JPS6230552U - - Google Patents
Info
- Publication number
- JPS6230552U JPS6230552U JP1985121316U JP12131685U JPS6230552U JP S6230552 U JPS6230552 U JP S6230552U JP 1985121316 U JP1985121316 U JP 1985121316U JP 12131685 U JP12131685 U JP 12131685U JP S6230552 U JPS6230552 U JP S6230552U
- Authority
- JP
- Japan
- Prior art keywords
- combustion
- oil burner
- combustion section
- opposite
- section
- 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
Links
- 238000002485 combustion reaction Methods 0.000 claims description 15
- 238000010438 heat treatment Methods 0.000 claims description 4
- 238000005338 heat storage Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A40/00—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production
- Y02A40/10—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in agriculture
- Y02A40/25—Greenhouse technology, e.g. cooling systems therefor
Landscapes
- Greenhouses (AREA)
- Central Heating Systems (AREA)
Description
図面は本考案に係る温室用温調装置の実施例を
示し、第１図は一部切欠き正面図、第２図は一部
切欠き側面図、第３図は第２図の―線断面矢
視図、第４図は温調装置使用状態の正面図、第５
図はブロツク図である。第６図は従来温調装置の
加熱装置配設部の平面図である。
２……機体、３……蓄熱装置、４……石油バー
ナ、５……加熱装置、８ａ，８ｂ……送風装置、
１６ｂ……第１機体側壁、１７……燃焼部、１９
……燃焼排ガス排出管、１９ａ，１９ｂ……第１
排出管部分、１９ｃ……第２排出管部分、２０ａ
，２０ｂ……第２機体側壁、２２，２３，２４…
…支柱。
The drawings show an embodiment of the temperature control device for a greenhouse according to the present invention, in which Fig. 1 is a partially cutaway front view, Fig. 2 is a partially cutaway side view, and Fig. 3 is a cross section taken along the line - - in Fig. 2. Arrow view, Figure 4 is a front view of the temperature controller in use, Figure 5 is a front view of the temperature controller in use.
The figure is a block diagram. FIG. 6 is a plan view of a heating device installation part of a conventional temperature control device. 2... Airframe, 3... Heat storage device, 4... Oil burner, 5... Heating device, 8a, 8b... Air blower,
16b...First fuselage side wall, 17...Combustion part, 19
... Combustion exhaust gas discharge pipe, 19a, 19b ... 1st
Discharge pipe part, 19c...Second discharge pipe part, 20a
, 20b...Second fuselage side wall, 22, 23, 24...
...Strut.
Claims (1)
とは反対の側から突出し、前記燃焼部１７の横側
方を通つて前記燃焼部１７の前記石油バーナ４と
は反対の側に戻ると共に前記燃焼部１７に対して
前記石油バーナ４とは反対側に位置する第１機体
横側壁１６ｂを貫通するように屈曲形成された燃
焼排ガス排出管１９と、前記燃焼部１７とから成
る加熱装置５、及び、潜熱利用の蓄熱装置３を機
体２に内装すると共に、前記蓄熱装置３及び前記
加熱装置５を通過して前記機体２から流出するよ
うに温室内気を循環流動させる送風装置８ａ，８
ｂを設け、前記燃焼排ガス排出管１９のうちの前
記燃焼部１７の横側方に位置する第１排出管部分
（１９ａまたは１９ｂ）と、前記燃焼部１７とが
並ぶ第１方向にて相対向する一対の第２機体横側
壁２０ａ，２０ｂの間に位置させた状態で、かつ
、前記燃焼排ガス排出管１９のうちの前記燃焼部
１７に対して前記石油バーナ４とは反対の側に位
置する第２排出管部分１９ｃと、前記燃焼部１７
とが並ぶ第２方向から見て前記第１排出管部分１
９ａまたは１９ｂと前記燃焼部１７の間に在るよ
うに位置させた状態で、さらには、前記第２方向
に並べた状態で立設した複数本の支柱２２，２３
，２４を設けた温室用温調装置であつて、複数本
の前記支柱２２，２３，２４を前記第２排出管部
分１９ｃに対して前記燃焼部１７の側に位置させ
てある温室用温調装置。 The oil burner 4 of the combustion section 17 of the oil burner 4
protrudes from the side opposite to the oil burner 4, passes through the lateral side of the combustion part 17, returns to the side of the combustion part 17 opposite to the oil burner 4, and is opposite to the oil burner 4 with respect to the combustion part 17. A heating device 5 consisting of a combustion exhaust gas exhaust pipe 19 bent to penetrate the first body side wall 16b located on the side and the combustion section 17, and a heat storage device 3 using latent heat are installed inside the body 2. At the same time, blower devices 8a and 8 circulate and flow the greenhouse air so that it passes through the heat storage device 3 and the heating device 5 and flows out of the airframe 2.
b, and a first exhaust pipe portion (19a or 19b) of the combustion exhaust gas exhaust pipe 19 located laterally of the combustion section 17 and the combustion section 17 are arranged opposite to each other in the first direction. located between a pair of second body side walls 20a, 20b, and located on the side opposite to the oil burner 4 with respect to the combustion section 17 of the combustion exhaust gas discharge pipe 19. the second exhaust pipe section 19c and the combustion section 17
The first discharge pipe portion 1 viewed from the second direction where
9a or 19b and the combustion section 17, and furthermore, a plurality of pillars 22, 23 are arranged upright in the second direction.
. Device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1985121316U JPS6230552U (en) | 1985-08-07 | 1985-08-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1985121316U JPS6230552U (en) | 1985-08-07 | 1985-08-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6230552U true JPS6230552U (en) | 1987-02-24 |
Family
ID=31010472
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1985121316U Pending JPS6230552U (en) | 1985-08-07 | 1985-08-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6230552U (en) |
-
1985
- 1985-08-07 JP JP1985121316U patent/JPS6230552U/ja active Pending