JPS59145695A - Method and device for adjusting buoyancy of airship - Google Patents

Method and device for adjusting buoyancy of airship

Info

Publication number
JPS59145695A
JPS59145695A JP1814483A JP1814483A JPS59145695A JP S59145695 A JPS59145695 A JP S59145695A JP 1814483 A JP1814483 A JP 1814483A JP 1814483 A JP1814483 A JP 1814483A JP S59145695 A JPS59145695 A JP S59145695A
Authority
JP
Japan
Prior art keywords
buoyancy
gas
gas bag
airship
side heat
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
JP1814483A
Other languages
Japanese (ja)
Inventor
貴雄 鈴木
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.)
Mitsui Engineering and Shipbuilding Co Ltd
Mitsui Zosen KK
Original Assignee
Mitsui Engineering and Shipbuilding Co Ltd
Mitsui Zosen KK
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 Mitsui Engineering and Shipbuilding Co Ltd, Mitsui Zosen KK filed Critical Mitsui Engineering and Shipbuilding Co Ltd
Priority to JP1814483A priority Critical patent/JPS59145695A/en
Publication of JPS59145695A publication Critical patent/JPS59145695A/en
Pending legal-status Critical Current

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Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明に浮揚カスの放出、または・・ラストの使用を不
要とした飛行−船の浮力調節方法及びその浮力調節装置
に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a method for adjusting the buoyancy of an airship and a buoyancy adjustment device thereof that eliminates the need to release buoyant debris or use a last.

水素ガス、寸たはヘリュウガス等の浮揚ガスにより浮力
を得ている飛行船においては、温度や大気圧の変化及び
燃料消費による重量変化に対応するために、その浮力の
調節が必要であり、従来は浮揚ガスである水素やヘリュ
ウムの放出、−jだは水や砂などのバラストの便用によ
り飛行船の浮力調節を行なっている。
Airships that obtain their buoyancy from buoyancy gas such as hydrogen gas, hydrangea gas, or helium gas need to adjust their buoyancy to accommodate changes in temperature, atmospheric pressure, and weight changes due to fuel consumption. The buoyancy of the airship is adjusted by releasing buoyant gases such as hydrogen and helium, and by using ballast such as water or sand.

しかしながら、上記の飛行船では、バラスト所持による
ペイロードの減少、甘だは浮揚ガス放出による旨価なヘ
リュウム等の損失という問題があると共に、これらの調
節が不可逆調節であるだめ、その調節回数に限度がある
という欠点があった。
However, the above-mentioned airships have problems such as a reduction in payload due to the possession of ballast and a loss of valuable helium due to the release of buoyant gas, and since these adjustments are irreversible, there is a limit to the number of times they can be adjusted. There was a drawback.

そこで、本発明は前記従来の飛行船の浮力調節における
欠点を解消するためになされたものであり、飛行船の浮
力調節を浮揚ガスの放出、またはバラストの使用なしに
迅速、かつ可逆的に行ないうる飛行船の浮力調節方法及
びその装置を提供することを目的とし/ζものである。
SUMMARY OF THE INVENTION The present invention has been made to solve the above-mentioned drawbacks in adjusting the buoyancy of an airship. The object of the present invention is to provide a buoyancy adjustment method and device for the same.

即ち、本発明の浮力調節方法は、飛行船のガス袋内の浮
揚ガス体積を、熱電拐料からなる冷却素子によって、該
ガス袋内及び外気側にそれぞれ設けられた各ヒートパイ
プとの間の伝熱制御により、増減させることを特徴とし
たものであり、その浮力調節装置は、飛行船のガス袋内
に設けられたガス袋側伝熱器を有するカス袋側ヒートパ
イプと、外気側に設けられた外気側伝熱器を有する外気
側ヒーI・パイプとを、熱電月料からなる加熱冷却素子
のガス袋側伝熱板及0・外気側伝熱板でそれぞれ連絡す
ると共に、」=6己加熱冷却素子に、順方向、または逆
方向に電流を切替可能に流しつるコントローラを設ける
ことにより構成される。
That is, the buoyancy adjustment method of the present invention uses a cooling element made of thermoelectric material to transfer the buoyant gas volume in the gas bag of an airship to each heat pipe provided inside the gas bag and on the outside air side. The buoyancy adjustment device is characterized by increasing or decreasing the buoyancy by thermal control, and the buoyancy adjustment device includes a waste bag side heat pipe with a gas bag side heat transferer installed in the gas bag of the airship, and a gas bag side heat pipe installed on the outside air side. and an outside air side heat transfer pipe having an outside air side heat transfer device connected to the gas bag side heat exchanger plate and the outside air side heat exchanger plate of the heating/cooling element made of thermoelectric power, respectively, and It is constructed by providing the heating/cooling element with a controller that allows current to flow in a forward or reverse direction in a switchable manner.

以下図面を参照して本発明の一実施例を説明するが、図
面は本発明の実施例における飛行船の概略構成図であり
、図中の1は飛行船の外殻、2はガス袋、6はへリュウ
ム等の浮揚ガス、4は太陽光、5は太陽電池、6は加熱
冷却素子、7はガス袋側伝熱板、8は外気側伝熱板、9
はガス袋側ヒートバイブ、10は外気側ピー1パイプ、
11はガス袋側伝熱器、12は外気側伝熱器である。
An embodiment of the present invention will be described below with reference to the drawings, which are schematic configuration diagrams of an airship in an embodiment of the present invention. In the drawings, 1 is the outer shell of the airship, 2 is a gas bag, and 6 is a Floating gas such as helium, 4 is sunlight, 5 is a solar cell, 6 is a heating and cooling element, 7 is a gas bag side heat exchanger plate, 8 is an outside air side heat exchanger plate, 9
is the heat vibrator on the gas bag side, 10 is the P1 pipe on the outside air side,
11 is a gas bag side heat transfer device, and 12 is an outside air side heat transfer device.

」二記のカス袋2内に設けられたガス袋側伝熱器11を
南するガス袋側ヒートバイブ9と、外気側に設けられた
外気1p11伝熱器12を有する外気側ヒ−]・パイプ
10とは、B12− Te3.  Pb −Te +B
+2Te3  Sb2Te3.B’2Te3  ’B’
2Se3なとの熱電イ」別からなる加熱冷却素子乙のガ
ス袋側伝熱板7及び外気(till伝熱板8てそれぞれ
連絡すると共に、その加熱冷却素子6に、順方向、また
は逆方向に電流を切替可能に流しうるコントローラ13
を設けている。
``An outside air side heater having a gas bag side heat vibrator 9 extending south of the gas bag side heat transfer device 11 provided in the waste bag 2 mentioned above, and an outside air 1p11 heat transferer 12 provided on the outside air side] The pipe 10 is B12-Te3. Pb −Te +B
+2Te3 Sb2Te3. B'2Te3 'B'
The heating and cooling element B, which is composed of a thermoelectric device 2 and 3, is connected to the gas bag side heat transfer plate 7 and the outside air (till heat transfer plate 8), respectively, and the heating and cooling element 6 is connected to the air in the forward or reverse direction. Controller 13 that can switchably flow current
has been established.

そこで、上記の構成からなる本発明の実施例の浮力調節
装置において浮力を増す際には、上記の加熱冷却素子6
に順方向に電流を流すと、カス袋側伝熱板7が発熱し、
外気側伝熱板8は吸熱する。
Therefore, when increasing the buoyancy in the buoyancy adjustment device of the embodiment of the present invention having the above configuration, the heating/cooling element 6
When a current is passed in the forward direction, the waste bag side heat exchanger plate 7 generates heat,
The outside air side heat exchanger plate 8 absorbs heat.

ガス袋側伝熱器11から浮揚ガス乙に伝えられ、浮揚ガ
ス乙の温度は上がり、膨張による体積増の結果、飛行船
の浮力が増すことになる。
It is transmitted from the gas bag side heat transfer device 11 to the floating gas B, and the temperature of the floating gas B increases, and as a result of the volume increase due to expansion, the buoyancy of the airship increases.

一方、吸熱側は、外気側伝熱器12から得だ熱が外気側
ヒートパイプ10を経て、外気側伝熱板8に伝えられる
On the other hand, on the heat absorption side, the heat obtained from the outside air side heat transfer device 12 is transmitted to the outside air side heat exchanger plate 8 via the outside air side heat pipe 10.

なお、以上の作動時はカス袋2内のガス6の温度を迅速
、かつ均一に変化させるためにファン19による攪拌を
行なうようにしている。
Incidentally, during the above operation, stirring is performed by the fan 19 in order to quickly and uniformly change the temperature of the gas 6 in the waste bag 2.

また、上記の電流の流れ方向の切替(は、リレースイッ
チ内蔵のコントローラ13によって行なわれる。
Further, the above-mentioned switching of the current flow direction is performed by a controller 13 having a built-in relay switch.

次に、浮力を減する時には、加熱冷却素子乙に逆方向の
電流を流すことによる上記と逆の作用により、浮揚ガス
乙の温度は下がり、体積減となる結果浮力が減する。
Next, when reducing the buoyancy, the temperature of the buoyant gas B decreases due to the opposite effect of flowing a current in the opposite direction to the heating/cooling element B, and the volume decreases, resulting in a decrease in buoyancy.

以上のごとく、本発明の浮力調節装置を使用して浮力の
増減を小きざみに調節することができるが、一方、浮力
調節の幅が犬で前記の温度による本発明の浮力調節方法
で徒かなえない場合、もしくは調節後の状態が長時間に
わたる場合、本実施例においては、ガス袋2に連結した
一B、<コンプンツサ18、カスタンク17、弁16ヲ
用いて浮力調節を行なうこともできる。
As described above, the buoyancy adjustment device of the present invention can be used to adjust the increase or decrease of buoyancy in small steps. If not, or if the condition after adjustment lasts for a long time, in this embodiment, the buoyancy can also be adjusted using the 1B, the compressor 18, the gas tank 17, and the valve 16 connected to the gas bag 2.

すなわち、浮力を減らす場合は、ガスコンプレソザ18
によりガス袋2内の浮揚カス6をガスタンク17に送り
、丑だ浮力を増す場合は、弁16を開いてカスタンク1
7の浮揚ガス3をガス袋2に送ることによってガス袋2
内の浮揚カス3の体j(’lを大幅に増減可能となって
いる。
In other words, when reducing buoyancy, the gas compressor 18
If you want to increase the buoyancy by sending the floating debris 6 in the gas bag 2 to the gas tank 17, open the valve 16 and transfer the floating debris 6 from the gas bag 2 to the gas tank 17.
By sending the levitation gas 3 of 7 to the gas bag 2, the gas bag 2
It is possible to significantly increase or decrease the body j('l) of floating debris 3 inside.

な二ひ、上記実施例の飛行船における各機器の作動の動
力源1j2、主として飛行船の外殻−上表面に設置1″
′1し、た太陽電池5により、太陽光4から得られ、蓄
’rJi a 14に蓄わえられた′重力によるものと
し、不足分は神助′屯源15により袖うようにしている
The power source 1j2 for operating each device in the airship of the above embodiment is mainly installed on the outer shell-upper surface of the airship 1''
It is assumed that the gravity is obtained from the sunlight 4 by the solar cell 5 and stored in the storage 14, and the shortfall is made up by the Kamisuke tungen 15.

従って、上1、己実施例の浮力Ah’、I節装置を孫装
置/こ飛行船において、浮力のgl、調節は本発明のペ
ルチェ効果を利用した加熱冷却装置と、ヒートパイプに
よる浮揚ガスの温度調節により行なうが、浮力の太りぶ
調節のうち、浮力を減するときは、ガス袋に連結したガ
スコンプレッサーによりガスタンクに浮揚ガスを送り、
浮力を増すときは、弁を開放してガスタンク内の浮揚カ
スをガス袋に送るようにしており、1だ、上記の各機器
に要する電力は主に飛行船の外殻界面上部に設置した太
陽型l■から伺るようにしている。
Therefore, in the above 1, the buoyancy Ah' of the own embodiment, the buoyancy gl of the device in section I and the grandchild device/this airship are adjusted by the heating/cooling device using the Peltier effect of the present invention and the temperature of the buoyant gas by the heat pipe. This is done by adjusting the buoyancy, but when reducing the buoyancy, a gas compressor connected to the gas bag sends buoyancy gas to the gas tank.
When increasing the buoyancy, a valve is opened to send the floating debris in the gas tank to the gas bag. I try to ask from l■.

その結果、本発明を適用した飛行船の浮力調節装置では
、浮揚ガスの放出や、バラストを使用することなく、迅
速、かつ可逆的な浮力調節を広範囲にわたって行なうこ
とができる。
As a result, the buoyancy adjustment device for an airship to which the present invention is applied can quickly and reversibly adjust buoyancy over a wide range without releasing buoyancy gas or using ballast.

特に、本発明の浮力調節装置はベルチェ//JJ果を用
いた加熱冷却素子と、ヒートパイプとjl(よる浮揚ガ
スの高度制御による浮力の微調節かできるという利点が
ある。
In particular, the buoyancy adjustment device of the present invention has the advantage of being able to finely adjust the buoyancy by controlling the height of the levitation gas using a heating/cooling element using a Beltier//JJ filter, a heat pipe, and a buoyant gas.

【図面の簡単な説明】[Brief explanation of the drawing]

図面は本発明の実施例における飛行船の概略構成図であ
る。 2・・ガス袋、6・浮揚ガス、6・、加熱冷却素子、7
・・・ガス象側伝熱板、8・・外気イ(1す伝熱板、9
・・ガス袋イ11リヒートパイプ、1o・・外気側ヒー
トパイプ、11・・ガス袋側伝熱器、12・・外気側伝
熱器、16・・コントローラ。 代理人 弁理士 小 川 信 − 弁理士  野  口  賢  照 弁理士 媚 下 和 彦
The drawing is a schematic configuration diagram of an airship in an embodiment of the present invention. 2. Gas bag, 6. Levitating gas, 6. Heating/cooling element, 7
...Gas side heat transfer plate, 8...Outside air A (1 heat transfer plate, 9
...Gas bag A11 reheat pipe, 1o.Outside air side heat pipe, 11..Gas bag side heat transferer, 12..Outside air side heat transferer, 16..Controller. Agent: Patent Attorney Makoto Ogawa - Patent Attorney: Masaru Noguchi Patent Attorney: Kazuhiko Ashita

Claims (1)

【特許請求の範囲】 1 飛行船のガス袋内の浮揚ガス体積を、熱電洞料から
なる加熱冷却素子によって、該ガス袋内及び外気側にそ
れぞれ設けられた各ヒートパイプの間の伝熱制御によシ
、増減さぜることを特徴とする飛行船の浮力調節方法。 2 飛行船のガス袋内に設けられたガス袋側伝熱器を有
するガス袋側ヒートパイプと、外気側に設けられた外気
側伝熱器を有する外気側ヒートパイプとを熱電材料から
なる加熱冷却素子のガス袋011J伝熱板及び外気側伝
熱板でそれぞれ連絡すると共に、上記加熱冷却素子に、
順方向また(は逆方向に電流を切替可能に流しうるコノ
トローラを設けたことを特徴とする飛行船の浮力調節装
置。
[Claims] 1. The volume of floating gas in the gas bag of an airship is controlled by heat transfer between heat pipes installed inside the gas bag and on the outside air side using a heating and cooling element made of a thermoelectric material. A method for adjusting the buoyancy of an airship, which is characterized by increasing and decreasing the buoyancy. 2 A gas bag-side heat pipe with a gas bag-side heat transferer installed in the airship's gas bag and an outside-air side heat pipe with an outside-air side heat transferer installed in the outside air side are heated and cooled using thermoelectric materials. While communicating with the gas bag 011J heat exchanger plate of the element and the outside air side heat exchanger plate, the heating and cooling element is connected to the
A buoyancy adjustment device for an airship, characterized in that it is provided with a conotrol that can switchably flow a current in the forward direction or in the reverse direction.
JP1814483A 1983-02-08 1983-02-08 Method and device for adjusting buoyancy of airship Pending JPS59145695A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1814483A JPS59145695A (en) 1983-02-08 1983-02-08 Method and device for adjusting buoyancy of airship

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1814483A JPS59145695A (en) 1983-02-08 1983-02-08 Method and device for adjusting buoyancy of airship

Publications (1)

Publication Number Publication Date
JPS59145695A true JPS59145695A (en) 1984-08-21

Family

ID=11963411

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1814483A Pending JPS59145695A (en) 1983-02-08 1983-02-08 Method and device for adjusting buoyancy of airship

Country Status (1)

Country Link
JP (1) JPS59145695A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002536246A (en) * 1999-02-09 2002-10-29 アドバンスト テクノロジーズ グループ リミティド Positioning of solar array on airship
JP2010006366A (en) * 2008-04-18 2010-01-14 Lockheed Martin Corp Laminate structure storing electronic equipment and method therefor
JP2013532088A (en) * 2010-05-25 2013-08-15 ニュー クリエイト リミテッド Controllable levitation system and method
JP5875093B1 (en) * 2015-06-17 2016-03-02 浩平 中村 Levitation aircraft

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002536246A (en) * 1999-02-09 2002-10-29 アドバンスト テクノロジーズ グループ リミティド Positioning of solar array on airship
JP4719842B2 (en) * 1999-02-09 2011-07-06 ハイブリッド エア ビークルズ リミティド Solar cell array positioning on an airship
JP2010006366A (en) * 2008-04-18 2010-01-14 Lockheed Martin Corp Laminate structure storing electronic equipment and method therefor
JP2013532088A (en) * 2010-05-25 2013-08-15 ニュー クリエイト リミテッド Controllable levitation system and method
JP5875093B1 (en) * 2015-06-17 2016-03-02 浩平 中村 Levitation aircraft
WO2016204180A1 (en) * 2015-06-17 2016-12-22 浩平 中村 Buoyant flying body
JP2017007411A (en) * 2015-06-17 2017-01-12 浩平 中村 Floating type flying body
US9802691B2 (en) 2015-06-17 2017-10-31 Kohei Nakamura Buoyant aerial vehicle

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