The lack of the winding structure composed of electrical pins and wires is due to the fact that the outer frame device greatly shields part of the iron core's external heat dissipation surface, which causes the external heat dissipation performance of the electromagnetic application device to deteriorate. The new "static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes" is not a rotary motor for generating turning energy, but is designed to be clamped to a stationary state. The electromagnetic effect application device of the electric motor is a structural innovation of the outer frame device of the magnetic circuit iron core. The application discloses "a static electrical machine iron frame device with outwardly extending cooling wings and / or cooling holes. "The outer frame device is made of heat dissipation holes with outwardly extending cooling wing structures and / or provided on the joint surface of the outer frame device and the magnetic circuit core. The heat dissipation holes enable the magnetic circuit core of the stationary motor to be increased. The area where the surrounding gaseous or liquid environment directly exposes heat dissipation, and the outwardly extending cooling fins increase the external heat dissipation surface area to further enhance the heat dissipation performance of the magnetic core it clamps to the surrounding gaseous or liquid environment.

101‧‧‧Horizontal (X-X) Bridge Radiator

102‧‧‧Vertical (Y-Y) Bridge-type Radiator

103‧‧‧ Bend the cooling wing outward from the outer edge

104‧‧‧Horizontal (X-X) Half-Bridge Radiator

105‧‧‧Vertical (Y-Y) Half-Bridge Radiator

106‧‧‧ oblique bridge cooling wing

107‧‧‧V-type bridge cooling wing

111‧‧‧horizontal (X-X) co-structured cooling holes

112‧‧‧longitudinal (Y-Y) co-structured cooling holes

116‧‧‧ oblique co-constructed cooling holes

117‧‧‧V type co-constructed cooling hole

120‧‧‧ Drain hole

130‧‧‧Ventilation holes

200‧‧‧ frame device

300‧‧‧ Magnetic core

400‧‧‧winding structure

E‧‧‧ Top side of frame device

A, B, C, D‧‧‧ Front side of the frame device

F‧‧‧ Left side of frame device

G‧‧‧Right side of frame device

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

H‧‧‧ bottom side of frame device

Figure 1 shows one of the positions of the upper side (E) of the outer frame device (200) of the magnetic circuit core (300) of the new stationary motor for providing outwardly extending cooling wings and / or holes.

Figure 2 shows the position of the front side (A, B, C, D) of the outer frame device (200) of the magnetic circuit core (300) of the new type of stationary motor for providing outwardly extending cooling wings and / or cooling holes. of two.

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

FIG. 4 shows the fourth position diagram of the right side surface (G) of the outer frame device (200) of the magnetic circuit core (300) of the novel stationary motor for providing outwardly extending cooling wings and / or holes.

Figure 5 shows the position of the rear side (I, J, K, L) of the outer frame device (200) of the magnetic circuit core (300) of the new type of stationary motor for providing outwardly extending cooling wings and / or cooling holes. Five.

Figure 6 shows the bottom side of the outer frame device (200) of the magnetic core (300) of the new stationary motor. (H) No. 6 of the position drawing for setting outwardly extending cooling wings and / or cooling 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 wing (101) and adjacent lateral (XX) co-constructed heat dissipation holes (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 new type. The outer frame device (200) is provided with at least one longitudinal (YY) bridge-type cooling fin (102) and adjacent longitudinal (YY) co-constructed cooling 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 new model. The outer frame device (200) is provided with a plurality of lateral (XX) bridge cooling fins (101) and adjacent lateral (XX) co-constructed cooling 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 cooling fins (102) and adjacent longitudinal (YY) co-constructed cooling holes (112). view.

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

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

FIG. 19 shows the fifth embodiment of the new model. The outer frame device (200) has a lateral (XX) bridge-type cooling fin (101) and an adjacent lateral (XX) co-constructing heat dissipation hole (111). (XX) A front view of a bridge-type cooling fin (101) with at least one drain hole (120).

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

FIG. 21 is a side view of FIG. 19.

FIG. 22 shows the sixth embodiment of the new model. The outer frame device (200) has a longitudinal (YY) bridge-type cooling fin (102) and an adjacent longitudinal (YY) co-constructed cooling hole (112). (YY) Front view of a bridge cooling fin (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 diagonal bridge-type heat dissipation wing (106) and adjacent diagonal 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 the eighth embodiment of the present invention. The outer frame device (200) is a front view of at least one V-shaped bridge cooling fin (107) and adjacent V-shaped co-structured cooling holes (117).

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

FIG. 30 is a side view of FIG. 28.

FIG. 31 shows the ninth embodiment of the new model. The outer frame device (200) is a plurality of lateral (XX) half-bridge cooling wings (104) and adjacent lateral (XX) co-constructed cooling 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 new invention. The outer frame device (200) is a plurality of longitudinal (YY) half-bridge cooling fins (105) and adjacent longitudinal (YY) co-constructed cooling 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 the outer frame device (200) of the new type, which has a plurality of lateral (XX) half-bridge cooling fins (104) arranged on the same side and adjacent lateral (XX) co-constructed cooling holes (111). The embodiment is schematic.

FIG. 38 shows the outer frame device (200) of the new type, which has a plurality of lateral (XX) half-bridge cooling fins (104) staggered on different sides and adjacent lateral (XX) co-constructed cooling holes (111). ) Of the embodiment.

FIG. 39 shows the eleventh embodiment of the new model. The outer frame device (200) is provided with at least one lateral (XX) half-bridge cooling fin (104) and adjacent lateral (XX) ) Front view of the co-constructed thermal via (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 new model. The outer frame device (200) is provided with at least one lateral (XX) half-bridge cooling fin (104) and adjacent lateral (XX) ) Front view of the co-constructed thermal via (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 new model. The outer frame device (200) and at least one of the outer edges of the abutting surface of the stationary motor iron core are provided with the heat radiation wing (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 new model. At least one of the outer frame device (200) and the outer edge of the abutting surface of the stationary motor iron core is provided with a heat radiation wing (103) bent outward from the outer edge. 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 new model. The outer frame device (200) has a longitudinal (YY) bridge-type cooling fin (102) and adjacent longitudinal (YY) co-constructed cooling holes (112), and A front view of an embodiment in which the outer frame device (200) and at least one of the outer edges of the abutting surface of the stationary motor core have a heat dissipation wing (103) bent outward from the outer edge and presenting 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 the sixteenth embodiment of the new model. The outer frame device (200) has a longitudinal (YY) bridge-type cooling wing (102) and an adjacent longitudinal (YY) co-constructing heat dissipation hole (112). The longitudinal (YY) bridge cooling fin (102) has at least one drain hole (120), and its outer frame device (200) is attached to the stationary motor core At least one of the outer edges of the surface has a front view of an embodiment in which the heat dissipation wing (103) is bent outward from the outer edge and has 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 new stationary motor core outer frame device (200) and the magnetic circuit iron core (300), which has a square shape for the magnetic circuit iron core (300) to directly dissipate heat to the outside. Front view of an embodiment of a heat dissipation hole (130).

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

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

Figure 60 shows the cross-section (XX) of various cooling holes of the new stationary motor core frame device (200) and magnetic circuit core (300) attached to the mask for the magnetic circuit core (300) to directly radiate to the outside. Examples of shapes of the structured heat dissipation holes (111), the longitudinal (YY) co-structured heat dissipation holes (112), the oblique co-structured heat dissipation holes (116), the V-shaped co-structured heat dissipation holes (117), and the heat dissipation holes (130).

FIG. 61 shows the seventeenth embodiment of the new model. The outer frame device (200) is a lateral (XX) bridge-type cooling wing (101) and an adjacent lateral (XX) co-constructed heat dissipation hole (111). The transverse (XX) bridge cooling fin (101) is provided with at least one drain hole (120), and the outer frame device (200) and the magnetic circuit core (300) fit a mask for the magnetic circuit core (300) to directly radiate 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 the eighteenth embodiment of the new model. The outer frame device (200) is a longitudinal (YY) bridge-type heat dissipation wing (102) and an adjacent longitudinal (YY) co-constructed heat dissipation hole (112). The longitudinal (YY) bridge cooling fin (102) is provided with at least one drain hole (120), and the outer frame device (200) and the magnetic circuit core (300) are fitted with a mask for the magnetic circuit core (300) to directly radiate heat. Front view of the heat dissipation hole (130).

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

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

FIG. 67 shows the nineteenth embodiment of the new model, and the outer frame device (200) of Co-structure heat dissipation holes (111) to (XX) half-bridge cooling fins (104) and adjacent transverse (XX), the outer frame device (200) and the magnetic circuit core (300) fit the mask for the magnetic circuit iron Front view of the heat dissipation hole (130) for the core (300) directly radiating to the outside.

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

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

FIG. 70 shows the twentieth embodiment of the novel embodiment. The outer frame device (200) is provided with at least one longitudinal (YY) half-bridge cooling wing (105) and adjacent longitudinal (YY) co-constructed cooling holes (112). ), A front view of a rectangular slot-shaped heat dissipation hole (130) whose outer frame device (200) and magnetic circuit core (300) are attached to a mask for the magnetic circuit core (300) to directly radiate to the outside.

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

FIG. 72 is a side view of FIG. 70. FIG.

Traditionally, a winding structure composed of a coil winding, an insulated wire frame (BOBBIN) and conductive pins, and a wire for passing a current, and an electromagnetic effect application device composed of a magnetic circuit core for passing magnetic flux, such as a stationary motor such as Transformers, inductors, electromagnetic effect actuators, electromagnets, or mobile energy relay devices for electromagnetic effect applications are usually fixed with outer frame devices made of thermally conductive materials. The advantage is that they can effectively fix electromagnetic applications. The magnetic core of the device and the winding structure that protects it from coil windings, insulated wire frames (BOBBIN), conductive pins, and wires are missing because the outer frame device greatly shields part of the core's external heat dissipation surface, resulting in The deterioration of the external heat dissipation performance of the electromagnetic application device is missing.

This new type is for stationary winding motors, such as transformers and inductors, which are composed of coil windings, insulated wireframes (BOBBIN), conductive pins and wires, and magnetic circuit cores for placement in gaseous or liquid working environments. , Electromagnets, electromagnetic effect linear displacement actuators, or linear reciprocating displacement energy can be converted into power generation devices such as electromagnetic effect application devices, an innovative invention of a "static motor with outwardly extending cooling wings and / or cooling holes (static electrical machine) "to enhance its heat dissipation performance; the aforementioned magnetic effect application devices, the magnetic circuit core is usually fixed by a frame device made of thermally conductive material, to facilitate assembly or disassembly, The above-mentioned device arranged on the outer frame of the magnetic circuit core inevitably forms a shield on the surface of the magnetic circuit core for external heat dissipation, so the formed multilayer structure causes a large heat transmission thermal resistance, which prevents the magnetic circuit core from external heat transmission and heat dissipation. Deteriorate its heat dissipation performance.

The new "static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes" is not a rotary motor for generating turning energy, but is designed to be clamped to a stationary state. The electromagnetic effect application device of the electric motor is a structural innovation of the outer frame device of the magnetic circuit iron core. The application discloses "a static electrical machine iron frame device with outwardly extending cooling wings and / or cooling holes. "The outer frame device is made of heat dissipation holes with outwardly extending cooling wing structures and / or provided on the joint surface of the outer frame device and the magnetic circuit core. The heat dissipation holes enable the magnetic circuit core of the stationary motor to be increased. The area where the surrounding gaseous or liquid environment directly exposes heat dissipation, and the outwardly extending cooling fins increase the external heat dissipation surface area to further enhance the heat dissipation performance of the magnetic core it clamps to the surrounding gaseous or liquid environment.

The subject disclosed in this case refers to an electromagnetic effect application device applied to a stationary motor such as a transformer, an inductor, an electromagnetic effect actuator, an electromagnet, or a bit-moving energy forwarding electric energy output. A three-dimensional polyhedral magnetic circuit core (300) structure composed of a superposed magnetic circuit core (300), or various three-dimensional shapes composed of a sintered block-shaped magnetic core powder core.

Taking the outer frame device (200) of a stationary motor core composed of a nearly square cube or rectangular cube magnetic circuit core (300) with six surfaces and the most widely used magnetic circuit core (300) as an example, the description is given below. The specific positions for providing outwardly extending cooling wing structures and / or heat dissipation holes provided on the joint surface of the outer frame device (200) and the magnetic circuit core (300) are described below: Figure 1 shows the new type of static type Motor magnetic core (300) framed Set (200) on

The side (E) is used to provide one of the location drawings for outwardly extending cooling wings and / or cooling holes.

Figure 2 shows the position of the front side (A, B, C, D) of the outer frame device (200) of the magnetic circuit core (300) of the new type of stationary motor for providing outwardly extending cooling wings and / or cooling holes. of two.

FIG. 3 shows the third position diagram of the left side (F) of the outer frame device (200) of the magnetic circuit core (300) of the new type of stationary motor for providing outwardly extending cooling wings and / or holes.

FIG. 4 shows the fourth position diagram of the right side surface (G) of the outer frame device (200) of the magnetic circuit core (300) of the novel stationary motor for providing outwardly extending cooling wings and / or holes.

Figure 5 shows the position of the rear side (I, J, K, L) of the outer frame device (200) of the magnetic circuit core (300) of the new type of stationary motor for providing outwardly extending cooling wings and / or cooling holes. Five.

FIG. 6 shows the sixth position diagram of the position where the bottom side (H) of the outer frame device (200) of the magnetic circuit core (300) of the new stationary motor is provided with outwardly extending cooling wings and / or holes.

As shown in Figs. 1 to 6, when the present invention is applied to the magnetic core (300) for clamping in an approximately square cube or a rectangular cube, it is specifically provided to provide outwardly extending cooling wings and / or cooling holes (130 ) Position is the side frame, front side, left side, right side, rear side, and bottom side of the above-mentioned outer frame device (200) sandwiched on the structure of the magnetic circuit core (300) 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, its bottom is used for fixing and fixing When it is covered by the fixed surface, it can be considered elastically whether to provide outwardly extending cooling wings and / or heat dissipation holes (130), and at least one of the remaining surfaces of the outer frame device (200) is provided for outwardly extending heat dissipation. Wings and / or heat dissipation holes (130).

When the stationary motor is set to be suspended, the magnetic circuit iron for clamping the stationary motor At least one of the surfaces of the outer frame device (200) of the core (300) and at least one of the surfaces of the housing device is provided with outwardly extending heat dissipation wings and / or heat dissipation holes (130).

As described above, in the application "Static electrical machine iron core frame device with outwardly extending cooling wings and / or heat dissipation holes", the feature is that the outer frame device (200) has outwardly extending heat dissipation The wing and / or heat dissipation holes for the magnetic circuit core (300) directly radiating to the outside constitute an optimized structure for improving the heat transmission performance of the magnetic circuit core (300) to the surrounding gaseous or liquid environment, of which: The outwardly extending cooling fins and cooling holes include one or more of the following: (1) transverse (XX) bridge-type cooling fins (101); (2) longitudinal (YY) bridge-type cooling fins (102); (3) from the outside The edge is bent outwardly (103); (4) transverse (XX) half-bridge heat sink (104); (5) longitudinal (YY) half-bridge heat sink (105); (6) diagonal bridge Radiating wing (106); (7) V-shaped bridge radiating wing (107); (8) transverse (XX) co-constructed cooling holes (111); (9) longitudinal (YY) co-constructed cooling holes (112); ( 10) oblique co-structured heat dissipation holes (116); (11) V-type 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) is a heat dissipation hole (130) for direct heat dissipation.

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 wing (101) and adjacent lateral (XX) co-constructed heat dissipation holes (111). view.

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

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

As shown in FIG. 7 to FIG. 9, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit iron core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200). At least one lateral (XX) bridge cooling fin (101) and adjacent lateral (XX) co-construct. The heat dissipation holes (111) are used to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 10 shows the second embodiment of the new type. The outer frame device (200) is provided with at least one longitudinal (YY) bridge-type cooling fin (102) and adjacent longitudinal (YY) co-constructed cooling 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 to 12, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200). At least one longitudinal (YY) bridge cooling fin (102) and adjacent longitudinal (YY) are co-constructed. The heat dissipation hole (112) is used to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 13 shows the third embodiment of the new model. The outer frame device (200) is provided with a plurality of lateral (XX) bridge cooling fins (101) and adjacent lateral (XX) co-constructed cooling 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 to 15, it is an example of a stationary motor core outer frame device (200) that is applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks multiple lateral (XX) bridge-type cooling fins (101) And adjacent transverse (X-X) co-constructing 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 cooling fins (102) and adjacent longitudinal (YY) co-constructed cooling holes (112). view.

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

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

As shown in FIG. 16 to FIG. 18, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks multiple longitudinal (YY) bridge cooling fins (102) and adjacent longitudinal (YY) co-constructions The heat dissipation hole (112) is used to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 19 shows the fifth embodiment of the new model. The outer frame device (200) has a lateral (XX) bridge-type cooling fin (101) and an adjacent lateral (XX) co-constructing heat dissipation hole (111). (XX) A front view of a bridge-type cooling fin (101) with at least one drain hole (120).

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

FIG. 21 is a side view of FIG. 19.

As shown in Fig. 19 ~ 21, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the top side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks lateral (XX) bridge-type cooling fins (101) and adjacent lateral (XX) co-constructed cooling holes (111), and its lateral (XX) bridge-type heat dissipation wing (101) has at least one drain hole (120) to improve the heat dissipation performance of its surrounding gaseous or liquid environment.

FIG. 22 shows the sixth embodiment of the new type. The outer frame device (200) has longitudinal (Y-Y) bridge-type cooling fins (102) and adjacent longitudinal (Y-Y) co-structured cooling holes (112). Front view of (Y-Y) bridge-type cooling 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, it is an example of a stationary motor core outer frame device (200) that is applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks longitudinal (YY) bridge cooling fins (102) and adjacent longitudinal (YY) co-constructed cooling holes (112), and the longitudinal (YY) bridge-type cooling wing (102) has at least one drain hole (120), so as to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

The aforementioned bridge radiating wing may further be composed of a diagonal or V-shaped bridge radiating wing structure and a co-constructing radiating hole, which will be described as follows: FIG. 25 shows the seventh embodiment of the present invention, and the outer frame device (200 ) Is a front view of at least one oblique bridge heat radiation fin (106) and adjacent oblique co-structure heat radiation 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, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks at least one oblique bridge cooling wing (106) and adjacent oblique co-constructing heat dissipation holes (116 ), In order to improve the heat dissipation performance of its surrounding gaseous or liquid environment.

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

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

FIG. 30 is a side view of FIG. 28.

As shown in FIGS. 28 to 30, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks at least one V-shaped bridge cooling fin (107) and adjacent V-shaped co-structured cooling holes (117 ), In order to improve the heat dissipation performance of its surrounding gaseous or liquid environment.

This "static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes" can further be composed of a half-bridge cooling wing and a co-structured cooling hole structure; It is as follows: Fig. 31 shows the ninth embodiment of the new model. The outer frame device (200) is a plurality of lateral (XX) semi-bridge cooling fins (104) and adjacent lateral (XX) co-constructed cooling 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, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks multiple lateral (XX) half-bridge cooling fins (104) and adjacent lateral (XX) The heat dissipation holes (111) are constructed to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 34 shows the tenth embodiment of the new invention. The outer frame device (200) is a plurality of longitudinal (YY) half-bridge cooling fins (105) and adjacent longitudinal (YY) co-constructed cooling 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, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks multiple longitudinal (YY) half-bridge cooling fins (105) and adjacent longitudinal (YY) The heat dissipation holes (112) are constructed to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

The “static electrical machine iron core frame device with outwardly extending cooling fins and / or cooling holes” described in FIG. 31 to FIG. 36 mentioned above, the half-bridge type cooling wing installation method includes the same side Set or staggered settings on different sides; here is an example to illustrate: Figure 37 shows the new frame device (200) of the new model with multiple lateral (XX) half-bridge cooling wings (104) and phase A schematic diagram of an embodiment of adjacent lateral (XX) co-constructed heat dissipation holes (111).

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

FIG. 38 shows the outer frame device (200) of the new type, which has a plurality of lateral (XX) half-bridge cooling fins (104) staggered on different sides and adjacent lateral (XX) co-constructed cooling holes (111). ) Of the embodiment.

As shown in FIG. 38, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300), which is characterized by an outer frame device ( 200) At least one of the upper side, front side, left side, right side, rear side, and bottom side has multiple lateral (XX) half-bridge cooling wings (104) And adjacent lateral (XX) co-constructing heat dissipation holes (111), each adjacent lateral (XX) half-bridge cooling fin (104) is staggered on different sides to enhance the heat dissipation to the surrounding gaseous or liquid environment Performance person.

FIG. 39 shows the eleventh embodiment of the new model. The outer frame device (200) is provided with at least one lateral (XX) half-bridge cooling fin (104) and adjacent lateral (XX) ) Front view of the co-constructed thermal via (111).

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

Fig. 41 is a side view of Fig. 39;

As shown in Fig. 39 ~ 41, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200). At least one of the lateral (XX) half-bridge cooling fins (104) and the opposite side are arranged in multiple rows on the same side. 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 new model. The outer frame device (200) is provided with at least one lateral (XX) half-bridge cooling fin (104) and adjacent lateral (XX) ) Front view of the co-constructed thermal via (111).

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

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

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

This "static motor with outwardly extending cooling wings and / or cooling holes (static electrical machine) ", further characterized in that the outer frame device (200) and the outer edge of the stationary motor iron core at least one of the bonding surfaces can be bent outward from the outer edge to dissipate heat. The wing (103); here is an example for illustration: 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 abutting surface of the stationary motor core are provided by the outer edge. Front view of an embodiment in which the cooling fins (103) are bent outward.

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

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

As shown in Fig. 45 ~ 47, it is an example of a stationary motor core outer frame device (200) applied to 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, the bottom side and the outer edge of the bonding surface of the stationary motor core with the frame device (200). 103), in order to improve the heat dissipation performance of its surrounding gaseous or liquid environment.

FIG. 48 shows the fourteenth embodiment of the new model. At least one of the outer frame device (200) and the outer edge of the abutting surface of the stationary motor iron core is provided with a heat radiation wing (103) bent outward from the outer edge. 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 Fig. 48 ~ 50, it is an example of a stationary motor core outer frame device (200) applied to 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, the bottom side and the outer edge of the bonding surface of the stationary motor core with the frame device (200). 103) And it has a multi-fold structure to further increase its heat dissipation area and improve its heat dissipation performance to its surrounding gaseous or liquid environment.

Fig. 51 shows the fifteenth embodiment of the new model, and the outer frame device (200) At least one of the longitudinal (YY) bridge cooling fins (102) and the adjacent longitudinal (YY) co-constructed cooling holes (112), and the outer edge of the outer frame device (200) and the bonding surface of the stationary motor core A front view of an embodiment in which the cooling fins (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 Fig. 51 ~ 53, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks longitudinal (YY) bridge cooling fins (102) and adjacent longitudinal (YY) co-constructed cooling holes (112), and at least one of the upper side, front side, left side, right side, rear side, bottom side of the outer frame device (200) and the outer edge of the stationary motor core bonding surface, with the outer edge The heat dissipation wing (103) is bent outward and has a multi-folded structure to further increase its heat dissipation area and improve its heat dissipation performance to its surrounding gaseous or liquid environment.

FIG. 54 shows the sixteenth embodiment of the new model. The outer frame device (200) has a longitudinal (YY) bridge-type cooling wing (102) and an adjacent longitudinal (YY) co-constructing heat dissipation hole (112). The longitudinal (YY) bridge cooling fin (102) has at least one drain hole (120), and at least one of the outer edges of the outer surface of the outer frame device (200) and the static motor core bonding surface. A front view of an embodiment in which the radiating fins (103) are bent outward and have 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 Fig. 54 ~ 56, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). At least one of the upper side, front side, left side, right side, rear side, and bottom side of the frame device (200) masks longitudinal (YY) bridge cooling fins (102) and adjacent longitudinal (YY) co-constructed cooling holes (112), and its longitudinal (YY) bridge cooling fin (102) has at least one drain hole (120), and the upper side, front side, left side of its outer frame device (200), At least one of the right side, the rear side, the bottom side and the outer edge of the stationary motor core bonding 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. In order to improve the heat dissipation performance of its surrounding gaseous or liquid environment.

This "static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes" has a lateral (XX) bridge-type cooling wing (101) or a lateral (XX) half-bridge type Radiating wing (104) and adjacent transverse (XX) co-constructing radiating holes (111), longitudinal (YY) bridge radiating fins (102) or longitudinal (YY) half-bridge radiating fins (105) and adjacent longitudinal (YY) Co-constructed cooling holes (112), oblique bridge cooling fins (106) and adjacent oblique co-construction cooling holes (116), V-bridge cooling fins (107) and adjacent V-shaped common cooling holes The structured heat dissipation hole (117) constitutes a function for the magnetic circuit core (300) to directly dissipate heat to the outside, and is further characterized in that it can be installed in the stationary motor core outer frame device (200) and the magnetic circuit core (300). At least one of them fits a square-shaped or rectangular-shaped heat-dissipating hole (130) for the magnetic circuit core (300) for direct heat dissipation; an example is given below: Figure 57 shows the outside of the new type of stationary motor core At least one of the bonding surfaces of the frame device (200) and the magnetic circuit core (300) has a square-shaped heat dissipation hole (130) for direct external heat dissipation by the magnetic circuit core (300).

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

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

As shown in Fig. 57 ~ 59, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300), which is characterized by being stationary At least one of the upper side, front side, left side, right side, rear side, bottom side of the motor core outer frame device (200) and the bonding surface of the magnetic circuit core (300), with a magnetic circuit The iron core (300) directly dissipates heat into a square-shaped heat dissipation hole (130) to enhance the heat dissipation performance of the surrounding gaseous or liquid environment.

Figure 60 shows various heat dissipation holes for the new stationary motor core frame (200) and the magnetic circuit core (300) to fit the mask for the magnetic circuit core (300) to directly dissipate heat. Among the horizontal (XX) co-structured heat dissipation holes (111), the longitudinal (YY) co-structured heat dissipation holes (112), the oblique co-structured heat dissipation holes (116), the V-shaped co-structured heat dissipation holes (117), and the heat dissipation holes (130). Shape example illustration.

As shown in FIG. 60, it is an example of a stationary motor core outer frame device (200) that is applied to an approximately square cube or rectangular cube magnetic circuit iron core (300), which is characterized by a stationary motor iron At least one of the bonding surfaces of the core outer frame device (200) and the magnetic circuit iron core (300) may further be composed of various arc-shaped heat dissipation holes and / or polygonal heat dissipation holes, as shown in FIG. 60 as an example. Various types of heat dissipation holes Horizontal (XX) co-structured heat dissipation holes (111), longitudinal (YY) co-structured heat dissipation holes (112), oblique co-structured heat dissipation holes (116), V-shaped co-structured heat dissipation holes (117), heat dissipation holes (130) The shape includes a hole shape or a slot hole shape; for example: (a) a circular heat sink; (b) an oval heat sink; (c) a semi-circular heat sink; (d) a triangular heat sink; e) Quadrangular cooling holes; (f) Pentagonal cooling holes; (g) Hexagonal cooling holes; (h) Heptagonal cooling holes; (i) Octagonal cooling holes; (j) Diamond-shaped cooling holes; (k) Oblique shapes Ventilation holes; (l) V-shaped vents; (m) Star-shaped vents; (n) Rectangular oval-shaped slot-shaped vents with convex arcs on both sides; (o) Rectangular slot-shaped vents Ventilation holes; (p) at least one side with toothed edges Shaped hole configuration of various geometries of holes and the like, and is constituted by at least one of which; the above-exemplified (a) ~ (p) to form a non-limiting, only illustrative.

In the application "Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes", the outer frame device (200) has outwardly extending cooling wings and / or The heat dissipation holes for the magnetic circuit core (300) to directly radiate to the outside constitute an optimized structure for improving the heat transmission performance of the magnetic circuit core (300) to the surrounding gaseous or liquid environment. Among them: the outwardly extending cooling wings and the cooling holes include the following One or more: (1) transverse (XX) bridge-type cooling fins (101); (2) longitudinal (YY) bridge-type radiating fins (102); (3) bending the cooling fins (103) outward from the outer edge (4) Lateral (XX) half-bridge cooling fins (104); (5) longitudinal (YY) half-bridge cooling fins (105); (6) oblique bridge cooling fins (106); (7) V-bridge cooling fins (107); (8) horizontal (XX) total Structured heat dissipation holes (111); (9) longitudinal (YY) co-structured heat dissipation holes (112); (10) oblique co-structured heat dissipation holes (116); (11) V-type co-structured heat dissipation holes (117); and ( 12) A heat dissipation hole (130) is provided on the bonding surface of the outer frame device (200) and the magnetic circuit core (300) for the magnetic circuit core (300) to directly radiate to the outside.

This "static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes" can be further installed on the static motor magnetic circuit iron by one or more of the above-mentioned heat dissipation structures as required. At least one of the upper side, front side, left side, right side, rear side, and bottom side of the outer frame device (200) of the core (300), and the required number of settings, the following examples are given By way of illustration, the embodiments are for illustration and are not intended to limit the structural types and number of the heat dissipation wings extending outwardly and / or the shape and number of the heat dissipation holes.

FIG. 61 shows the seventeenth embodiment of the new model. The outer frame device (200) is a lateral (XX) bridge-type cooling wing (101) and an adjacent lateral (XX) co-constructed heat dissipation hole (111). The transverse (XX) bridge cooling fin (101) is provided with at least one drain hole (120), and the outer frame device (200) and the magnetic circuit core (300) fit a mask for the magnetic circuit core (300) to directly radiate 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, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). The frame device (200) is a lateral (XX) bridge-type cooling wing (101) and Adjacent lateral (XX) co-constructed cooling holes (111), the lateral (XX) bridge-type cooling fins (101) have at least one drain hole (120), the outer frame device (200) and the magnetic circuit core ( 300) Fit the mask with a 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.

FIG. 64 shows the eighteenth embodiment of the new model. The outer frame device (200) is a longitudinal (YY) bridge-type heat dissipation wing (102) and an adjacent longitudinal (YY) co-constructed heat dissipation hole (112). The longitudinal (YY) bridge cooling fin (102) is provided with at least one drain hole (120), and the outer frame device (200) and the magnetic circuit core (300) are fitted with a mask for the magnetic circuit core (300) to directly radiate heat. Front view of the heat dissipation hole (130).

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

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

As shown in FIGS. 64 to 66, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300), which is characterized by: The outer frame device (200) is provided with a longitudinal (YY) bridge-type cooling fin (102) and an adjacent longitudinal (YY) co-constructed cooling hole (112), and the longitudinal (YY) bridge-type radiating fin (102) has at least one The drain hole (120), whose outer frame device (200) and the magnetic circuit iron core (300) fit a mask for the magnetic circuit iron core (300), a heat dissipation hole (130) for direct external heat dissipation, so as to improve its gaseous or Thermal performance in liquid environment.

FIG. 67 shows the nineteenth embodiment of the new model, and the outer frame device (200) thereof is provided with at least one lateral (XX) half-bridge cooling fin (104) and adjacent lateral (XX) co-constructed cooling holes (111). ), A front view of the heat dissipation hole (130) of the outer frame device (200) and the magnetic circuit iron core (300) attached to the mask for the magnetic circuit iron core (300) to directly radiate to the outside.

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

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

As shown in Fig. 67 ~ 69, it is a stationary motor core outer frame device composed of a magnetic core (300) applied to an approximately square cube or a rectangular cube. (200) is taken as an example, which is characterized in that the outer frame device (200) has at least one lateral (XX) half-bridge cooling wing (104) and adjacent lateral (XX) co-constructed heat dissipation holes (111), and the outer frame The device (200) and the magnetic circuit iron core (300) are fitted with a mask for the magnetic circuit iron core (300) to directly dissipate heat dissipation holes (130) for external heat dissipation, so as to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

FIG. 70 shows the twentieth embodiment of the novel embodiment. The outer frame device (200) is provided with at least one longitudinal (YY) half-bridge cooling wing (105) and adjacent longitudinal (YY) co-constructed cooling holes (112). ), A front view of a rectangular slot-shaped heat dissipation hole (130) whose outer frame device (200) and magnetic circuit core (300) are attached to a mask for the magnetic circuit core (300) to directly radiate to the outside.

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

FIG. 72 is a side view of FIG. 70. FIG.

As shown in Figures 70 to 72, it is an example of a stationary motor core outer frame device (200) applied to an approximately square cube or rectangular cube magnetic circuit core (300). The frame device (200) is provided with at least one longitudinal (YY) half-bridge cooling fin (105) and adjacent longitudinal (YY) co-constructed cooling holes (112). The outer frame device (200) and the magnetic circuit core ( 300) A rectangular slot-shaped heat dissipation hole (130) that fits the mask for the magnetic circuit core (300) to directly radiate to the outside, in order to improve the heat dissipation performance of the surrounding gaseous or liquid environment.

Applications for "static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes" applications include "with outwardly extending cooling wings and / or heat dissipation made of thermally conductive material" The static electrical machine (core iron outer frame device of the hole) is clamped to the winding structure composed of the coil winding, the insulated wire frame (BOBBIN), the conductive pins, and the wire, and the magnetic circuit iron core for placement. Magnetic cores of stationary motors in gaseous or liquid working environments such as transformers, inductors, electromagnets, electromagnetic effect linear displacement actuators, or linear reciprocating displacements can be converted to electromagnetic effect application devices such as power generation devices, and A static motor that forms an iron core frame device with outwardly extending heat dissipation wings and / or heat dissipation holes to increase the heat dissipation surface area of its surrounding gaseous or liquid environment and further improve its heat dissipation performance.

The outer frame device of the "static electrical machine iron core frame device with outwardly extending fins and / or radiating holes" disclosed in the above application is made into an outwardly extending radiating wing structure and / or phase. The co-constructed heat dissipation holes and / or heat dissipation holes arranged adjacent to the bonding surface of the outer frame device and the magnetic circuit iron core, so that the magnetic circuit iron core of the stationary motor can increase the area directly exposed to the surrounding gaseous or liquid environment. In addition to the aforementioned, by extending the heat dissipation wings outwardly to increase the external heat dissipation surface area, the heat dissipation performance of the clamped magnetic circuit core to its surrounding gaseous or liquid environment is further improved.

Claims (24)

A static electrical machine iron core outer frame device with outwardly extending cooling wings and / or heat dissipation holes, the outer frame device is made of an outwardly extending heat dissipation wing structure and / or is provided on the outer frame device and Radiating holes on the surface of the magnetic core of the magnetic circuit. The thermal holes allow the magnetic core of the stationary motor to increase the area directly exposed to the surrounding gaseous or liquid environment, and the outwardly extending cooling fins increase the surface area for external heat dissipation. The heat dissipation performance of the clamped magnetic circuit iron core to its surrounding gaseous or liquid environment; characterized in that the outer frame device (200) has outwardly extending cooling wings and / or the magnetic circuit iron core (300) directly externally The heat radiation holes constitute an optimized structure for improving the heat transmission performance of the magnetic circuit iron core (300) to the surrounding gaseous or liquid environment. Among them: the outwardly extending heat radiation wings and heat radiation holes include one or more of the following: (a) transverse ( XX) bridge-type cooling wing (101); (two) longitudinal (YY) bridge-type radiating wing (102); (three) bending the heat-radiating wing (103) outward from the outer edge; (four) transverse (XX) half-bridge Cooling fins (104); (5) longitudinal (YY) half-bridge cooling fins (105); (6) oblique Bridge cooling fins (106); (7) V-shaped bridge cooling fins (107); (8) horizontal (XX) co-structured cooling holes (111); (9) longitudinal (YY) co-structured cooling holes (112) (10) oblique co-constructed heat dissipation holes (116); (11) V-type co-constructed heat dissipation holes (117); and (12) bonding of the outer frame device (200) and the magnetic circuit core (300) A heat dissipation hole (130) is provided on the surface for the magnetic circuit core (300) to directly dissipate heat to the outside. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes as described in item 1 of the scope of patent application, including a magnetic circuit for clamping in an approximately square cube or rectangular cube In the case of the iron core (300), its specific position is provided for outwardly extending cooling wings and / or heat dissipation holes (130), and the above-mentioned outer frame device (200) is sandwiched on the side of the structure of the magnetic circuit iron core (300), The front side, left side, right side, rear side, and bottom side are at least one of A, B, C, D, E, F, G, H, I, J, K, and L positions. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 lateral (XX) bridge-type cooling wing (101) and adjacent lateral (XX) co-constructed cooling holes (111) to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 longitudinal (YY) bridge-type cooling wing (102) and adjacent longitudinal (YY) co-constructed heat dissipation holes (112) to enhance the heat dissipation performance of its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 mask has multiple lateral (XX) bridge-type cooling fins (101) and adjacent lateral (XX) co-constructed cooling holes (111) to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 multiple longitudinal (YY) bridge cooling fins (102) and adjacent longitudinal (YY) co-constructed heat dissipation holes (112) to enhance the heat dissipation performance of its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 lateral (XX) bridge cooling fin (101) and adjacent lateral (XX) co-constructed cooling holes (111), and the lateral (XX) bridge cooling fin (101) has at least one drain hole (120) ), In order to improve the heat dissipation performance of its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 longitudinal (YY) bridge cooling fin (102) and adjacent longitudinal (YY) co-constructed cooling holes (112), and the longitudinal (YY) bridge cooling fin (102) has at least one drain hole (120) ), In order to improve the heat dissipation performance of its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 oblique bridge heat dissipation wing (106) and adjacent oblique co-construction heat dissipation holes (116), so as to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 V-shaped bridge radiating wing (107) and an adjacent V-shaped co-constructed radiating hole (117), so as to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electricai machine core frame device with outwardly extending fins and / or radiating holes as described in item 1 or 2 of the scope of patent application, including application to approximately square cube or rectangular cube magnetic circuit iron The outer frame device (200) of the stationary motor iron core 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) semi-bridge cooling fins (104) and adjacent lateral (XX) co-constructed cooling holes (111). Each adjacent lateral (XX) half-bridge cooling fin (104) is It is set on the same side to improve the heat dissipation performance of its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 cooling fins (104) and adjacent lateral (XX) co-constructing cooling holes (111). Each of the adjacent lateral (XX) half-bridge cooling fins (104) is Different sides are staggered to improve the heat dissipation performance of its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling fins and / or cooling holes as described in item 1 or 2 of the scope of patent application, including magnetic iron used in approximately square cubes or rectangular cube The outer frame device (200) of the stationary motor iron core 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 lateral (XX) half-bridge cooling fin (104) arranged in multiple rows on the same side and adjacent lateral (XX) co-constructed cooling holes (111) to enhance the heat dissipation to the surrounding gaseous or liquid environment. Performance person. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 lateral (XX) half-bridge cooling fin (104) arranged in multiple rows on different sides and adjacent lateral (XX) co-constructed cooling holes (111) to enhance the heat dissipation to the surrounding gaseous or liquid environment. Performance person. Static electrical machine iron core frame device with outwardly extending cooling fins and / or cooling holes as described in item 1 or 2 of the scope of patent application, including magnetic iron used in approximately square cubes or rectangular cube The outer frame device (200) of the stationary motor iron core formed by the core (300) is characterized by the upper side, front side, left side, right side, rear side, bottom side and stationary of the outer frame device (200). At least one of the outer edges of the motor iron core bonding surface has a heat dissipation wing (103) bent outward from the outer edge to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core formed by the core (300) is characterized by the upper side, front side, left side, right side, rear side, bottom side and stationary of the outer frame device (200). At least one of the outer edges of the bonding surface of the motor core has a heat dissipation wing (103) bent outward from the outer edge and has a multi-folded structure to further increase its heat dissipation area and enhance its surrounding gaseous or liquid environment. Thermal performance. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 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), At least one of the rear side, the bottom side, and the outer edge of the stationary motor core bonding surface has a heat dissipation wing (103) bent outwardly from the outer edge and has a multi-folded structure to further increase its heat dissipation area and improve alignment. The heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core 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 longitudinal (YY) bridge cooling fin (102) and adjacent longitudinal (YY) co-constructed cooling 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, front side, left side, right side, rear side, bottom side of the outer frame device (200) and the outer edge of the stationary motor core bonding surface, with the outer edge outward The heat dissipation wing (103) is bent and has a multi-folded structure to further increase its heat dissipation area and improve its heat dissipation performance to its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The stationary motor core outer frame device (200) composed of a core (300) is characterized by the upper side, front side, left side, right side, and rear of the stationary motor core outer frame device (200). At least one of the side surface, the bottom side surface and the bonding surface of the magnetic circuit core (300) is provided with a square-shaped heat dissipation hole (130) for direct external heat dissipation of the magnetic circuit core (300) to enhance the gaseous or Thermal performance in liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core formed by the core (300) is characterized in that the outer frame device (200) is a transverse (XX) bridge-type cooling wing (101) and an adjacent transverse (XX) ) Co-structured cooling holes (111), whose transverse (XX) bridge-type cooling fins (101) are provided with at least one drain hole (120), and the outer frame device (200) and the magnetic circuit core (300) are fitted with a mask for The magnetic circuit core (300) directly radiates heat to the outside (130), so as to improve the heat dissipation performance of the surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core formed by the core (300) is characterized in that the outer frame device (200) is provided with a longitudinal (YY) bridge-type cooling wing (102) and an adjacent longitudinal ( YY) co-constructed cooling holes (112), whose longitudinal (YY) bridge-type cooling wing (102) has at least one drain hole (120), and its outer frame device (200) and magnetic circuit iron core (300) fit a mask 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 iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary 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 cooling fin (104) and adjacent Horizontal (XX) co-constructed heat dissipation holes (111), whose outer frame device (200) and magnetic circuit iron core (300) fit a mask for the heat dissipation holes (130) of the magnetic circuit iron core (300) for direct external heat dissipation to enhance The heat dissipation performance of its surrounding gaseous or liquid environment. Static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, as described in item 1 or 2 of the scope of patent application, including a magnetic circuit iron applied to an approximately square cube or a rectangular cube The outer frame device (200) of the stationary motor iron core formed by the core (300) is characterized in that the outer frame device (200) is provided with at least one longitudinal (YY) half-bridge cooling wing (105) and adjacent Longitudinal (YY) co-structured cooling holes (112), whose outer frame device (200) and magnetic circuit iron core (300) fit a mask for the magnetic circuit iron core (300) to directly radiate heat in a rectangular slot shape. Hole (130) to improve the heat dissipation performance of its surrounding gaseous or liquid environment. As described in item 1 or 2 of the scope of the patent application, a static electrical machine iron core frame device with outwardly extending cooling wings and / or cooling holes, the application of which includes a "tool with a thermally conductive material" The static electrical machine iron core frame device that extends the cooling wings and / or cooling holes outwards is clamped to the winding structure composed of the coil winding, the insulated wire frame (BOBBIN), and the conductive pins and wires. A magnetic circuit iron core constitutes a stationary motor such as a transformer, an inductor, an electromagnet, an electromagnetic effect linear displacement actuator, or a linear reciprocating displacement device that can be placed in a gaseous or liquid working environment. The magnetic circuit iron core of the device is used, and the static motor constituting the iron core frame device with outwardly extending cooling wings and / or heat dissipation holes is used to increase the heat dissipation surface area of the surrounding gaseous or liquid environment and further improve its heat dissipation performance.