KR840001836Y1 - Burner of the using powden fuel - Google Patents

Burner of the using powden fuel Download PDF

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Publication number
KR840001836Y1
KR840001836Y1 KR2019820008418U KR820008418U KR840001836Y1 KR 840001836 Y1 KR840001836 Y1 KR 840001836Y1 KR 2019820008418 U KR2019820008418 U KR 2019820008418U KR 820008418 U KR820008418 U KR 820008418U KR 840001836 Y1 KR840001836 Y1 KR 840001836Y1
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KR
South Korea
Prior art keywords
fuel
burner
cylinder
rotating cylinder
outlet
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Application number
KR2019820008418U
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Korean (ko)
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KR840002336U (en
Inventor
강영부
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강영부
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Priority to KR2019820008418U priority Critical patent/KR840001836Y1/en
Publication of KR840002336U publication Critical patent/KR840002336U/en
Application granted granted Critical
Publication of KR840001836Y1 publication Critical patent/KR840001836Y1/en

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D1/00—Burners for combustion of pulverulent fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2201/00—Burners adapted for particulate solid or pulverulent fuels
    • F23D2201/10—Nozzle tips
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2201/00—Burners adapted for particulate solid or pulverulent fuels
    • F23D2201/20—Fuel flow guiding devices

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)

Abstract

내용 없음.No content.

Description

분말연료를 사용하는 버너Burner using powdered fuel

제1도는 본 고안의 전체사시도.1 is a perspective view of the present invention.

제2도는 본 고안의 요부분리 사시도.2 is a partial perspective view of the present invention.

제3도는 본 고안의 전체단면도이다.3 is an overall cross-sectional view of the present invention.

* 도면의 부호에 대한 간단한 설명* Brief description of the symbols in the drawing

1 : 상부동체 2 : 하부동체1: upper fuselage 2: lower fuselage

3 : 모우터 4 : 감속기3: motor 4: reducer

5체인 6 : 회전원통5 chain 6: rotating cylinder

7 : 연료안내부 8 : 연료통7: fuel guide 8: fuel container

9 : 공기통로 10 : 송풍기9: air passage 10: blower

11 : 공기유출구 12 : 연료유출구11 air outlet 12 fuel outlet

13 : 홴 14 : 철편13: 홴 14: iron piece

본 고안은 분말연료을 사용하도록 된 버너에 관한 것이다.The present invention relates to a burner adapted to use powdered fuel.

종래의 버너는 주로 석유류를 연료로 사용토록 되어있기 때문에 구조가 액체분 사식으로 되어있음은 물론 연료가 오일류에 국한되는 폐단이 있기 때문에 고가의 석유류를 사용해야만 하는 결점이 있었다.The conventional burner has a drawback of having to use expensive petroleum because the structure is liquid injection type as well as a closed end where the fuel is limited to oil because the petroleum is mainly used as fuel.

본 고안은 종래의 상기와 같은 제 결점을 시정하기 위하여 분말형태의 연료를 서서히 공급하되 분말연료의 배출구의 중앙에서, 공기가 분출되도록 하므로서, 일체의 석유류의 낭비를 없애고 연소가 용이하도록 된 분말을 버너를 제공함에 목적이 있다.The present invention is to gradually supply the fuel in the form of powder in order to correct the above drawbacks of the prior art, so that the air is ejected from the center of the outlet of the powder fuel, eliminating the waste of any petroleum and the powder to facilitate combustion The purpose is to provide a burner.

본 고안은 첨부된 예시도면과 함께 상세히 설명하면 다음과 같다.The present invention is described in detail with the accompanying exemplary drawings as follows.

본 고안은 전체를 상부동체(1)와 하부동체(2)로 형성하되 하부동체(2) 내에는 모우터(3)와 감속기(4)를 설치하여 체인(5)에 의해 상부동체(1)의 회전원통(6)을 회전시키도록 하고 회전원통(6)의 전방외주에 회전원통(6)과 일체로 회전되는 나선형 연료안내부(7)가 연료통(8)의 하단에 밀접되도록 하며, 회전원통(6)의 후방에는 외부로부터 회전원통(6)의 내측공기통로(9)로 공기를 유입하는 송풍기(10)를 설치하며, 공기유출구 (11)와 연료유출구(12)에는 각각 확산용 홴(13)과 불완전연소물 제거용철편 (14)을 결합한 구조로 되어있다.The present invention forms the whole of the upper body (1) and the lower body (2) but in the lower body (2) by installing a motor (3) and a reducer (4) by the upper body (1) by the chain (5) To rotate the rotating cylinder (6) of the helical fuel guide (7) which is integrally rotated with the rotating cylinder (6) on the front outer periphery of the rotating cylinder (6) close to the lower end of the fuel cylinder (8), and rotates At the rear of the cylinder 6, a blower 10 for introducing air from the outside into the inner air passage 9 of the rotating cylinder 6 is provided, and the air outlet 11 and the fuel outlet 12 are respectively provided with diffusion fans. (13) and the incomplete combustion material removal iron piece (14) combined.

미설명부호 15는 베어링, 16은 가이드, 17은 벨트이다.Reference numeral 15 is a bearing, 16 is a guide, 17 is a belt.

본 고안은 모우터(3)의 회전력이 벨트(17)를 통하여 감속기(4)에 전달되고 다시 감속기(4)에서 감속된 회전력은 체인(5)을 통하여 상부동체(1)의 전단 즉, 회전원통(6)에 전달되어 회전원통(6) 및 이와 일체로 형성된 나선형 연로안내부(7)가 서서히 회전되는 것이다.According to the present invention, the rotational force of the motor 3 is transmitted to the speed reducer 4 through the belt 17, and the rotational force reduced in the speed reducer 4 is the front end of the upper body 1, that is, the rotation, through the chain 5. It is transmitted to the cylinder (6) is a rotary cylinder (6) and the spiral flue guide portion 7 formed integrally therewith is to rotate slowly.

이와같이 나선형연료 안내부(7)가 회전됨에 따라서 연료용(8) 내의 분말연료는 나선형열료 안내부(7)에 의해서 연료유출구(12) 즉, 가이드(16)내로 이송되고 동시에 상부동체(1)의 후단부에서는 별도의 모우터(도시되지 않음)에 의해 회전되는 송풍기 (10)에 의해 외부공기가 상부동체(1) 내의 공기통로(9)로 유입되어 공기유출구(11)로 유출되는데 이들은 모두 동시에 이루어지고 또한 가이드(16)내에서 이루어진다.As the helical fuel guide 7 is rotated in this way, the powdered fuel in the fuel 8 is transported into the fuel outlet 12, ie, the guide 16 by the helical fuel guide 7, and at the same time the upper body 1 At the rear end of the external air flows into the air passage (9) in the upper body (1) by a blower (10) rotated by a separate motor (not shown), these all flow out to the air outlet (11) It is done simultaneously and in the guide 16.

공기우출구(11)에 설치된 홴(13)은 각각의 날개가 일정방향으로 약간 뒤틀린 상태로서 공기유출구(11)에서 유출되는 공기를 확산시키는 역할을 하며 회전원통(6)과 일체로 되어 동일한 속도로 회전한다.13 13 installed at the air outlet 11 serves to diffuse the air flowing out of the air outlet 11 with each wing slightly twisted in a predetermined direction, and is integrated with the rotary cylinder 6 to have the same speed. Rotate to

연료유출구(12)의 철편(14)은 가이드(16) 내측에 불완전 연소된 물질이 붙어있을때 이를 제거하는 역할을 하며 베어링(15)은 회전원통(6)의 회전을 원활히 하도록 된 것이다.The iron piece 14 of the fuel outlet 12 serves to remove the incompletely burned material attached to the inside of the guide 16, and the bearing 15 is to smoothly rotate the rotating cylinder 6.

본 고안은 모우터(3)에 의한 회전력을 감속기(4)로 알맞게 감속시켜 나선형 연료안내보(7)를 일정한 속도로 회전시키므로서 연료공급을 균일하게 할 수 있으며, 송풍기(10)에 의한 공기분출로 인하여 연료유출구(12)에서의 연료를 확산하되 공기유출구 (11)에 홴(13)을 설치하여 가이드(16) 내에서의 연료확산을 용이하게 할 수 있는 효과가 있다.The present invention can reduce the rotational force by the motor (3) accordingly to reduce the speed (4) to rotate the helical fuel guide (7) at a constant speed to uniform fuel supply, the air by the blower (10) Due to the ejection, the fuel is diffused at the fuel outlet 12, but the fin 13 is installed at the air outlet 11 to facilitate fuel diffusion in the guide 16.

Claims (1)

(정정)전체를 상부동체(1)와 하부동체(2)로 형성하되, 하부동체(2) 내에는 모우터(3)와 감속기(4)를 설치하여 체인(5)에 의해 상부동체(1)의 회전원통(6)을 회전시키도록하고, 회전원통(6)의 전방외주에 회전원통(6)과 일체로 회전되는 나선형연료안내부 (7)가 연료통(8)의 하단에 밀접되도록 한 버어너에 있어서, 회전원통(6)의 후방에는 외부로부터 회전원통(6)의 내측 공기통로(9)로 공기를 유입하는 송풍기(10)를 설치하며, 공기유출구(11)와 연료유출구(12)에는 각각 확산용 홴(13)과 불완전연소를 제거용 철편(14)을 결합시킨 분말연료를 사용하는 버너.(Correction) The whole body is formed of the upper body 1 and the lower body 2, but in the lower body 2, the motor 3 and the speed reducer 4 are installed, and the upper body 1 by the chain 5 To rotate the rotating cylinder (6), and the spiral fuel guide (7) integrally rotated with the rotating cylinder (6) on the front outer circumference of the rotating cylinder (6) to be close to the lower end of the fuel cylinder (8) In the burner, a rear side of the rotary cylinder 6 is provided with a blower 10 for introducing air from the outside into the inner air passage 9 of the rotary cylinder 6, and the air outlet 11 and the fuel outlet 12 Burner using powdered fuel, which combines diffusion fin (13) and incomplete combustion to remove iron pieces (14).
KR2019820008418U 1982-10-26 1982-10-26 Burner of the using powden fuel KR840001836Y1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR2019820008418U KR840001836Y1 (en) 1982-10-26 1982-10-26 Burner of the using powden fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR2019820008418U KR840001836Y1 (en) 1982-10-26 1982-10-26 Burner of the using powden fuel

Publications (2)

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KR840002336U KR840002336U (en) 1984-06-27
KR840001836Y1 true KR840001836Y1 (en) 1984-09-25

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KR2019820008418U KR840001836Y1 (en) 1982-10-26 1982-10-26 Burner of the using powden fuel

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KR840002336U (en) 1984-06-27

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