JPS6238809A - Power plant by temperature difference - Google Patents
Power plant by temperature differenceInfo
- Publication number
- JPS6238809A JPS6238809A JP17801885A JP17801885A JPS6238809A JP S6238809 A JPS6238809 A JP S6238809A JP 17801885 A JP17801885 A JP 17801885A JP 17801885 A JP17801885 A JP 17801885A JP S6238809 A JPS6238809 A JP S6238809A
- Authority
- JP
- Japan
- Prior art keywords
- fluid
- heat receiving
- heat
- receiving part
- circulating system
- 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
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野コ
本発明は温度差から動力を得ようとする温度差動力装置
に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a temperature differential power device that attempts to obtain power from a temperature difference.
[技術的背景]
たとえば宇宙空間に打ち上げられた宇宙船1人工衛星等
は太陽からの強烈な輻射熱をあびて日なた側は高温度に
加熱され、反対の日影側は低温状態にあり大きな温度差
がある。そこでその温度差を緩和するものとして周知の
ヒートパイプがあるが、このヒートパイプは単に温度差
を緩和するだけのものであった。[Technical background] For example, a spacecraft or a satellite launched into outer space is exposed to intense radiant heat from the sun and is heated to a high temperature on the sunny side, while the opposite shaded side is cold and large. There is a temperature difference. There is a well-known heat pipe that alleviates this temperature difference, but this heat pipe only serves to alleviate the temperature difference.
[本発明の目的および構成]
本発明はヒートパイプの技術をさらに一歩進め、流体が
熱を伴なって循環系内で移動するときの運動エネルギー
を有効に利用せんとするものであり、この目的を達成す
るため本発明は外部から閉鎖された循環系の一端に受熱
部を設け他端に放熱部を設けると共に、該循環系内に受
熱部によって加熱されて気化し放熱部によって冷却され
て液化する流体を充填し、該流体の受熱部と放熱部との
間の行路途中に気化した流体の流動によって動かされる
翼車等の起動力装置を設け、該流体の放熱部と受熱部と
の間の帰路途中に毛管部が設けられてなる温度差動力装
置を提供するものである。[Objects and Structure of the Present Invention] The present invention takes heat pipe technology one step further and aims to effectively utilize kinetic energy when a fluid moves with heat in a circulation system. In order to achieve this, the present invention provides a heat receiving section at one end of a circulation system that is closed from the outside and a heat dissipation section at the other end. A motive force device such as a blade wheel that is moved by the flow of the vaporized fluid is provided between the heat receiving part and the heat radiating part of the fluid, and a driving force device such as a blade wheel that is moved by the flow of the vaporized fluid is provided between the heat receiving part and the heat receiving part of the fluid. The present invention provides a temperature differential power device in which a capillary portion is provided on the return path of the temperature differential power device.
[実施例]
第1図に示した温度差動力装置について説明すれば、1
は外部から閉鎖された環状の循環系でその内部には流体
2が充填されている。3はこの循環系1の一端に適当な
広さの受熱面積をもち熱伝導性に優れた材料により設け
られた受熱部である。[Example] To explain the temperature differential power device shown in FIG. 1, 1
is an annular circulation system closed from the outside, and the inside thereof is filled with fluid 2. Reference numeral 3 denotes a heat receiving portion provided at one end of the circulation system 1 and made of a material having an appropriate heat receiving area and excellent thermal conductivity.
4はこの循環系1の他端に設けられた放熱部である。5
は受熱部3を囲繞する保温断熱材、6は放熱部4を囲繞
する放熱材を示す。かかる循環系1では流体2が受熱部
3によって加熱され気化すると、その蒸気が放熱部4へ
向かって流動し、放熱部4によって冷やされて液化した
復元の流体2となり、毛管部12の毛細管現象により受
熱部3へ □戻される。そして受熱部3へ戻ってきた流
体2は再加熱されて気化し同じ運動をくり返すもので、
このために受熱部3の熱が放熱部4へ際限なく伝えられ
る。かくして本発明では該流体2の受熱部3と放熱部4
との間の行路途中に起動力装置7を設ける。図示した起
動力装置7は翼車8と出力軸9とよりなり、翼車8を行
路に臨ませると共に出力軸9を循環系1外へ導出させて
いる。4 is a heat dissipation section provided at the other end of this circulation system 1. 5
6 indicates a heat-retaining insulating material surrounding the heat receiving section 3, and 6 indicates a heat dissipating material surrounding the heat dissipating section 4. In this circulation system 1, when the fluid 2 is heated and vaporized by the heat receiving part 3, the vapor flows toward the heat radiating part 4, and is cooled by the heat radiating part 4 and becomes the liquefied restoration fluid 2, which causes capillary action in the capillary part 12. It is returned to the heat receiving part 3 by □. Then, the fluid 2 that returns to the heat receiving part 3 is reheated and vaporized, repeating the same movement.
Therefore, the heat of the heat receiving part 3 is transmitted to the heat radiating part 4 without limit. Thus, in the present invention, the heat receiving part 3 and the heat radiating part 4 of the fluid 2 are
A starting force device 7 is provided in the middle of the journey between. The illustrated starting force device 7 is composed of a blade wheel 8 and an output shaft 9, with the blade wheel 8 facing the path and the output shaft 9 leading out of the circulation system 1.
しかしてこのように構成された温度差動力装置では、流
体2が熱を伴なって循環系1内を移動するとき、その運
動エネルギーにより翼車8を回す。However, in the temperature differential power device configured in this way, when the fluid 2 moves in the circulation system 1 accompanied by heat, the impeller 8 is rotated by its kinetic energy.
そのために該翼車8の回転力が出力軸9を介して循環系
1外へ取り出される。Therefore, the rotational force of the impeller 8 is extracted to the outside of the circulation system 1 via the output shaft 9.
なお、本願における毛管部は管状のものに限られるもの
ではなく毛細管現象が起こるものなら吸取紙状のものス
ポンジ状のものであってもかまわない。Note that the capillary portion in the present application is not limited to a tubular shape, but may be a blotter-like or sponge-like shape as long as capillarity occurs.
第2図は他の実施例に係る動力装置を示したものである
が、この例では受熱部3の受熱側表面に黒色塗料の被膜
10を形成している。このようにすれば、被膜10が熱
を良く吸収するので受熱部3による受熱効率が高まり、
流体2の運動エネルギーが増大する。したがって起動力
装置7により取り出される動力も大きなものとなる。FIG. 2 shows a power plant according to another embodiment, and in this example, a black paint coating 10 is formed on the heat receiving side surface of the heat receiving portion 3. In this way, since the coating 10 absorbs heat well, the heat receiving efficiency by the heat receiving part 3 increases,
The kinetic energy of fluid 2 increases. Therefore, the power extracted by the starting force device 7 also becomes large.
第3図に示した動力装置は、更に集光レンズ11を受熱
部3および黒色被膜1oの前方に衝立状に設けており、
このようにすれば、集光レンズ11を介して多量の受熱
が可能となり一層大きな動力を取り出すことができるも
のである。The power plant shown in FIG. 3 further includes a condensing lens 11 arranged in a screen-like manner in front of the heat receiving section 3 and the black coating 1o.
In this way, a large amount of heat can be received through the condenser lens 11, and even greater power can be extracted.
[発明の効果]
外部から閉鎖された循環系内で流体が受熱部より放熱部
へ向かって移動するときの運動エネルギーを起動力とし
て取り出せるようにしたものであるから、太陽光などの
熱源さえあれば機能し、特別な電源、燃料、電池などは
必要でない。したがって、宇宙空間において宇宙船や人
工衛星等の動力源とじてに利用することができるなど有
益である。[Effects of the invention] Since the kinetic energy generated when the fluid moves from the heat receiving part toward the heat radiating part in a circulation system closed from the outside can be extracted as a driving force, it is possible to use even a heat source such as sunlight. It is fully functional and requires no special power source, fuel, or batteries. Therefore, it is advantageous that it can be used as a power source for spacecraft, artificial satellites, etc. in outer space.
図面は本発明の実施例を示したもので、第1図は縦断面
図、第2図および第3図は他の実施例の縦断面図である
。
■・・・・循環系、2・・・・流体、3・・・・受熱部
、4・・・・放熱部、7・・・・起動力装置、8・・・
・翼車、12・・・・毛管部。
特許出願人 大同特殊鋼株式会社
第2図
第 8 図The drawings show an embodiment of the present invention, and FIG. 1 is a longitudinal sectional view, and FIGS. 2 and 3 are longitudinal sectional views of other embodiments. ■... Circulation system, 2... Fluid, 3... Heat receiving section, 4... Heat radiation section, 7... Starting force device, 8...
- Impeller, 12... Capillary section. Patent applicant: Daido Steel Co., Ltd. Figure 2 Figure 8
Claims (1)
放熱部を設けると共に、該循環系内に受熱部によつて加
熱されて気化し放熱部によつて冷却されて液化する流体
を充填し、該流体の受熱部と放熱部との間の行路途中に
気化した流体の流動によつて動かされる翼車等の起動力
装置を設け、該流体の放熱部と受熱部との間の帰路途中
に毛管部が設けられてなることを特徴とする温度差動力
装置。A heat receiving section is provided at one end of a circulation system that is closed from the outside, and a heat radiating section is provided at the other end, and a fluid that is heated by the heat receiving section and vaporized and cooled by the heat radiating section and liquefied is contained in the circulation system. A driving force device such as a impeller, which is moved by the flow of the vaporized fluid, is installed between the heat receiving part and the heat radiating part of the fluid, and A temperature difference power device characterized in that a capillary section is provided on the way back.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17801885A JPS6238809A (en) | 1985-08-13 | 1985-08-13 | Power plant by temperature difference |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17801885A JPS6238809A (en) | 1985-08-13 | 1985-08-13 | Power plant by temperature difference |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6238809A true JPS6238809A (en) | 1987-02-19 |
Family
ID=16041131
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP17801885A Pending JPS6238809A (en) | 1985-08-13 | 1985-08-13 | Power plant by temperature difference |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6238809A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62137306U (en) * | 1986-02-24 | 1987-08-29 | ||
JP2011099660A (en) * | 2009-10-05 | 2011-05-19 | Denso Corp | Heat engine |
US9371744B2 (en) | 2009-10-05 | 2016-06-21 | Denso Corporation | Heat engine |
-
1985
- 1985-08-13 JP JP17801885A patent/JPS6238809A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62137306U (en) * | 1986-02-24 | 1987-08-29 | ||
JP2011099660A (en) * | 2009-10-05 | 2011-05-19 | Denso Corp | Heat engine |
JP2011099661A (en) * | 2009-10-05 | 2011-05-19 | Denso Corp | Heat engine |
US9371744B2 (en) | 2009-10-05 | 2016-06-21 | Denso Corporation | Heat engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4320246A (en) | Uniform surface temperature heat pipe and method of using the same | |
US4513732A (en) | Passive integral solar heat collector system | |
US4217882A (en) | Passive solar heat collector | |
US4033118A (en) | Mass flow solar energy receiver | |
SU797613A3 (en) | Sun irradiation collector | |
US5931156A (en) | Integral heat-pipe type solar collector | |
US8484974B1 (en) | Dual-phase thermal electricity generator | |
US3903699A (en) | Solar energy power system | |
US4267826A (en) | Solar collector for heating and cooling | |
US4856281A (en) | Solar power plant and still | |
US3957030A (en) | Solar energy power system | |
EP2507846B1 (en) | Energy generation system | |
US5586549A (en) | Combined solar and gas heater | |
JPS6238809A (en) | Power plant by temperature difference | |
US5261390A (en) | System for heating fluid in process equipment with solar energy | |
CA1283549C (en) | Heat pipe having a turbine built therein and apparatus using same | |
Sodha et al. | Transient analysis of closed loop solar water heating system | |
JPS62101086A (en) | Solar battery cooling system | |
RU2013656C1 (en) | Power plant | |
US20080000469A1 (en) | Unknown | |
JPS5853261B2 (en) | solar energy collector | |
JPH0322696Y2 (en) | ||
JPH0447570Y2 (en) | ||
US4160444A (en) | Omnidirectional heat pipe | |
JPH01190274A (en) | Space solar thermal power generation system |