CN204141738U - Desktop air-conditioning - Google Patents

Desktop air-conditioning Download PDF

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Publication number
CN204141738U
CN204141738U CN201420521468.0U CN201420521468U CN204141738U CN 204141738 U CN204141738 U CN 204141738U CN 201420521468 U CN201420521468 U CN 201420521468U CN 204141738 U CN204141738 U CN 204141738U
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CN
China
Prior art keywords
air
fuselage
half shell
conditioning
desktop
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Withdrawn - After Issue
Application number
CN201420521468.0U
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Chinese (zh)
Inventor
王友宁
朱振学
袁珊娜
庄佳兰
马令庆
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Qingdao Haier Air Conditioner Gen Corp Ltd
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Qingdao Haier Air Conditioner Gen Corp Ltd
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Priority to CN201420521468.0U priority Critical patent/CN204141738U/en
Application granted granted Critical
Publication of CN204141738U publication Critical patent/CN204141738U/en
Withdrawn - After Issue legal-status Critical Current
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Abstract

The utility model relates to desktop air-conditioning.Particularly, the utility model provides a kind of desktop air-conditioning, comprises base and fuselage, and especially, the outer surface of base has horizontally outward flange sections that is outstanding, a circumferentially angle, flange sections has circumferential detent; Fuselage comprises two fuselage half shells and movement, and the bottom of one of them fuselage half shell has the groove section corresponding with flange sections, is provided with the circumference corresponding with the circumferential detent of flange sections and locates floor in groove section.Desktop air-conditioning of the present utility model and installation method thereof, because the special structure of base and fuselage, significantly improve the installation effectiveness of desktop air-conditioning.

Description

Desktop air-conditioning
Technical field
The utility model relates to a kind of air-supply arrangement or aircondition, particularly relates to a kind of desktop air-conditioning.
Background technology
Desktop small-size fan generally can only blow out the natural wind identical with ambient temperature, can not change the temperature of wind.Therefore, when needs are lowered the temperature, desktop small-size fan can not play good cooling-down effect; When needs heat, desktop small-size fan is idle because not producing hot blast.
In addition, although domestic air conditioning can produce cold wind or hot blast, because its volume is too large, can not place on the table or be moved everywhere, it is convenient not to use.Therefore, domestic air conditioning is is not easily installed and used in indoor office table or less space.
In order to solve the problem, the desktop air-conditioning adopting semiconductor chilling plate to carry out freezing is subject to the favor of consumer, how producing a large amount of products rapidly to satisfy the demands of consumers, is that desktop air-conditioning producer and those skilled in the art need to consider and the technical problem solved.
Utility model content
An object of the present utility model is to provide a kind of desktop air-conditioning that can carry out installing combination fast, to improve its production efficiency.
As far as possible a further object of the present utility model will make accurate positioning between fuselage and base, installation firmly.
In order to realize at least one object above-mentioned, the utility model provides a kind of desktop air-conditioning, comprise base and the fuselage with cooling and warming module, described fuselage is arranged on described base, be configured to suck two mutually isolated air-flows from its perisporium and upwards blow, heat exchange is carried out with described cooling and warming module respectively in the process that two described air-flows upwards blow, temperature when sucking lower than it to make the temperature of an air-flow, become cold wind air-flow, the temperature when temperature of another air-flow is sucked higher than it, become hot-air flow, thus make described desktop air-conditioning blow out described cold wind air-flow and described hot-air flow to different directions.Especially, the outer surface of described base has horizontally outward flange sections that is outstanding, a circumferentially angle, and described flange sections has circumferential detent; Described fuselage also comprises two fuselage half shells, one of them fuselage half shell and another fuselage half shell be adjacent, the common central cavity limiting described fuselage in the horizontal direction, and the bottom of fuselage half shell has the groove section corresponding with described flange sections described in one of them, be provided with the circumference corresponding with the circumferential detent of described flange sections in described groove section and locate floor.
Alternatively, the top surface of described base has at least one positioning convex inserted block; Described fuselage also comprises movement, is arranged in the central cavity of described fuselage, and it has described cooling and warming module, and the lower surface of described movement has at least one locating notch corresponding respectively with each described positioning convex inserted block.
Alternatively, described cooling and warming module comprises the central baffle vertically arranged, and locating notch described at least one is spaced apart and arranged in the lower edge of described central baffle along the length direction of described central baffle.
Alternatively, the quantity of at least one positioning convex inserted block described is 2, and 2 described positioning convex inserted blocks are symmetrical arranged about the central symmetry face of described base.
Alternatively, the top of described two fuselage half shells is connected by buckle.
Alternatively, described cooling and warming module comprises the central baffle vertically arranged; Described two fuselage half shells are respectively first fuselage half shell and the second fuselage half shell with described groove section; Described first fuselage half shell is fixed on the first vertical side of described central baffle, and described second fuselage half shell is fixed on the second vertical side of described central baffle.
Alternatively, to extend internally out multiple screw hole post with screw hole from the inner surface of described first fuselage half shell, the installing hole that multiple screw is each passed through described central baffle screws in corresponding described screw hole post, so that described first fuselage half shell is fixed on described central baffle.
Alternatively, the perisporium bottom of described second fuselage half shell has safeguards opening, the described frame safeguarding opening has multiple installing hole, multiple mounting screw screws in the respective screws hole post in described central baffle through corresponding described installing hole, so that described second fuselage half shell is fixed on described central baffle.
Alternatively, described fuselage also comprises safeguards cover plate, is configured to operationally safeguard opening described in opening and closing.
Alternatively, desktop air-conditioning also comprises cap assembly; Extend two mounting lugs straight down from the lower surface of described cap assembly, each described mounting lug has the locating hole and installing hole that run through its thickness direction; Second vertical side of described central baffle has two mounting grooves corresponding respectively with two mounting lugs, the bottom land of each described mounting groove has locating dowel corresponding with described locating hole and described installing hole respectively and screw hole.
Alternatively, described flange sections is 180 ° in the outer surface angle circumferentially of described base; Described circumferential detent is positioned at the central position of described flange sections.
Alternatively, the bottom of the inner surface of described first fuselage half shell has level inwardly outstanding, circumferentially the lower flat plate section of 180 ° and upper flat plate section, described lower flat plate section and described upper flat plate is intersegmental limits described groove section; The bottom of the inner surface of described second fuselage half shell has level inwardly outstanding, the circumferentially flat plate section of 180 °, and it is concordant with the lower flat plate section of described first fuselage half shell.
Desktop air-conditioning of the present utility model, because the special structure of base and fuselage, significantly improves the installation effectiveness of desktop air-conditioning.
Further, owing to adopting three-point fix, accurate positioning in desktop air-conditioning of the present utility model, installation effectiveness is further increased.
According to hereafter by reference to the accompanying drawings to the detailed description of the utility model specific embodiment, those skilled in the art will understand above-mentioned and other objects, advantage and feature of the present utility model more.
Accompanying drawing explanation
Hereinafter describe specific embodiments more of the present utility model with reference to the accompanying drawings by way of example, and not by way of limitation in detail.Reference numeral identical in accompanying drawing denotes same or similar parts or part.It should be appreciated by those skilled in the art that these accompanying drawings may not be drawn in proportion.In accompanying drawing:
Fig. 1 is the schematic diagram of the desktop air-conditioning according to the utility model embodiment;
Fig. 2 is the schematic cross sectional views of the desktop air-conditioning according to the utility model embodiment;
Fig. 3 is the schematic explosive view of the desktop air-conditioning according to the utility model embodiment;
Fig. 4 is the structure chart of desktop air-conditioning cold wind side fuselage half shell according to the utility model embodiment;
Fig. 5 is the schematic diagram of the desktop air-conditioning maintenance cover plate according to the utility model embodiment;
Fig. 6 is the schematic explosive view of the desktop base plate of air conditioner according to the utility model embodiment;
Fig. 7 is the schematic diagram of the desktop air-conditioning central baffle according to the utility model embodiment;
Fig. 8 is the schematic explosive view of the desktop air-conditioner top cover assembly of root the utility model embodiment.
Detailed description of the invention
Fig. 1 is the schematic diagram of the desktop air-conditioning according to the utility model embodiment.The utility model embodiment provides a kind of small table air-conditioning providing the novel structure of cold wind or hot blast, and it comprises base 100, has the fuselage 200 of cooling and warming module and cap assembly 300.Particularly, fuselage 200 is arranged on base 100, be configured to suck two mutually isolated air-flows from its perisporium and upwards blow, heat exchange is carried out with cooling and warming module respectively in the process that two air-flows upwards blow, temperature when sucking lower than it to make the temperature of an air-flow, becomes cold wind air-flow, the temperature when temperature of another air-flow is sucked higher than it, become hot-air flow, thus enable desktop air-conditioning blow out cold wind air-flow and hot-air flow to different directions.Cap assembly 300 is arranged on the upper end of fuselage 200, is configured to receive cold wind air-flow and hot-air flow respectively from fuselage 200, and makes cold wind air-flow and hot-air flow blow out desktop air-conditioning by different directions.When needs cold wind, cold wind air-flow is mainly used in providing cold wind, and hot-air flow is used for heat radiation.The desktop air-conditioning of the utility model embodiment is because structure is simple, clearly demarcated, compact.
Fig. 2 is the schematic cross sectional views of the desktop air-conditioning of the utility model embodiment.As shown in Figure 2, and with reference to figure 3, in the utility model embodiment, the fuselage 200 of desktop air-conditioning comprises fuselage cover and movement.Movement is arranged in fuselage cover, and movement has cooling and warming module.Cooling and warming module can have at least one semiconductor chilling plate 221, two air-flows and carries out heat exchange directly or indirectly to the corresponding alternating temperature surface of each semiconductor chilling plate 221 respectively and change temperature, to become described cold wind air-flow and described hot-air flow.This desktop air-conditioning, owing to adopting semiconductor chilling plate refrigeration, significantly reduces the noise of desktop air-conditioning, simplifies the structure of desktop air-conditioning, makes desktop air-conditioning miniaturized.
Cooling and warming module also can comprise central baffle 222 and two heat exchangers.Central baffle 222 is vertically arranged, and it has the construction opening running through its thickness direction.At least one semiconductor chilling plate 221 is arranged in construction opening.Heat insulating mattress 223 such as, is installed in construction opening.Heat insulating mattress 223 has the semiconductor accommodation hole that at least one runs through its thickness direction, to hold a corresponding semiconductor cooling piece 221.In the utility model embodiment, the quantity of at least one semiconductor chilling plate 221 can be two, and the central position of heat insulating mattress 223 vertically offers two semiconductor accommodation holes in compartment of terrain.
Two heat exchangers are respectively cold wind side heat exchanger 231 and hot blast side heat exchanger 232.Two heat exchangers are individually fixed in the both sides of central baffle 222, and are folded in therebetween by the Partial Block of at least one semiconductor chilling plate 221 and central baffle 222.Each heat exchanger can comprise substrate and multiple fin vertically extended, and multiple fin in the horizontal direction compartment of terrain is fixed on a vertical side of corresponding substrate.The substrate of each heat exchanger respectively to the corresponding alternating temperature surface contact of each semiconductor chilling plate, so that the Partial Block of at least one semiconductor chilling plate 221 and central baffle 222 is folded in therebetween.
Movement also comprises two centrifugal blowers and two movement half shells.Two centrifugal blowers are respectively cold wind side centrifugal blower 241 and hot blast side centrifugal blower 242.Two centrifugal blowers are individually fixed in two vertical sides of central baffle 222, and each centrifugal blower is positioned at the below of respective heat exchanger, and each centrifugal blower is configured to suck corresponding air flow from its air intake district and upwards blow.
Two movement half shells are respectively cold wind side movement half shell 251 and hot blast side movement half shell 252.Two movement half shells cover respectively and are buckled on two vertical sides of central baffle 222, to form cold air duct and the hot-air channel of two isolation, receive the air-flow from corresponding centrifugal blower respectively, and respectively respective heat exchanger is held within it, in the process upwards blowed, carry out heat exchange with respective heat exchanger to make two air-flows respectively.Wherein, the inner surface of cold wind side movement half shell 251 has reclined heat-insulation layer 253, and the cold produced to prevent each semiconductor chilling plate 221 is diffused into desktop air-conditioning, to improve cryogenic energy utilization rate from cold wind side movement half shell 251.
Fuselage cover comprises the first fuselage half shell and the second fuselage half shell.Particularly, in the utility model embodiment, the first fuselage half shell is hot blast side fuselage half shell 212, second fuselage half shell is cold wind side fuselage half shell 211.Cold wind side fuselage half shell 211 and hot blast side fuselage half shell 212 adjoin in the horizontal direction, jointly limit central cavity in fuselage 200.Such as, hot blast side fuselage half shell 212 is fixed on a vertical side of central baffle 222, and another vertical side of central baffle 222 is fixed in the bottom of cold wind side fuselage half shell 211.The middle and lower part of cold wind side fuselage half shell 211 perisporium is provided with inlet section, cold wind side 213, and the middle and lower part of hot blast side fuselage half shell 212 perisporium is provided with inlet section, hot blast side 214.
The course of work of the desktop air-conditioning of the utility model embodiment is: two centrifugal blowers operate simultaneously, to be entered in centrifugal blower respectively to make two air-flows and is upwards blowed by the inlet section of corresponding fuselage half shell.The cold air duct of two isolation and hot-air channel receive the air-flow from corresponding centrifugal blower respectively, and make two air-flows in cold air duct and hot-air channel, carry out heat exchange with respective heat exchanger respectively in the process upwards blowed, become cold wind air-flow and hot-air flow.After cold wind air-flow and hot-air flow enter cap assembly along cold air duct and hot-air channel respectively, by different directions blowout desktop air-conditioning.
In a preferred embodiment of the present utility model, integral of the scroll casing shape of each movement half shell and corresponding centrifugal blower, to make the spiral case of each centrifugal blower cover the corresponding vertical side being buckled in central baffle 222 together with corresponding movement half shell, thus simplify the structure of movement.The substrate area of hot blast side heat exchanger 232 is greater than the substrate area of cold wind side heat exchanger 231, to improve desktop air-conditioning heat dissipation efficiency and operating efficiency.
For the ease of cold wind air-flow and hot-air flow are imported cap assembly.Movement also comprises cold wind side deflector 261 and hot blast side deflector 262, is fixed on two vertical sides of central baffle 222, and lays respectively at the top of respective heat exchanger respectively by screw, respectively cold wind air-flow and hot-air flow are imported cap assembly 300.
For the ease of the collection of the condensed water that desktop air-conditioning produces, cold wind side heat exchanger 231 is also configured to condensate water guide that it produces to its lower end minimum point, movement also comprises condensation water collection structure, be arranged on the below of cold wind side heat exchanger 231, be configured to accept the condensed water from cold wind side heat exchanger 231 drippage, and make the condensed water of undertaking come together in the first side in fuselage cover.The lower edge of each fin of cold wind side heat exchanger 231 is towards the downward-sloping hypotenuse of corresponding substrate.The lower surface of the substrate of cold wind side heat exchanger 231 only comprises the plane towards the inclined-plane of the downward-sloping lower edge through each fin of central baffle 222 and the lower sideline through inclined-plane.
Condensation water collection structure has collecting tray 271 and collecting box 272.Collecting tray 271 to be fixed in central baffle 222 and to be in the below of the lower end minimum point of cold wind side heat exchanger 231, to accept the condensed water from cold wind side heat exchanger 231 drippage.The water inlet of collecting box 272 is positioned at the vertical below of the delivery port of collecting tray 271 so that collecting tray 271 by accept condensate water guide to collecting box 272.
In embodiments more of the present utility model, cold wind side fuselage half shell 211 perisporium has and safeguards opening and be formed in the baffle plate 215 safeguarded in opening, baffle plate 215 offers inlet section, cold wind side 213, it is communicated with the air inlet of cold wind side centrifugal blower 241.Fuselage 100 also has safeguards cover plate 280, be configured to operationally opening and closing and safeguard opening, it has cover plate inlet section 281, safeguard and form gas channel between cover plate 280 and baffle plate 215, to receive the air-flow from cover plate inlet section 281, and by the inlet section, cold wind side 213 on baffle plate 215 to supply air flow in cold wind side fuselage half shell 211, then by the air inlet of cold wind side centrifugal blower 241 to supply air flow in cold wind side centrifugal blower 241.Gas channel is formed, to receive the air-flow of inlet section, Self-air-heating side 214, and by the air inlet of hot blast side centrifugal blower 242 to supply air flow in hot blast side centrifugal blower 242 between the spiral case of hot blast side fuselage half shell 212 and hot blast side centrifugal blower 242.Main wind inlet channel and wind inlet channel diffusion region that gas channel comprises hot blast side centrifugal blower 242 is formed between the spiral case of hot blast side fuselage half shell 212 and hot blast side centrifugal blower 242.
Movement also can comprise Detection of Air Quality module 224 and Temperature and Humidity module.Detection of Air Quality module 224 is fixed in central baffle 222, and be in the below of hot blast side centrifugal blower 242 and the wind inlet channel diffusion region of hot blast side centrifugal blower 242, to detect air quality according to the air-flow in the wind inlet channel diffusion region of hot blast side centrifugal blower 242.Detection of Air Quality mould 224 pieces generally adopts PM2.5 checkout gear and/or VOC sensor.Temperature and Humidity module is fixed in central baffle 222, and be in the below of hot blast side centrifugal blower 242 and the wind inlet channel diffusion region of hot blast side centrifugal blower 242, to detect the temperature and humidity of air according to the air-flow in the wind inlet channel diffusion region of hot blast side centrifugal blower 242.
In embodiments more of the present utility model, as shown in Figure 4, for the ease of picking and placeing of filter and collecting box, baffle plate 215 has in the radial outer periphery of its air inlet one or more floor extended in corresponding air flow passage, one or more floor surrounds ring, to place screen pack or filtration membrane 283 in ring.Every bar floor and safeguard to have gap between cover plate 280, to allow to safeguard the inlet section, cold wind side 213 on the air flow direction baffle plate 215 in the gas channel that formed between cover plate 280 and baffle plate 215.Baffle plate 215 comprises and has the vertical plate portion of inlet section, cold wind side 213 and the horizontal side in vertical plate portion to the recessed collecting box accommodating cavity formed.The lower limb that baffle plate 215 also comprises vertical connecting plate portion and the horizontal plate part of lower limb safeguarding opening.Spaced apart vertical between horizontal plate part and ring, with devices such as sandwiched champignon modules betwixt.
Safeguard cover plate inlet section 281 on cover plate 280 for safeguard cover plate 280 perisporium on a circumferentially angle and there is the ribbon perisporium section of multiple eyelet.Inlet section, cold wind side 213 is a grid type air port.Inlet section, hot blast side 214 be hot blast side fuselage half shell 212 perisporium on a circumferentially angle and there is the ribbon perisporium section of multiple eyelet, and concordant, not only attractive in appearance with cover plate inlet section 281, inlet section, cold wind side 213 etc., and intake is large.
For the ease of safeguarding dismounting and the installation of cover plate, safeguarding that the upper ledge edge of opening has at least one block button hole, safeguarding the magnet ring 216 that the bottom of opening is provided with at least one and has central annular distance.As shown in Figure 5, safeguard that the upper end-face edge of cover plate 280 has the convex tongue 282 of at least one corresponding with each block button hole respectively buckle, bottom has at least one corresponding with each magnet ring 216 respectively magnetic absorption member 285, such as magnet ring or magnet.Safeguard that cover plate 280 also has at least one the installation projection 284 extended from its inner surface, each magnetic absorption member 285 is fixed on the end of a corresponding installation projection 284.The quantity of the convex tongue 282 of at least one buckle is two, and two convex tongues of buckle 282 are about safeguarding that the vertical plane of symmetry of the central authorities of cover plate 280 is arranged symmetrically.At least one quantity of installing projection 284 is two, installs projection 284 about safeguarding that the vertical plane of symmetry of the central authorities of cover plate 280 is arranged symmetrically for two.Each magnet ring 216 can be fixed on baffle plate 215.Multiple mounting screw screws in central baffle 222 through after corresponding magnet ring 216 and baffle plate 215 respectively successively.Safeguarding that the position of the upper ledge edge of opening with two the side frame intersect edge safeguarding opening is also provided with installing hole, two mounting screws are each passed through the corresponding mounting hole and screw in central baffle 222.That is, the frame safeguarding opening has multiple installing hole, multiple mounting screw screws in the respective screws hole post in central baffle, so that cold wind side fuselage half shell 211 is fixed on central baffle 222 through the corresponding mounting hole.
For the ease of Long-distance Control, movement also comprises wifi module 226, and it is fixed in central baffle 222, and is in the below of hot blast side centrifugal blower 242, realizes Based Intelligent Control to be connected with the intelligent terminal such as mobile phone, computer.For the ease of carrying out sterilization processing to the cold wind air-flow formed, movement has anion generation module 227 further.The ion generation end of anion generation module 227 is arranged in central baffle, and the emission of ions brush of anion generation module 227 is fixed on the madial wall of cold wind side movement half shell 251.
Fig. 6 is the schematic explosive view of the desktop base plate of air conditioner of root the utility model embodiment, in the utility model embodiment, the base 100 of desktop air-conditioning comprises base plate 110 and covers the seat cover 120 be buckled on base plate 110, central cavity is limited between base plate 110 and seat cover 120, the roof of central cavity has threading opening, with the fuselage cavity connects with desktop air-conditioning.Desktop air-conditioning in the utility model embodiment also has main control board 130, is arranged in central cavity.Base plate 110 lower surface is provided with antiskid, shock-absorbing pad 140, is convenient to the placement of desktop air-conditioning.
Cover 120 inner surfaces from seat and extend many roots bar 121 straight down, the lower limb of every root bar 121 and the upper surface of main control board 130 are conflicted.Cover 120 inner surfaces from seat and extend at least one locating dowel 122 straight down; At least one boss 111 with positioning jack is extended straight up from base plate 110 upper surface.The corresponding positioning through hole that each locating dowel 122 passes main control board 130 inserts the positioning jack of a corresponding boss 111, and the upper surface of each boss contacts with the lower surface of main control board 130.Cover 120 inner surfaces from seat and extend multiple screw hole post straight down, multiple screw is each passed through base plate 110 and screws in respective screws hole post, so that base plate 110 is fixed on seat cover 120.The circumferential exterior surface of each screw hole post contacts against with the circumferential edge of main control board 130 respectively.The circumferential side wall of base 100 is also provided with power line connection-peg, to power to main control board 130.
Coordinate for the ease of the installation between base with fuselage, to improve the installation effectiveness of desktop air-conditioning, the outer surface of base 100 has horizontally outward flange sections 123 that is outstanding, a circumferentially angle, and flange sections 123 has circumferential detent.The bottom of hot blast side fuselage half shell 212 has the groove section 217 corresponding with flange sections 123, is provided with the circumference corresponding with the circumferential detent of flange sections 123 and locates floor in groove section 217.During installation, first hot blast side fuselage half shell 212 is fixed on a vertical side of central baffle 222, to form the first pre-arrangement; The base 100 of desktop air-conditioning is inserted the first pre-arrangement, groove section 217 is inserted to make the flange sections 123 of base 100, and make the circumferential detent in the location of the circumference in groove section 217 floor insertion flange sections 123, thus realize the quick position between base 100 and fuselage 200.
In order to improve location efficiency and firm position further, as shown in Figure 7, the top surface of base 100 has at least one positioning convex inserted block 124.The lower surface of movement has at least one locating notch 228 corresponding respectively with each positioning convex inserted block 124.Such as, the quantity of at least one positioning convex inserted block 124 is 2, and 2 positioning convex inserted blocks 124 are symmetrical arranged about the central symmetry face of base 100.2 locating notches 228 can be spaced apart and arranged in the lower edge of central baffle 222 along the length direction of central baffle 222.Three-point fix, significantly improves the location efficiency between base and fuselage, makes follow-up easier for installation.
In order to improve the installation fixed efficiency between two fuselage half shells further, the top of two fuselage half shells is connected by buckle, to reduce the operation complexity of the installation between two fuselage half shells.To extend internally out multiple screw hole post with screw hole from the inner surface of hot blast side fuselage half shell 212, the installing hole that multiple screw is each passed through central baffle 222 screws in respective screws hole post, so that hot blast side fuselage half shell 212 is fixed on central baffle 222.During installation, hot blast side fuselage half shell 212 is fixed on a vertical side of central baffle 222.The top card of cold wind side fuselage half shell 211 is connected to the top of hot blast side fuselage half shell 212.Another vertical side of central baffle 222 is fixed in the bottom of cold wind side fuselage half shell 211.Safeguard that cover plate 280 is covered on and safeguard opening.The inner surface of the desktop air-conditioning fuselage cover of this embodiment does not have screw, and desktop air-conditioning can be made attractive in appearance.
In the utility model preferred embodiment, flange sections 123 is 180 ° in the outer surface angle circumferentially of base 100.Circumference detent is positioned at the central position of flange sections 123.The bottom of the inner surface of hot blast side fuselage half shell 212 has level inwardly outstanding, circumferentially the lower flat plate section of 180 ° and upper flat plate section, lower flat plate section and upper flat plate is intersegmental limits groove section 217.The bottom of the inner surface of cold wind side fuselage half shell 211 has level inwardly outstanding, the circumferentially flat plate section of 180 °, and it is concordant with the lower flat plate section of hot blast side fuselage half shell 212.
Fig. 8 is the schematic explosive view of the desktop air-conditioner top cover assembly according to the utility model embodiment, in the utility model embodiment, cap assembly 300 comprises air channel base plate 310 and air channel top board 320, wherein, air channel base plate 310 there is horizontal part and upwards extend from the circumferential edge of horizontal part, the lower air dam 311 of the equal flaring of circumferential inside and outside contour, the horizontal part of air channel base plate 310 offers cold wind import 312 and hot wind inlet 313, to receive cold wind air-flow and hot-air flow respectively.Air channel top board 320 have the equal flaring of that extend from bottom to top, circumferential inside and outside contour upper air dam 321 and from the circumferential exterior surface of upper air dam 321 to multiple floors 322 of downward-extension.The circumferential inner surface of lower air dam 311, the circumferential exterior surface of upper air dam 321, and two opposite flanks of two floors 322 being positioned at cold wind import 312 both sides surround cold wind blowout air channel.The circumferential inner surface of lower air dam 311, the circumferential exterior surface of upper air dam 321, and two opposite flanks of two floors 322 being positioned at hot wind inlet 313 both sides surround hot blast blowout air channel.Especially, be oppositely arranged before and after the cold wind outlet in cold wind blowout air channel and the hot-blast outlet in hot blast blowout air channel, namely be oppositely arranged before and after the cold wind outlet of cap assembly 300 and hot-blast outlet, to make opposingly before and after cold wind air-flow and hot-air flow liftoffly to blow out desktop air-conditioning.Lower air dam 311 is also provided with case ring 315.
Cap assembly also can comprise: the light guide plate 330 set gradually from bottom to top, leaded light cover plate 340 and display touch pad 350, luminous circuit board 360 and input/output control circuit plate 370.Light guide plate 330 is arranged on the top of air channel top board 320.Luminous circuit board 360 is posted by the horizontal part of air channel base plate 310 by the central stepped through hole of air channel top board 320, and at least one electroluminescent lamp on luminous circuit board 360 enters in the light groove of light guide plate 330, to be injected in light guide plate 330 by the light sent when light-emitting component is energized through the central stepped through hole on air channel top board 320.Input/output control circuit plate 370 is arranged on leaded light and covers between plate 340 and display touch pad 350.
Electroluminescent lamp on luminous circuit board 360 sends the light of different colours according to different air quality grades, is guided by light guide plate 330.Leaded light is covered plate 340 and is configured to hide the portion of upper surface of light guide plate 330, to make when light-emitting component is energized, is not covered by leaded light the surface formation ring of light that plate 340 hides at light guide plate 330 upper surface.
Display touch pad 350 is configured to show information to user and receive the operation of user.The touch operation that user can carry out has start-stop to operate, opens refrigerating operation, opens pushing wind manipulation, improves wind speed operation and reduce wind speed operation etc.Display touch pad can show the information such as the temperature of current environment, humidity, collecting box water level and wireless signal.Display touch pad is arranged on the top of desktop air-conditioning, can be convenient to user while sitting down, take advantage of a situation and press switch, and it is convenient to control.
Form a whole to make each plate of cap assembly 300, extend multiple screw hole post 351 with screwed hole straight down from the lower surface of display touch pad 350, every root screw hole post is covered plate 340, light guide plate 330, air channel top board 320 and luminous circuit board 350 and is fixed on air channel base plate 310 through input/output control circuit plate 370, leaded light by screw successively.
Coordinate for the ease of the installation between cap assembly 300 with fuselage 200, extend two mounting lugs 314 straight down from the lower surface of cap assembly 300, each mounting lug 314 has the locating hole and installing hole that run through its thickness direction.The vertical side, cold wind side of central baffle 222 has two mounting grooves 229 corresponding respectively with two mounting lugs 314, the bottom land of each mounting groove 229 has locating dowel corresponding with locating hole and installing hole respectively and screw hole.
According to another aspect of the present utility model, the utility model additionally provides a kind of installation method for any one desktop air-conditioning above-mentioned.This installation method comprises: movement fuselage half shell with groove section 217 of desktop air-conditioning being fixed on desktop air-conditioning, to form the first pre-arrangement.The base 100 of desktop air-conditioning is inserted the first pre-arrangement, to make the flange sections 123 of base 100 insert groove section 217, and make the circumferential detent in the location of the circumference in groove section 217 floor insertion flange sections 123.
In this utility model embodiment, before the pre-arrangement of formation first, first all parts assembling in movement is formed this movement, it has the installation steps of two heat exchangers.Particularly, two heat exchanger installation processes can be: utilize screw hot blast side heat exchanger 232 to be fixed on a vertical side of central baffle 222.Heat insulating mattress 223 is placed in the construction opening of central baffle 222.The cold surface of each semiconductor chilling plate 221 and hot surface are smeared heat-conducting silicone grease, and each semiconductor chilling plate 221 is positioned in corresponding semiconductor holding tank, and the substrate contacts of the hot surface of each semiconductor chilling plate 221 and hot blast side heat exchanger.Cold wind side heat exchanger 231 is placed on another vertical side of central baffle.One end inner surface of Z-type pressing plate is pasted heat insulation foam, and is posted by the substrate of cold wind side heat exchanger 231, utilized by the other end of Z-type pressing plate screw to be fixed on the substrate of hot blast side heat exchanger 232.In alternate embodiment more of the present utility model, screw can be utilized cold wind side heat exchanger 231 to be directly fixed on another vertical side of central baffle 222.Two vertical sides of central baffle 222 all can have the substrate recess of depression, so that the location of two heat exchangers.
Also comprised insert the first pre-arrangement after the pre-arrangement of formation first and by base 100 before: the central baffle cap assembly 300 of desktop air-conditioning being installed on movement.Also comprise after base 100 being inserted the first pre-arrangement: the top top card of cold wind side fuselage half shell 211 of desktop air-conditioning being connected to hot blast side fuselage half shell 212.Cold wind side fuselage half shell 211 is fixed on the central baffle 222 of movement.Insert collecting box 272, and place filter and/or champignon etc.Finally cover and safeguard cover plate 280.
So far, those skilled in the art will recognize that, although multiple exemplary embodiment of the present utility model is illustrate and described herein detailed, but, when not departing from the utility model spirit and scope, still can directly determine or derive other modification many or amendment of meeting the utility model principle according to content disclosed in the utility model.Therefore, scope of the present utility model should be understood and regard as and cover all these other modification or amendments.

Claims (12)

1. a desktop air-conditioning, comprise base and the fuselage with cooling and warming module, described fuselage is arranged on described base, be configured to suck two mutually isolated air-flows from its perisporium and upwards blow, heat exchange is carried out with described cooling and warming module respectively in the process that two described air-flows upwards blow, temperature when sucking lower than it to make the temperature of an air-flow, become cold wind air-flow, the temperature when temperature of another air-flow is sucked higher than it, become hot-air flow, thus make described desktop air-conditioning blow out described cold wind air-flow and described hot-air flow to different directions, it is characterized in that,
The outer surface of described base has horizontally outward flange sections that is outstanding, a circumferentially angle, and described flange sections has circumferential detent;
Described fuselage also comprises two fuselage half shells, one of them fuselage half shell and another fuselage half shell be adjacent, the common central cavity limiting described fuselage in the horizontal direction, and the bottom of fuselage half shell has the groove section corresponding with described flange sections described in one of them, be provided with the circumference corresponding with the circumferential detent of described flange sections in described groove section and locate floor.
2. desktop air-conditioning according to claim 1, is characterized in that,
The top surface of described base has at least one positioning convex inserted block;
Described fuselage also comprises movement, is arranged in the central cavity of described fuselage, and it has described cooling and warming module, and the lower surface of described movement has at least one locating notch corresponding respectively with each described positioning convex inserted block.
3. desktop air-conditioning according to claim 2, is characterized in that, described cooling and warming module comprises:
The central baffle vertically arranged, locating notch described at least one is spaced apart and arranged in the lower edge of described central baffle along the length direction of described central baffle.
4. desktop air-conditioning according to claim 2, is characterized in that,
The quantity of at least one positioning convex inserted block described is 2, and 2 described positioning convex inserted blocks are symmetrical arranged about the central symmetry face of described base.
5. desktop air-conditioning according to claim 1, is characterized in that,
The top of described two fuselage half shells is connected by buckle.
6. desktop air-conditioning according to claim 5, is characterized in that,
Described cooling and warming module comprises the central baffle vertically arranged;
Described two fuselage half shells are respectively first fuselage half shell and the second fuselage half shell with described groove section;
Described first fuselage half shell is fixed on the first vertical side of described central baffle, and described second fuselage half shell is fixed on the second vertical side of described central baffle.
7. desktop air-conditioning according to claim 6, is characterized in that,
To extend internally out multiple screw hole post with screw hole from the inner surface of described first fuselage half shell, the installing hole that multiple screw is each passed through described central baffle screws in corresponding described screw hole post, so that described first fuselage half shell is fixed on described central baffle.
8. desktop air-conditioning according to claim 6, is characterized in that,
The perisporium bottom of described second fuselage half shell has safeguards opening, the described frame safeguarding opening has multiple installing hole, multiple mounting screw screws in the respective screws hole post in described central baffle through corresponding described installing hole, so that described second fuselage half shell is fixed on described central baffle.
9. desktop air-conditioning according to claim 8, is characterized in that,
Described fuselage also comprises safeguards cover plate, is configured to operationally safeguard opening described in opening and closing.
10. desktop air-conditioning according to claim 6, is characterized in that, also comprise cap assembly;
Extend two mounting lugs straight down from the lower surface of described cap assembly, each described mounting lug has the locating hole and installing hole that run through its thickness direction;
Second vertical side of described central baffle has two mounting grooves corresponding respectively with two mounting lugs, the bottom land of each described mounting groove has locating dowel corresponding with described locating hole and described installing hole respectively and screw hole.
11. desktop air-conditionings according to claim 6, is characterized in that,
Described flange sections is 180 ° in the outer surface angle circumferentially of described base;
Described circumferential detent is positioned at the central position of described flange sections.
12. desktop air-conditionings according to claim 11, is characterized in that,
The bottom of the inner surface of described first fuselage half shell has level inwardly outstanding, circumferentially the lower flat plate section of 180 ° and upper flat plate section, described lower flat plate section and described upper flat plate is intersegmental limits described groove section;
The bottom of the inner surface of described second fuselage half shell has level inwardly outstanding, the circumferentially flat plate section of 180 °, and it is concordant with the lower flat plate section of described first fuselage half shell.
CN201420521468.0U 2014-09-11 2014-09-11 Desktop air-conditioning Withdrawn - After Issue CN204141738U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420521468.0U CN204141738U (en) 2014-09-11 2014-09-11 Desktop air-conditioning

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420521468.0U CN204141738U (en) 2014-09-11 2014-09-11 Desktop air-conditioning

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CN201420521468.0U Withdrawn - After Issue CN204141738U (en) 2014-09-11 2014-09-11 Desktop air-conditioning

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104266266A (en) * 2014-09-11 2015-01-07 青岛海尔空调器有限总公司 Table top air conditioner and mounting method thereof
CN106839226A (en) * 2017-03-29 2017-06-13 虞扬 Semiconductor cold-warm energy-conserving and environment-protective VMC based on Internet of Things
CN107041091A (en) * 2017-05-07 2017-08-11 江苏绿阳新能源科技有限公司 A kind of high frequency type intelligent power converter

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104266266A (en) * 2014-09-11 2015-01-07 青岛海尔空调器有限总公司 Table top air conditioner and mounting method thereof
CN104266266B (en) * 2014-09-11 2017-04-19 青岛海尔空调器有限总公司 Table top air conditioner and mounting method thereof
CN106839226A (en) * 2017-03-29 2017-06-13 虞扬 Semiconductor cold-warm energy-conserving and environment-protective VMC based on Internet of Things
CN107041091A (en) * 2017-05-07 2017-08-11 江苏绿阳新能源科技有限公司 A kind of high frequency type intelligent power converter
CN107041091B (en) * 2017-05-07 2019-09-17 江苏绿阳新能源科技有限公司 A kind of high frequency type intelligent power converter

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