KR960002603Y1 - Damper apparatus of ducts - Google Patents

Damper apparatus of ducts Download PDF

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Publication number
KR960002603Y1
KR960002603Y1 KR2019930001622U KR930001622U KR960002603Y1 KR 960002603 Y1 KR960002603 Y1 KR 960002603Y1 KR 2019930001622 U KR2019930001622 U KR 2019930001622U KR 930001622 U KR930001622 U KR 930001622U KR 960002603 Y1 KR960002603 Y1 KR 960002603Y1
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KR
South Korea
Prior art keywords
wing
damper device
state
blade
shaft
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KR2019930001622U
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Korean (ko)
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KR940021038U (en
Inventor
원희섭
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원희섭
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Priority to KR2019930001622U priority Critical patent/KR960002603Y1/en
Publication of KR940021038U publication Critical patent/KR940021038U/en
Application granted granted Critical
Publication of KR960002603Y1 publication Critical patent/KR960002603Y1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/02Ducting arrangements
    • F24F13/0236Ducting arrangements with ducts including air distributors, e.g. air collecting boxes with at least three openings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/14Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
    • F24F13/1486Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by bearings, pivots or hinges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24FAIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
    • F24F13/00Details common to, or for air-conditioning, air-humidification, ventilation or use of air currents for screening
    • F24F13/08Air-flow control members, e.g. louvres, grilles, flaps or guide plates
    • F24F13/10Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers
    • F24F13/14Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre
    • F24F13/1426Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by actuating means
    • F24F2013/1433Air-flow control members, e.g. louvres, grilles, flaps or guide plates movable, e.g. dampers built up of tilting members, e.g. louvre characterised by actuating means with electric motors

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air-Flow Control Members (AREA)

Abstract

내용 없음.No content.

Description

덕트의 댐퍼장치Duct damper

제1도는 종래의 댐퍼장치를 보인 개략도1 is a schematic view showing a conventional damper device

제2도는 종래의 또 다른 댐퍼장치를 보인 측단면도2 is a side cross-sectional view showing another conventional damper device

제3도는 본 고안에 따른 댐퍼장치의 구조를 보인 일부 단면 분해사시도Figure 3 is an exploded perspective view of a partial cross section showing the structure of the damper device according to the present invention

제4도는 본 고안에 따른 댐퍼장치의 작동관계를 보인 예시단면도로서4 is an exemplary cross-sectional view showing the operation of the damper device according to the present invention

(a)도는 개폐된 상태도이고,(a) is a state diagram opened and closed,

(b)도는 개방된 상태도이다,(b) is an open state diagram,

제5도는 본 고안에 따른 댐퍼장치의 요부를 발췌한 예시도5 is an exemplary view extracting the main portion of the damper device according to the present invention

* 도면의 주요부분에 대한 부호의 설명* Explanation of symbols for main parts of the drawings

1,10 : 댐퍼장치 2,14 : 날개1,10: damper device 2,14: wing

3 : 보조날개 4 : 모터3: auxiliary wing 4: motor

5 : 건물벽 6 : 덕트5: building wall 6: duct

13 : 축봉 15,16,17,18 : 만곡밀폐부13: shaft 15, 16, 17, 18: curved airtight

15-1,16-1,17-1,18-1 : 플랜지부 19 : 밀폐패킹축봉15-1,16-1,17-1,18-1: Flange 19: Sealed sealing shaft

30 : 댐퍼장치 30-1 : 장치틀30: damper device 30-1: device frame

30-2 : 공간부 31 : 상면판30-2: space part 31: top plate

32 : 하면판 33,34 : 스톱퍼32: bottom plate 33,34: stopper

35 : 측면판 36-2,37-2 : 수직밀착면35: side plate 36-2,37-2: vertical contact surface

37-3 : 안치홈 39 : 축베어링요입홈37-3: Settle groove 39: Shaft bearing insertion groove

40 : 축베어링 41 : 날개40: shaft bearing 41: wings

41-1 : 장측날개부 41-2 : 단측날개부41-1: Long side wing 41-2: Single side wing

42 : 축봉 43,44 : 연접부42: shaft 43,44: junction

본 고안은 건물의 환기실비에 설치되는 댐퍼장치에 관한 것으로서,The present invention relates to a damper device installed in the ventilation chamber ratio of a building,

특히 덕트의 적소에 설치되어 공기의 유통을 단속하고 공기의 유통을 차단했을때 완전한 밀폐상태가 유지되도록하되 그 구조가 복잡하지 않는 구조로 된 것이다.In particular, it is installed in the right place of the duct to control the air flow and block the air flow to maintain a completely closed state, but the structure is not complicated structure.

이를 좀더 구체적으로 설명하면,In more detail,

공기의 유통을 단속하는 날개가 장치들의 측면에 요설된 요입부내에서 작동되어지도록 하고 상호인접하는 날개는 그 양단들이 서로 중첩되어지도록 하여 밀폐효과를 향상시킬 수 있도록 하였으며, 날개의 축봉을 축착시킬때 베어링을 개입시켜 축착시킴으로써 보다 부드럽게 작동될 수 있도록 된 그러한 댐퍼장치를 제공코자한 것이다.Wings that control the flow of air are operated in the concave indents on the sides of the devices, and the mutually adjacent wings allow the two ends to overlap each other to improve the sealing effect. It is an object of the present invention to provide such a damper device that can be operated more smoothly by bearing through a bearing.

주지된 바와 같이 댐퍼장치는 일반적으로 평상시에는 건물의 실내에 신선한 공기를 공급할 때 주로 사용되고, 건물의 화재시에는 매연과 유독가스와 같은 연기를 외부로 배출시킬 수 있도록 하고 또 화염이 덕트를 따라 확산되어지는 것을 방지해 주는데 사용된다.As is well known, dampers are generally used to supply fresh air into a building's interiors in normal times, and in the event of a building's fire, it is possible to discharge smoke such as fumes and toxic gases to the outside, and flames spread along the duct. It is used to prevent it.

제1도는 종래의 댐퍼장치(1)룰 보인 일예시도이다.1 is an exemplary view showing a conventional damper apparatus 1.

덕트(6)를 개폐하는 날개(2)는 모터(4)에 의해 작동되고 외측편으로는 상기 날개(2)가 건물벽(8)의 외부로 누출되지 않도록하기 위하여 보조날개(3)가 별도로 설치되어 있다.The wing 2 for opening and closing the duct 6 is operated by the motor 4 and on the outside side the auxiliary wing 3 is separately provided so that the wing 2 does not leak out of the building wall 8. It is installed.

상기와 같은 상태에서 실내의 공기 예컨대 화재로 인한 매연이나 유독가스와 같은 연기를 배출시키고자 할때 모터(4)에 의해 날개(2)를 작동시켜서 덕트(6)의 통로를 개방시키게 되며, 구체적으로 도시되어 있지 않으나 송풍팬에 의해 연기를 흡입하여 배출시키게 되는 것이다.In such a state, when the air in the room, for example, smoke or toxic gas from the fire is to be discharged, the blades 2 are operated by the motor 4 to open the passage of the duct 6. Although not shown as is to suck the smoke by the blowing fan to be discharged.

그러나 상기 댐퍼장치(1)는 다음과 같은 문제들이 단점으로 지적된다.However, the damper device 1 is pointed out as the following problems.

평상시에 날개(2)들이 닫혀진 상태에서 외부의 공기(외기)가 보조날개(3)를 통하여 유입되어 날개(2)의 상하 및 측단과 댐퍼장치(1)의 장치를 사이의 틈 사이를 통하여 덕트(7)로 인입되어 실내에까지 역류유입되는 현상이 발생되는 문제가 있고,In the state in which the wings 2 are normally closed, outside air (outside air) flows in through the auxiliary blades 3, so that the upper and lower sides of the wings 2 and the device of the damper device 1 pass through the gap between the devices. There is a problem that a phenomenon that the flow back into the room (7) flows into the room occurs,

날개(2)와 장치를 사이로 외부에서 먼지나 이물질이 유입되어지고 유입된 먼지와 이물질들이 장기간의 비가동으로 인하여 누적되어서 고형화되는 현상도 초래되며, 이러한 상태에서 모터(4)를 작동시키더라도 고형화된 적층먼지에 의해 억류된 날개(2)가 원활하게 작동되지 못하는 현상까지 발생되는 문제도 있었으며,Dust or foreign matter is introduced from the outside between the wing 2 and the device, and the dust and foreign matters are accumulated and solidified due to prolonged inactivity. There was also a problem that occurred until the phenomenon that the wing (2) detained by the laminated dust is not operated smoothly,

특히, 모터(4)에 의해 작동되는 날개(2)를 건드리면 모터(5)에 무리가 가기 때문에 건물벽(5)의 외부에서 날개(2)를 건드리는 것을 방지하기 위하여 별도의 보조날개(3)를 설치해야 하는 번거로움이 있고 따라서 제작비가 증가되는 문제가 있었다.In particular, since touching the blade (2) actuated by the motor (4) is a burden on the motor (5) separate auxiliary wings (to prevent the touch of the blade (2) from the outside of the building wall (5) 3) there is a problem of having to install and thus the production cost increases.

또한 구체적으로 도시되어 있지 않으나 풍력에 의해 날개가 개발되어지도록 된 댐퍼장치는 송풍팬의 풍력이 너무 강한 경우에는 날개가 무리하게 개방되어져서 원상복귀가 되지 않는 등의 문제가 있었다.In addition, the damper device, which is not specifically shown to be developed by the wind power, there was a problem that the wing is unreasonably open when the wind power of the blowing fan is too strong, the wing is not open.

이러한 문제들을 해소할 수 있도록 하기 위한 것으로서 제2도에서 도시된 바와 같이 댐퍼장치(10)가 알려져있다.The damper device 10 is known as shown in FIG. 2 to solve these problems.

지지틀(11)의 내부 중앙에 날개(14)가 일체로 된 축봉(13)이 축착되고 상기 날개(14)의 양단에는 플렌지부(15-1)(16-1)(17-1)(18-1)가 구비된 만곡밀폐부(15)(16)(17)(18)를 형성하되 동일한 날개(14)의 양단에 형성되는 만곡밀폐부(15)(17)와 (16)(18)는 반대발향으로 형성되며, 서로 인접하는 날개(14)가 절첩될때 중첩되는 만곡밀폐부(16)와 (17)의 사이에는 밀폐 패킹축봉(19)이 축착되고 상면(11-1)과 바닥면(11-2)에는 스톱퍼(12)(12-1)를 구비하여 상하측에 위치하는 날개(14)의 플렌지부(15-1)와 (l8-1)가 당접되어지도록 되어었으며, 이들 날개(14)는 연결부재(21)이 개입되어 연결간(22)으로 연결되어 있다.In the center of the support frame 11, the shaft rod 13 in which the blade 14 is integrated is compressed, and flanges 15-1, 16-1, 17-1 ( Curved sealed portions 15, 16, 17 and 18 having 18-1 are provided, but curved sealed portions 15, 17 and 16 are formed on both ends of the same wing 14, respectively. ) Is formed in the opposite direction, and the sealing packing shaft rod 19 is condensed between the curved sealing portions 16 and 17 overlapping when the wings 14 adjacent to each other are folded, and the upper surface 11-1 and the bottom are condensed. On the surface 11-2, stoppers 12 and 12-1 are provided so that the flange portions 15-1 and l8-1 of the wings 14 positioned on the upper and lower sides are brought into contact with each other. The wing 14 is connected to the connecting rod 22 through the connecting member 21.

이와 같이 된 종래의 댐퍼장치(10)는 임의 수단에 의해 연결간(22)이 상하작동되면 날개(14)가 축봉(13)을 중심으로 하여 90°각도씩 정역회전되면서 개폐되어지는데 개방시에는 각 날개(14)가 수평상태(실선으로 도시됨)로 되고 폐쇄시에는 각 날개(14)가 수직상태(가상선으로 도시됨)로 된다.In the conventional damper device 10 as described above, when the connecting rod 22 is operated up and down by any means, the blade 14 is opened and closed while being rotated forward and backward by 90 ° with respect to the shaft 13. Each wing 14 is in a horizontal state (shown in solid line) and when closed, each wing 14 is in a vertical state (shown in phantom line).

특히, 폐쇄시에는 상측에 위치하는 날개(14)는 만곡밀폐부(15)의 플랜지부(15-1)가 상면(11-1)의 스톱퍼(12)에 연접되어 정지되고 하측에 위치하는 날개(14)는 만곡밀폐부(18)의 플렌지부(18-1)가 바닥면(11-2)의 스톱퍼(12-1)에 연접되어 정지되며, 인접하는 날개(14)의 만곡밀폐부(16)와 (17)은 밀폐패킹축봉(19)을 감싸듯 연점되어져서 서로간에 마주보고 중첩되어 진다.Particularly, in the closing, the wing 14 positioned on the upper side is the wing 15 positioned on the lower side after the flange portion 15-1 of the curved airtight portion 15 is connected to the stopper 12 on the upper surface 11-1. 14, the flange portion 18-1 of the curved sealing portion 18 is connected to the stopper 12-1 of the bottom surface 11-2 and stopped, and the curved sealing portion of the adjacent blade 14 ( 16) and (17) are softened as if enveloping the sealed packing shaft bar (19) and overlap each other facing each other.

이와 같이 작동되는 종래의 댐퍼장치(l0)는 다음과 같이 문제가 단점으로 지적된다.The conventional damper device 100 operated in this way is pointed out as a disadvantage as follows.

상기 댐퍼장치(10)가 폐쇄상태로 되어 있을때 날개(14)의 만곡밀폐부(16)(17)가 밀폐패킹축봉(19)에 중첩되듯이 당접되어지므로 공기의 유통이 다소 차단되지만, 날개(14)의 양측단과 지지틀(11)이 측면과의 사이가 이격되어 있으므로 이들 틈사이로 외기(외풍)가 유입되어 실내로까지 역류되는 문제가 있었고,When the damper device 10 is in a closed state, the curved sealing portions 16 and 17 of the wings 14 are abutted as overlapping the sealed packing shaft rod 19, so that air flow is somewhat blocked, but the wings ( 14) because both sides of the support frame 11 and the side is spaced apart from the outside air (outdraft) is introduced between these gaps there was a problem that backflow into the room,

날개(14)의 중첩되어지는 만곡밀폐부(16)와 (17)이 설로 대향되듯이 외측으로 만곡되어 있기 때문에 중첩되는 만곡밀폐부(16)(17)가 밀폐패킹축봉(19)에 연접되어지도록 하기 위하여 상기 밀폐 패킹축봉(19)을 횡착시켜야 하는 제작상의 번거로움으로 인하여 제작시간과 비용이 많이 소요되는 문제도 있었으며,Since the overlapping curved sealing portions 16 and 17 of the wings 14 are curved outwardly as opposed to the tongue, the overlapping curved sealing portions 16 and 17 are connected to the sealed packing shaft rod 19. There was also a problem that the production time and costs are high due to the manufacturing hassle to transverse the sealed packing shaft rod 19 in order to lose,

날개(14)의 축봉(13)이 단순히 지지틀(11)의 측면에 단순히 삽입되는 것에 축설되어 있으므로 각 축봉(13)간에 좌우요동이 발생되고 따라서 부드럽게 작동되지 못하는 문제가 있었다.Since the shaft bar 13 of the wing 14 is simply installed in the side of the support frame 11 is simply inserted, there is a problem that the left and right fluctuations occur between the shaft bar 13 and thus cannot operate smoothly.

또한 날개(14)의 양단에 형성되는 만곡밀폐부(15)(17)와 (16)(18)이 서로 반대방향으로 만곡되어 있으므로 날개(14)를 성형하기 위한 프레스성형틀을 성형하기가 용이치 못하다는 것이다.In addition, since the curved sealing portions 15, 17 and 16, 18 formed at both ends of the wing 14 are curved in opposite directions, it is easy to form a press mold for forming the wing 14. That's not good.

본 고안은 상기와 같은 문제를 해소할 수 있도록 된 댐퍼장치를 제공하는데 있다.The present invention is to provide a damper device that can solve the above problems.

본 고안은 밀폐효과가 더욱 향상되어 외기가 역류유입되는 것은 방지할 수 있도록 된 댐퍼장치를 제공하는데 그 목적이 있다.The object of the present invention is to provide a damper device to further improve the sealing effect to prevent the inflow of outside air backflow.

본 고안은 다른 목적은 장치틀을 성형함에 있어서 측면판의 내측에 날개를 가이드하고 지지하는 요입부를 형성하여 줌으로써 날개가 요동없이 원활하게 작동되고 따라서 폐쇄상태에서도 원활하제 작동될 수 있도록 된 댐퍼장치를 제공하는데 있다.Another object of the present invention is to provide a damper device for forming a frame to form a concave portion for guiding and supporting the wing on the inner side of the side plate so that the wing can operate smoothly without fluctuation, and thus can be operated smoothly even in a closed state. To provide.

본 고안은 또 다른 목적은 별도의 패킹축봉을 축설시키지 않고도 밀폐효과를 얻을 수 있도록하고, 용이하제 제작할 수 있도록 된 댐퍼장치를 제공하는데 있으며,Another object of the present invention is to provide a damper device that enables to achieve a sealing effect without easily laying a separate packing shaft rod, and to be easily manufactured.

본 고안의 또 다른 목적은 날개(41)에 고정되는 축봉(42)을 편향되게 축착시켜 줌으로써 장측날개부의 자중에 의해 닫혀진(폐쇄) 상태가 유지되어지도록 된 댐퍼장치를 제공하는데 있으며, 본 고안의 또 다른 목적은 날개의 축봉을 측면판에 축설시킬때 베어링을 개입시켜 축설시켜 줌으로써 보다 원활하게 작동될 수 있도록 된 댐퍼장치를 제공하는데 있다.Still another object of the present invention is to provide a damper device that is maintained in a closed state (closed) by the self-weight of the long side wings by biasing the shaft rod 42 fixed to the wing 41, the present invention Still another object is to provide a damper device that can be operated more smoothly by placing the shaft of the wing on the side plate through the bearing through the bearing.

본 고안의 상기 및 기타 목적은,The above and other objects of the present invention,

장치틀(30-1)의 상면판(31)과 하면판(32)의 내측면에 스톱퍼(33)(34)가 대향되게 고정되고 대향되는 측면판(36)에 날개(41)가 고정된 축봉(42)을 다단으로 축설시키되 인접하는 날개(41) 끼리는 각 양단에 반대방향으로 형성된 만곡밀폐부가 대향되게 중첩되어지도록 된 것에 있어서,The stoppers 33 and 34 are fixed to the inner side surfaces of the upper plate 31 and the lower plate 32 of the apparatus frame 30-1 so that the wings 41 are fixed to the opposite side plates 36. In the shaft bar 42 is laid in multiple stages, but adjacent wings 41 are arranged so that the curved airtight portions formed in opposite directions on both ends thereof overlap each other,

상기 측면판(36)에 축베어링요입홈부(39)를 중심으로 상하측 반대방향에 날개요입부(37)(36)를 반복적으로 연하여 요실하되 인접하는 날개요입부(37)(36)는 수직밀착면(37-2)(36-2)이 중첩되어 연통부(38)에서 연통되어지도록 된 것과,The wing plate 37 and 36 are repeatedly connected to the side plate 36 in the up and down direction of the shaft bearing hole groove 39, and the wing blades 37 and 36 are adjacent to each other. The vertical contact surfaces 37-2 and 36-2 overlap and communicate with each other in the communication section 38,

날개(41)의 양단에 형성되는 연접부(43)(44)를 동일 방향으로 형성하여서 된 것을 특징으로 하는 댑퍼장처(30)에 의해 달성된다.It is achieved by the adapter 30, which is formed by forming the connecting portions 43 and 44 formed at both ends of the blade 41 in the same direction.

본 고안은 상기와 같이 구성되어 있으므로 축베어링요입홈(39)에 축베어링(40)을 개입시켜 축설되는 날개(41)는 날개요입부(36)(37)내에서만 제한적으로 개방되어지게 되고, 수평으로 회전되어 개방된 상태에서 지지력이 제거되면 편향되어지게 되고, 수평으로 회전되어 개방된 상태에서 지지력이 제거되면 편향되게 고정된 축봉(42)에 의해 상기 날개(41)중에서 장측날개부(41-1)의 자중에 의해 직립상태로 회전되면서 인접하는 날개(41) 끼리의 연접부(43)(44)들이 연통부(38) 선상에서 연접되어 중첩되면서 밀폐되어지며, 특히 날개(41)의 양측단의 전후면이 수직밀착면(36-2)(37-2)에 밀착되면서 외측으로 유입되어지는 외기까지 차단하게 된다.Since the present invention is constructed as described above, the wings 41 which are constructed by interposing the shaft bearings 40 in the shaft bearing insertion grooves 39 are limited to be opened only in the blade insertion portions 36 and 37, When the bearing force is removed in the horizontally rotated open state, the deflection is deflected, and when the bearing force is removed in the horizontally rotated open state, the long side wing part 41 is formed in the blade 41 by the shaft rod 42 fixedly deflected. -1) while being rotated in an upright state by the weight of self, the connecting portions 43 and 44 of the adjacent blades 41 are connected to each other on the line of the communicating portion 38 and overlapped, and are sealed. The front and rear surfaces of both side ends are in close contact with the vertical contact surfaces 36-2 and 37-2 to block the outside air introduced to the outside.

이하 본 고안의 상기 및 기타목적과 특징 및 효과는 첨부도면에 의거한 다음의 상세한 설명에 의해 더욱 명확하게 이해할 수 있을 것이다.Hereinafter, the above and other objects, features, and effects of the present invention will be more clearly understood by the following detailed description based on the accompanying drawings.

제3도 내지 제5도는 본 고안에 따른 구체적인 구현에 즉, 댐퍼장치(30)의 예시도이다.3 to 5 are exemplary views of the damper device 30 in a specific embodiment according to the present invention.

내부가 공간부(30-2)로 되고 개방된 직육면체형의 장치틀(30-1)을 형성하였다. 상기 장치틀(30-1)은 상면판(31)과 하면판(32) 및 측면판(35)을 일체형으로 한 것으로서 각기 별도로 제작하여 용접과 같은 방법에 의해 일체화시킬 수 있으며, 특히 측면판(35)의 내측면에 형성되는 요칠부는 철판을 프레싱하거나 금형틀에 성형할 수 있다.The inside was made into the space part 30-2 and the open rectangular parallelepiped apparatus frame 30-1 was formed. The apparatus frame 30-1 is made of the upper plate 31, the lower plate 32 and the side plate 35 as an integral type, and can be separately manufactured to be integrated by a method such as welding. The recessed portion formed on the inner side of 35 may press the steel sheet or mold the mold.

장치틀(30-1)에서 상면판(31)과 하면판(32)의 내면에 스톱퍼(33)(34)를 길이 방향으로 고정시키되 차후에 구체적으로 설명되는 측면판(36)이 축베어링요입홈(39)과 동일선상에서 전후로 약간의 편차를 유지시켜 고정시킨 것으로서, 제5도에 구체적으로 도시된 바와 같이 상면판(31)의 고정된 스톱퍼(33)는 좌측으로 약간 편차되게 고정하고 하면판(32)에 고정된 스톱퍼(33)는 우측으로 약간 편차되게 고정하였다.In the frame 30-1, the stoppers 33 and 34 are fixed to the inner surfaces of the upper plate 31 and the lower plate 32 in the longitudinal direction, but the side plate 36, which will be described in detail later, has a shaft bearing recess groove. As fixed to maintain a slight deviation back and forth on the same line as (39), as shown in Fig. 5 specifically, the fixed stopper 33 of the upper plate 31 is fixed slightly to the left side and the lower plate ( The stopper 33 fixed to 32 is fixed slightly to the right side.

특히 상면판(31)에 스톱퍼(33)는 차후에 구체적으로 설명되는 날개(41)의 양단에 형성된 연접부(43)를 감안하여 상기 연접부(43)와 동일한 형상으로 요칠형성하되 스톱퍼(33)에 형성된 요철부를 날개(41)의 연접부(43)가 외측으로 감싸지면서 서로 연접되어지도록 하였다.In particular, the stopper 33 on the top plate 31 is formed in the same shape as the connection portion 43 in consideration of the connection portion 43 formed on both ends of the wing 41 which will be described later in detail, but the stopper 33 Concave-convex portions formed in the connecting portion 43 of the wing 41 is to be connected to each other while wrapped outside.

상기 상ㆍ하면판(31)(32)의 스톱퍼(33)(34)는 측면판(35)에 축착되는 날개(41)가 닫혀진 상태 즉 공간부(30-2)를 폐쇄시키도록 직립상태로 되어 있을때 최상측에 축착되는 날개(41)의 연접부(43)와 최하측에 축착되는 날개(41)의 연접부(44)가 각각 연접되어서 공간부(30-2)이 상ㆍ하측에 역유입되려는 외기를 차단시키게 된다.The stoppers 33 and 34 of the upper and lower plates 31 and 32 are in an upright state so as to close the space part 30-2, that is, the wing 41 which is fixed to the side plate 35 is closed. When the connection part 43 of the blade 41 which is affixed to the uppermost side and the connection part 44 of the blade 41 which is affixed to the lowermost side are respectively connected, the space part 30-2 is reversed up and down. It blocks the outside air to be introduced.

측면판(35)에는 제3도 및 제5도에 도시된 바와 같이 날개(41)의 축봉(42)을 용이하게 축착시킬 수 있도록 하기 위하여 축베어링요입홈(39)이 등간격으로 요설하고 상기 축베어링요입부(39)를 축베어링요입홈(39)에서 연통되어지도록 요설형성하되, 날개요입부(37)는 상부우측에 형성하고 날개요입부(36)는 하부좌측에 형성하였으며, 날개(41)가 회전되는 것을 감안하여 4등분된 원형으로 형성하였다.As shown in FIGS. 3 and 5, the side plate 35 is provided with a shaft bearing indentation groove 39 at equal intervals so that the shaft rod 42 of the wing 41 can be easily compressed. The shaft bearing indentation part 39 is formed in the main body so as to be in communication with the shaft bearing inlet groove 39, but the wing indentation part 37 is formed on the upper right side, and the wing indentation part 36 is formed on the lower left side. Considering the rotation of 41), it was formed into quadrant circles.

특히, 최상단의 날개요입부(37)와 최하단의 날개요입부(16)를 제외한 인접하는 날개요입부(36)(37) 끼리는 서로 중첩되어지도록 형성하되, 그 중첩부를 연통부(38)로 연통시켜주어서 날개(41)가 닫혀진 직립상태로 될때 상하측에 위치하는 날개(41)의 연접부(44)와 연접부(43)가 용이하제 서로 연접될 수 있도록 하였으며, 또한 각 날개요입부(37)에서 수평밀착면(37-1)의 외측에 안치홈(37-3)을 형성하여 날개(41)가 수평상태로 되었을때 돌출된 연접부(43)를 수용할 수 있도록 하였고,In particular, adjacent wing recesses 36 and 37 are formed so as to overlap each other, except for the wing recess 37 at the uppermost stage and the wing recess 16 at the lowermost stage, and the overlapping portion communicates with the communication section 38. When the wing 41 is in a closed upright state, the connecting portion 44 and the connecting portion 43 of the upper and lower sides of the wing 41 can be easily connected to each other, and each wing recess 37 Settle groove 37-3 on the outer side of the horizontal contact surface (37-1) in the) to accommodate the protruding connecting portion 43 when the wing 41 is in a horizontal state,

최하측의 날개요입부(36)에서 수직밀착면(36-2)의 하측에 안치홈(36-3)을 형성하여 날개(41)가 수직상태로 되었을때 돌출된 연접부(44)를 수용할 수 있도록 하였다.In the lower wing indentation portion 36, a lower recess 36-3 is formed at the lower side of the vertical contact surface 36-2 to accommodate the connecting portion 44 protruding when the wing 41 is in a vertical state. I could do it.

이와 같이 형성된 측면판(35)의 축베어링요입홈(39)는 축베어링(40)을 삽입하여 날개(41)의 축봉(42)을 축실하게 되며, 축봉(42)이 축베어링(40)내에서 회전되어지도록 함으로써 부드럽게 작동(회전)되어지도록 하고 또 좌우요동을 최소화시킬 수 있도록 하였으며, 특히 날개(41)의 양측단은 날개요입부(36)(37)에 수용되어진 상태에서 축설되어진다.The shaft bearing insertion groove 39 of the side plate 35 formed as described above is inserted into the shaft bearing 40 so as to lose the shaft 42 of the wing 41, and the shaft 42 is in the shaft bearing 40. In order to be rotated in a smooth operation (rotation) and to minimize the left and right fluctuations, in particular, both ends of the wing 41 is built in the state accommodated in the wing indentation (36, 37).

상기 날개(41)는 전후측단에 연접부(43)(44)를 요철형으로 형성하였는데 날개요입부(36)(37)에서서 서로 연접되어지는 것을 감안하여 동일방향으로 형성하였으며, 축봉(42)을 날개요입부(36)(37)와 일치하도록 일측으로 편향되게 고정하여 수평상태에서 힘이 제거되면 장측날개부(41-1)의 자중에 의해 스스로 하향회전되어져서 장치틀(30-1)의 공간부(30-2)를 폐쇄시킬 수 있도록 하였다.The wing 41 is formed in the same direction in consideration of being connected to each other in the wings recessed portion 36, 37 formed in the concave-convex portion 43, 44 at the front and rear side ends, shaft rod 42 ) To be deflected to one side to coincide with the wing indenters 36 and 37 so that when the force is removed in the horizontal state, the frame itself is rotated downward by the weight of the long wing 41-1. The space part 30-2 of) was made to be closed.

이하 작용효과를 설명한다.The effect will be described below.

본 고안에 따른 댐퍼장치(30)는 제4도의 (a)(b)도에 도시된 바와 같이 개폐작동된다.The damper device 30 according to the present invention is opened and closed as shown in (a) and (b) of FIG. 4.

(a)도에 도시된 상태는 장치틀(30-1)의 공간부(30-2)가 폐쇄된 상태를 보인 예시도로서 평상시의 상태를 보인 것이다.The state shown in (a) is an exemplary view showing a state in which the space part 30-2 of the apparatus frame 30-1 is closed, and shows a normal state.

축설되어 있는 날개(41)는 장측날개부(41-1)가 하향되고 단축날개부(41-2)가 상향된 상태로서 장측날개부(4l-1)의 자중에 의해 직립상태로 유지되어지는 것이다.The wing 41 which has been built up is kept in an upright state by its own weight of the long side wing portion 4l-1 with the long side wing portion 41-1 downward and the short side wing portion 41-2 upward. will be.

날개(41)가 직립상태를 유지하게 되면 최상단에 축설된 날개(41)의 연접부(43)가 상면판(31)의 스톱퍼(33)에 연접되어 상단으로 유입될려는 외기를 차단하게 되고, 최하단에 축설된 날개(41)의 연접부(44)가 수직밀착면(36-2)의 안치홈(36-3)에 안치된 상태에서 하면판(32)의 스톱퍼(34)에 연접되어지므로 하단으로 유입될려는 외기를 차단하게 된다.When the wing 41 maintains the upright state, the connecting portion 43 of the wing 41 which is arranged at the top end is connected to the stopper 33 of the upper surface plate 31 to block external air from entering the upper end, Since the connecting portion 44 of the blade 41 arranged at the lower end is connected to the stopper 34 of the lower plate 32 in a state where it is placed in the settling groove 36-3 of the vertical contact surface 36-2. It will block the outside air that wants to flow to the bottom.

특히, 날개(41)가 직립상태에 있을때 단축날개부(4l-2)는 좌우양측면이 날개요입부(37)의 수직밀착면(37-2)애 연점되어진 상태이고 장축날개부(41-1)는 좌우양측면이 날개요입부(36)의 수직밀착면(36-2)에 연접되어진 상태로 유지되므로 공간부(30-2)의 양측편으로 유입될려는 외기가 차단되어진다.In particular, when the blade 41 is in an upright position, the short-wing blade portion 4l-2 is in a state where the left and right sides thereof are connected to the vertical contact surface 37-2 of the blade recess portion 37, and the long-axis blade portion 41-1 is provided. The left and right sides are kept in contact with the vertical contact surface 36-2 of the wing indentation 36, so that the outside air to be introduced to both sides of the space portion 30-2 is blocked.

또한 날개(41)가 직립상태에 있을때 상하인접하는 날개(41)는 연통부(38) 선상에서 연접부(44)와 (43)이설로 연접되어진 상태로 유지되므로 공간부(30-2)에서 유입될려는 외기는 차단되어지는 것이다.In addition, when the wing 41 is in an upright state, the wing 41 adjacent to the upper and lower sides is maintained in the state in which the connecting part 44 and 43 are connected by repositioning on the line of the communicating part 38, The outside air to be introduced is blocked.

제4도의 (b)도는 댐퍼장치(30)를 작동시킨 상태를 보인 예시도이다.(B) of FIG. 4 is an exemplary view showing a state in which the damper device 30 is operated.

각 날개(41)는 구체적으로 도시되어 있지않으나 통상의 연결부재와 연결간 그리고 모터와 같은 동력수단에 의해 작동되거나 도시되어 있지 않은 팬의 강풍의 압력에 의해 개방된다.Each wing 41 is not shown in detail but is opened by the pressure of the strong wind of the fan, which is not shown or operated by a power connection such as a motor and a conventional connecting member.

동력수단 또는 동력에 의해 날개(41)가 회전될때 축봉(42)이 축베어링(40)에서 회전되므로 매우 부드럽게 회전 되어지고, 상기 축베어링(40)에 의해 좌우요동이 극히 제한적인 상태에서 작동(회전)된다.When the blade 41 is rotated by the power means or power, the shaft 42 is rotated in the shaft bearing 40 so that it is rotated very smoothly, the shaft bearing 40 is operated in a state in which the left and right swing is extremely limited ( Rotation).

(b)도에 도시된 바와 같이 수평상태로 회전되었을때 각 날개(41)의 장측날개부(41-1)와측날개부(41-2)가 날개요입부(36)(37)의 수평밀착면(36-1)(37-1)에 각각 연접되어지고 특히 연접부(43)가 수평밀착면(37-1)의 안차홈(37-3)에 안치되어지므로 날개(41)가 너무 회전되어 개방되는 것이 제한되므로 동력수단의 힘이 제거되었을때 용이하게 회전되어지는 것이다.As shown in (b), the long side blade portion 41-1 of each blade 41 when rotated in a horizontal state and The side wing portions 41-2 are respectively connected to the horizontal tight surfaces 36-1 and 37-1 of the wing recesses 36 and 37, and the joint 43 is a horizontal tight surface 37-. Since the wing 41 is placed in the car recess 37-3 of 1), the blade 41 is too rotated to be opened and thus is easily rotated when the power of the power means is removed.

특히 날개(41)가 측면판(35) 사이에서 회전될때 그 양측단이 날개요입부(36)(37)에 수용되고 축봉(42)이 축베어링(40)에 축성되어 있으므로 날개(41)의 좌우요동은 최대한 억제되어지며, 동력 또는 풍력이 제거되면 장측날개부(41-1)의 자중에 의해 각 날개(41)는 하향회전되어서 제4도의 (a)도에 도시된 바와 같이 공간부(30-2)를 폐쇄시키게 되는 것이다.Particularly, when the blade 41 is rotated between the side plates 35, both ends thereof are accommodated in the blade recesses 36 and 37 and the shaft 42 is built up in the shaft bearing 40. Left and right fluctuations are suppressed as much as possible, and when the power or wind power is removed, each wing 41 is rotated downward by the weight of the long side wing portion 41-1, as shown in (a) of FIG. 30-2) will be closed.

이상에서와 같이 본 고안에 따르면 날개(41)가 수직상태에 있을때 각 날개(41)이 연접부(43)(44)가 서로중첩되어 연접되고 양측편이 수직밀착면(36-2)(37-2)에 연접되어지며, 상하측단은 스톱퍼(33)(34)와 연접부(43)(44)가 밀착되어지므로 밀폐력이 크게 향상되어지고, 축봉(42)이 축베어링(40)에 축설되고 날개(41)의 양측단이 날개요입부(36)(37)에 수용된 상태에서 작동되므로 날개(41)의 요동이 억제되면서 매우 부드럽게 작동되어지며, 날개(41)가 수평상태로 되었을때 수평밀착면(36-1)(37-1)에 의해 회전되는 각도가 억제되므로 압력이 제거되었을때 자중에 의해 곧바로 회전되면서 공간부(30-2)를 폐쇄시키게 되는 것인바, 평상시에는 외기의 유입이 완전히 차단되어지고 비상시에는 즉시 개방되어지므로 실비의 효율성을 극대화시킬 수 있을 뿐만 아니라 중첩되는 날개에 의해 외부와 차단되므로 보호용 별도의 보조날개를 구비하지 않아도 되므로 제작비도 절감할 수 있게 된다는 것이다.As described above, according to the present invention, when the wings 41 are in a vertical state, each of the wings 41 is connected to each other by connecting the joints 43 and 44 with each other, and both sides are vertically contact surfaces 36-2 and 37-. 2), the upper and lower ends of the stopper 33, 34 and the connecting portion 43, 44 is in close contact with the sealing force is greatly improved, the shaft 42 is built in the shaft bearing (40) Since both ends of the wing 41 are operated in the state of being accommodated in the wing indents 36 and 37, the fluctuation of the wing 41 is suppressed and is operated very smoothly. When the wing 41 is in a horizontal state, the horizontal contact Since the angle rotated by the planes 36-1 and 37-1 is suppressed, when the pressure is removed, the space 30-2 is closed by being directly rotated by its own weight. They are completely shut off and open immediately in an emergency to maximize the efficiency of the actual cost as well as overlapping blades. Since it is cut off from the outside by a dog, it is possible to reduce the manufacturing cost because it does not have to have a separate auxiliary wing for protection.

Claims (1)

(정정) 장치틀(30-1)의 상면판(31)과 하면판(32)의 내측면에 스톱퍼(33)(34)가 대향되게 고정되고 대향되는 측면판(36)에 날개(41)가 고정된 축봉(42)을 다단으로 축설시키되 인접하는 날개(41)끼리는 각 양단에 반대방향으로 형성된 만곡밀폐부가 대향되게 중첩되어지도록 된 것에 있어서,(Correction) Wings 41 on the side plates 36 which are fixedly opposed to the stoppers 33 and 34 on the inner surface of the upper plate 31 and the lower plate 32 of the apparatus frame 30-1. In that the shafts 42 are fixed in multiple stages, but adjacent blades 41 are arranged so that the curved airtight portions are formed opposite to each other at opposite ends to overlap each other. 상기 측면판(36)에 축베어링요홈부(39)룰 중심으로 상하측 반대방향에 날개요입부(37)(36)를 반복적으로 연하여 요설하되 인접하는 날개요입부(37)(36)는 수직밀착면(37-2)(36-2)이 중첩되어 연통부(38)에서 연통되어지도록 된 것과,Repeatedly extends the wing recesses 37 and 36 in the up and down opposite directions with respect to the axial bearing recess 39 in the side plate 36, but adjacent wing recesses 37 and 36 are The vertical contact surfaces 37-2 and 36-2 overlap and communicate with each other in the communication section 38, 날개(41)의 양단에 형성되는 연접부(43)(44)를 동일 방향으로 형성하여서 된 것을 특징으로 하는 덕트의 댐퍼장치.The damper device of the duct, characterized in that the connecting portion (43) 44 formed on both ends of the blade (41) formed in the same direction.
KR2019930001622U 1993-02-08 1993-02-08 Damper apparatus of ducts KR960002603Y1 (en)

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KR2019930001622U KR960002603Y1 (en) 1993-02-08 1993-02-08 Damper apparatus of ducts

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KR940021038U KR940021038U (en) 1994-09-24
KR960002603Y1 true KR960002603Y1 (en) 1996-03-27

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