CN1979050A - Air conditioner - Google Patents

Air conditioner Download PDF

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Publication number
CN1979050A
CN1979050A CNA2006100665848A CN200610066584A CN1979050A CN 1979050 A CN1979050 A CN 1979050A CN A2006100665848 A CNA2006100665848 A CN A2006100665848A CN 200610066584 A CN200610066584 A CN 200610066584A CN 1979050 A CN1979050 A CN 1979050A
Authority
CN
China
Prior art keywords
grid
suction
air conditioner
suction inlet
fuselage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CNA2006100665848A
Other languages
Chinese (zh)
Inventor
金晋伯
牟珍勇
韩在五
金荣宰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Samsung Electronics Co Ltd
Original Assignee
Samsung Electronics Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Samsung Electronics Co Ltd filed Critical Samsung Electronics Co Ltd
Publication of CN1979050A publication Critical patent/CN1979050A/en
Pending legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00—Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/28—Arrangement or mounting of filters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00—Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08—Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00—Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08—Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10—Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/12—Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of sliding members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00—Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/20—Casings or covers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F2221/00—Details or features not otherwise provided for
    • F24F2221/36—Modules, e.g. for an easy mounting or transport

Abstract

The invention discloses an air conditioner, having a vacuum filter for strengthening structure to reduce components number of the air conditioner, to joint and separate easily. The air conditioner air conditioner including: airframe with a suction inlet; a suction grate set on the suction inlet and a vacuum filter integrated with the suction grate. The suction grate and the suction inlet joint glidable.

Description

Air conditioner
Technical field
The present invention relates to a kind of air conditioner, more particularly, the present invention relates to a kind of suction filter separation and easy air conditioner of combination of making.
Background technology
Disclosed air conditioner is provided with suction filter in (putting down) 08-285312 Japan Patent is open, and this suction filter can filter out the airborne exterior materials that is inhaled in the air conditioner.The purpose that suction filter is set on the air conditioner is: in the time of in air is inhaled into air conditioner, prevent that by filtering out dust in air dust is accumulated in the heat exchanger.
Before being releasably attached to, the suction filter of air conditioner sucks the rear side of grid.Like this, when cleaning or replacement suction filter, after opening the suction grid that is positioned at the air conditioner front side, suction filter is separated.
Yet, the problem of disclosed air conditioner is, because suction filter and preceding suction grid are as independent parts setting, so air conditioner has many parts, and, must open or separate the preceding grid that sucks in advance owing to will clean or replace suction filter, so cleaning or replacement suction filter trouble.
Summary of the invention
Therefore, an aspect of of the present present invention is to provide a kind of air conditioner with the suction filter that structurally strengthens, to reduce the number of air conditioner parts.
Another aspect of the present invention is to provide a kind of combination easily and the air conditioner that separates suction filter.
For others of the present invention and/or advantage, a part will be set forth in the following description, and a part is apparent by description, and perhaps can understand by implementing the present invention.
Above-mentioned and others of the present invention realize that by a kind of air conditioner is provided described air conditioner comprises: fuselage has suction inlet; Suck grid, be set on the suction inlet, and have and suck the suction filter that grid forms.
Preferably, sucking grid combines slidably with suction inlet.
Preferably, air conditioner also comprises the guide rail that combines slidably with suction inlet and suction grid, thereby separates with fuselage by sucking grid along horizontal promotion suction grid.
Preferably, during forming the technology that sucks grid by injection molding, suction filter forms with the suction grid.
According to a further aspect in the invention, air conditioner comprises: fuselage has suction inlet; Suck grid, combine slidably with the suction inlet of fuselage.
According to a further aspect in the invention, air conditioner comprises: fuselage, second floss hole that has the suction inlet that forms at rear side, first floss hole that forms on the top of front side and form in the bottom of described front side; Heat exchanger is arranged on the rear portion in the fuselage; First blower fan and second blower fan are used for blowing air by heat exchanger to first floss hole and second floss hole; Suck grid, combine, and comprise and suck the suction filter that grid forms with suction inlet
Preferably, suction inlet comprises first suction inlet and second suction inlet, first suction inlet forms on the top of the described rear side of fuselage, second suction inlet forms in the bottom of the described rear side of fuselage, sucks grid and comprises respectively with first suction inlet and second suction inlet combine slidably and first suck grid and second and suck grid.
Preferably, air conditioner also comprises with first and sucks grid and second and suck the guide rail that the top and bottom of the top and bottom of grid and first suction inlet and second suction inlet combine slidably, thus by at the either side of fuselage along laterally promoting to suck the separable suction grid of grid.
Description of drawings
By the description of embodiment being carried out below in conjunction with accompanying drawing, these and/or others of the present invention and advantage will become clear and be easier to and understand, wherein:
Fig. 1 is the sectional view that the internal structure of air conditioner according to an embodiment of the invention is shown;
Fig. 2 is the front view of air conditioner;
Fig. 3 is the detail drawing of the circle III that shows among Fig. 1;
Fig. 4 is the perspective view that the rear side of air conditioner is shown.
The specific embodiment
To describe embodiments of the invention in detail now, its example is shown in the drawings.Embodiment is described to explain the present invention hereinafter with reference to accompanying drawing.
With reference to Fig. 1, air conditioner according to the present invention has rear side 11 and is fixed to fuselage 10 on the wall of building.The fuselage 10 of air conditioner has first suction inlet 12 and second suction inlet 13 that forms in the upper and lower of described rear side, and first floss hole 14 and second floss hole 15 that form in the upper and lower of front side.
As shown in figures 1 and 3, the upper and lower that is formed with the described rear side 11 of first suction inlet 12 and second suction inlet 13 thereon tilts, thereby when fuselage 10 is fixed on the wall, first suction inlet 12 and second suction inlet 13 separate with the wall of building, to suck room air by first suction inlet 12 and second suction inlet 13.Here, although air conditioner is shown as two suction inlets that have in upper and lower formation in Fig. 1, as long as the described rear side and the wall of fuselage separate, air conditioner can only have a suction inlet.
As shown in Figure 2, first floss hole 14 and second floss hole 15 transversely prolong in the upper and lower of the front side of fuselage 10 respectively.This structure allows to pass through first floss hole 14 to the top in room discharged air, passes through second floss hole 15 simultaneously to the bottom in room discharged air.
As shown in Figure 1, fuselage 10 is provided with heat exchanger 16 and first blower fan 17 and second blower fan 18 therein, heat exchanger 16 is positioned at the position at the rear portion that is close to first suction inlet 12 and second suction inlet 13, and first blower fan 17 and second blower fan 18 are positioned at the upside and the downside of the front of heat exchanger 16.In addition, fuselage 10 is provided with first ways 21 and first stabilizer 22 and second ways 23 and second stabilizer 24 therein, the air that first ways 21 and second stabilizer 22 are used for being blowed by first blower fan 17 is directed to first floss hole 14, and the air that second ways 23 and second stabilizer 24 are used for being blowed by second blower fan 18 is directed to second floss hole 15.
Heat exchanger 16 separates with the described rear side of fuselage 10.In addition, heat exchanger 16 comprises middle heat interchanger 16a, goes up heat exchanger 16b and following heat exchanger 16c, makes heat exchanger 16b and following heat exchanger 16c respectively from the top and bottom bending of middle part heat exchanger 16a and the corresponding predetermined angular in inclined-plane of first suction inlet 12 and second suction inlet 13.
Each of first blower fan 17 and second blower fan 18 comprises typical aerofoil fan.Although do not show in the accompanying drawings, first blower fan 17 is driven by different drive motors with second blower fan 18.Therefore, the controller (not shown) control drive motors of air conditioner is operated first blower fan 17 and second blower fan 18 simultaneously, perhaps optionally operate first blower fan 17 and second blower fan 18, perhaps one after the other operate first blower fan 17 and second blower fan 18.In addition, first blower fan 17 can have identical size with second blower fan 18, so that the air of first floss hole 14 and second floss hole, 15 discharging equivalent, first blower fan 17 and second blower fan 18 also can be of different sizes, so that the air of first floss hole 14 and second floss hole, 15 discharging inequalities.
First ways 21 extends to the top of first blower fan 17 from the upper end of first floss hole 14, and centers on the top of first blower fan 17.First stabilizer 22 extends to the part adjacent with first blower fan 17 from the lower end of first floss hole 14.Therefore, the air that is blowed by first blower fan 17 can be directed into first floss hole 14 on the top that is positioned at fuselage 10.
Second ways 23 extends to the top of second blower fan 18 from the upper end of second floss hole 15, and centers on the top of second blower fan 18.In other words, the structure of second ways 23 is divided into upper space and lower space with the inner space of fuselage 10, and first blower fan 17 is arranged in described upper space, and second blower fan 18 is arranged in described lower space.Separate with heat exchanger 16 rear end of second ways 23.Second stabilizer 24 extends to the part adjacent with second blower fan 18 from the lower end of second floss hole 15.Therefore, the air that is blowed by second blower fan 18 can be directed into second floss hole 15 of the bottom that is positioned at fuselage 10.
Second ways 23 has downward-sloping angle [alpha] 2, this angle is greater than the angle [alpha] of first ways 21 1Second stabilizer 24 also has downward-sloping angle beta 2, the angle beta of about first stabilizer 22 of this angle 1The purpose that designs this structure is to be discharged into distant location by the air that first floss hole 14 blows, and the air that blows by second floss hole 15 is discharged into closely and locates simultaneously.
Air conditioner also comprises removably being attached to respectively and sucks grid 31 and second at first of first suction inlet 12 of the rear side of fuselage 10 and second suction inlet 13 and suck grid 32, as shown in Figure 3 and Figure 4.First sucks grid 31 and second sucks the upper and lower that each upper and lower of grid 32 is attached to first suction inlet 12 and second suction inlet 13 respectively slidably.In other words, as shown in Figure 3, first each that sucks the grid 31 and the second suction grid 32 has channled rail 33a and 33b, described guide rail 33a and 33b suck grid 31 and second top and bottom that suck grid 32 are extended along the longitudinal first, and engage with each the guide rail 34a and the 34b of top and bottom that is arranged on first suction inlet 12 and second suction inlet 13 respectively.Therefore, as shown in Figure 4, it can be separated by sucking grid 32 to the both sides of the fuselage 10 promotion first suction grid 31 and second.
According to this structure, be fixed at fuselage 10 under the state on the wall of building, by along laterally pushing away or drawing first to suck grid 31 and second and suck grid 32 and can suck grid 31 and second with first and suck grid 32 and separate or combination with air conditioner.In addition, this structure allows the first suction grid 31 and the second suction grid 32 to separate from the both sides of fuselage 10, thereby can with first suck grid 31 and second suck grid 32 from the user easily a side (that is, not with other parts or the side of conflicting on every side) separate.
As shown in Figure 3, the first suction grid 31 and second sucks grid 32 and is provided with suction filter 36 integratedly, and this suction filter 36 can filter out the exterior materials in the inhaled air.Suck the technology that grid 31 and second sucks grid 32 by injection molding molded of resin material first, suction filter 36 sucks grid 31 with first respectively and the second suction grid 32 forms.In other words, come molded suction grid 31 and 32 in the mould that is associated by each suction filter 36 is embedded in, suction filter 36 forms with suction grid 31 and 32.
Like this, because suction filter forms with sucking grid 31 and 32,, can reduce the number of air conditioner parts so compare with the traditional air conditioner that sucks grid with having independent suction filter.In addition, when any suction filter 36 of cleaning, sucking grid 31 and/or 32 by separation can separate with the suction filter 36 that sucks grid 31 and/or 32, thereby can easily carry out the cleaning of suction filter 36.
Be clear that from above description,, can reduce part count so compare with traditional air conditioner because air conditioner of the present invention comprises the suction filter of parts as a whole and suck grid.
In addition, because the global facility of suction filter and suction grid combines slidably with fuselage, can easily separate or combination so suck grid, and suction filter can be separated with fuselage, thereby easily suction filter be cleaned by only separating the suction grid with fuselage.
Although shown and described some embodiments of the present invention, but those skilled in the art are to be understood that, without departing from the principles and spirit of the present invention, can carry out various modifications, increase and replacement to these embodiment, scope of the present invention is limited by claim and equivalent thereof.
The application requires to be submitted on December 9th, 2005 rights and interests of the 2005-0121020 korean patent application of Korea S Department of Intellectual Property, and it openly is contained in this by reference.

Claims (8)

1, a kind of air conditioner comprises: fuselage has suction inlet; Suck grid, be arranged on the described suction inlet, and have the suction filter that forms with this suction grid.
2, air conditioner as claimed in claim 1, wherein, described suction grid combines slidably with described suction inlet.
3, air conditioner as claimed in claim 2 also comprises the guide rail that combines slidably with described suction inlet and described suction grid, thereby by along laterally promoting described suction grid it being separated with described fuselage.
4, air conditioner as claimed in claim 1, wherein, during the technology that forms described suction grid by injection molding in, described suction filter and described suction grid form.
5, a kind of air conditioner comprises: fuselage has suction inlet; Suck grid, combine slidably with the described suction inlet of described fuselage.
6, a kind of air conditioner comprises: fuselage, second floss hole that has the suction inlet that forms at rear side, first floss hole that forms on the top of front side and form in the bottom of described front side; Heat exchanger is arranged on the rear portion in the fuselage; First blower fan and second blower fan are used for blowing air by described heat exchanger to described first floss hole and described second floss hole; Suck grid, combine with described suction inlet, and have the suction filter that forms with this suction grid.
7, air conditioner as claimed in claim 6, wherein, second suction inlet that described suction inlet is included in first suction inlet that the top of the described rear side of described fuselage forms and forms in the bottom of the described rear side of described fuselage, and described suction grid comprises respectively with described first suction inlet and described second suction inlet combine slidably and first sucks grid and second and suck grid.
8, air conditioner as claimed in claim 7, also comprise guide rail, described guide rail and described first sucks the grid and the top and bottom of the described second suction grid and the top and bottom of described first suction inlet and described second suction inlet and combines slidably, thereby it can be separated along laterally promoting described suction grid by the either side at described fuselage.
CNA2006100665848A 2005-12-09 2006-04-03 Air conditioner Pending CN1979050A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR1020050121020 2005-12-09
KR1020050121020A KR20070060876A (en) 2005-12-09 2005-12-09 Air conditioner

Publications (1)

Publication Number Publication Date
CN1979050A true CN1979050A (en) 2007-06-13

Family

ID=38130307

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2006100665848A Pending CN1979050A (en) 2005-12-09 2006-04-03 Air conditioner

Country Status (3)

Country Link
KR (1) KR20070060876A (en)
CN (1) CN1979050A (en)
IT (1) ITTO20060243A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102917837A (en) * 2010-06-03 2013-02-06 大金工业株式会社 Oil cooling device
CN103062836A (en) * 2011-10-20 2013-04-24 Lg电子株式会社 Indoor unit of air conditioner
CN103453650A (en) * 2012-05-28 2013-12-18 珠海格力电器股份有限公司 Fixing device and air conditioner with same

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102917837A (en) * 2010-06-03 2013-02-06 大金工业株式会社 Oil cooling device
CN103062836A (en) * 2011-10-20 2013-04-24 Lg电子株式会社 Indoor unit of air conditioner
CN103062836B (en) * 2011-10-20 2016-03-16 Lg电子株式会社 The indoor unit of air-conditioner
US9335060B2 (en) 2011-10-20 2016-05-10 Lg Electronics Inc. Indoor unit of air conditioner
EP2584274A3 (en) * 2011-10-20 2018-03-21 LG Electronics Inc. Indoor unit of air conditioner
CN103453650A (en) * 2012-05-28 2013-12-18 珠海格力电器股份有限公司 Fixing device and air conditioner with same
CN103453650B (en) * 2012-05-28 2015-08-26 珠海格力电器股份有限公司 Fixture and comprise the air-conditioner of this fixture

Also Published As

Publication number Publication date
ITTO20060243A1 (en) 2007-06-10
KR20070060876A (en) 2007-06-13

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication