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JP7071771B2 - Flying object container - Google Patents
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JP7071771B2 - Flying object container - Google Patents

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JP7071771B2
JP7071771B2 JP2021153606A JP2021153606A JP7071771B2 JP 7071771 B2 JP7071771 B2 JP 7071771B2 JP 2021153606 A JP2021153606 A JP 2021153606A JP 2021153606 A JP2021153606 A JP 2021153606A JP 7071771 B2 JP7071771 B2 JP 7071771B2
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container
small space
container body
space
gas
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JP2022051566A (en
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圭介 岩谷
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株式会社岩谷技研
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Priority to CN202210262472.9A priority patent/CN115107985A/en
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本発明は、気球、飛行船等の飛翔体のための容器に関する。 The present invention relates to a container for a flying object such as a balloon or an airship.

人(搭乗員)を収容する容器であるキャビンの設けられた気球、飛行船等の飛翔体がある。そのような飛翔体によれば、人は空中を移動できる。 There are flying objects such as balloons and airships equipped with cabins that are containers for accommodating people (crew members). According to such a projectile, a person can move in the air.

人を収容するキャビンを備える飛翔体を開示している特許文献として、例えば特許文献1がある。特許文献1には、人を収容したドローン本体を気球で吊って飛翔させる構造を備えた有人ドローンが提案されている。 For example, Patent Document 1 discloses a flying object including a cabin for accommodating a person. Patent Document 1 proposes a manned drone having a structure in which a drone body containing a person is suspended by a balloon and flies.

特開2020-97345号公報Japanese Unexamined Patent Publication No. 2020-9734

飛翔体の地上からの高度が高くなる程、一般的に周囲の温度は低下する。従って、飛翔体のキャビンの内側の空気の温度に対し、キャビンの壁面の温度が低くなり、キャビンの壁面に接する空気が冷却されて、空気中に含まれる水蒸気が水に変化し、壁面の内側に露として付着する現象である結露が生じる場合がある。 The higher the altitude of the projectile from the ground, the lower the ambient temperature. Therefore, the temperature of the wall surface of the cabin becomes lower than the temperature of the air inside the cabin of the flying object, the air in contact with the wall surface of the cabin is cooled, the water vapor contained in the air changes to water, and the inside of the wall surface. Dew may occur, which is a phenomenon that adheres to the air as dew.

キャビンの壁面の一部が窓(光を透過する板)である場合、その窓に結露が生じると、キャビン内の搭乗員がキャビン外を視認しにくくなる。また、キャビンの壁面に結露が生じて、発生した水がその近辺の電子機器等に浸水すると、浸水された電子機器等が故障する等の不都合が生じ得る。 When a part of the wall surface of the cabin is a window (a plate that transmits light), if dew condensation occurs on the window, it becomes difficult for the crew inside the cabin to see the outside of the cabin. Further, if dew condensation occurs on the wall surface of the cabin and the generated water infiltrates the electronic equipment or the like in the vicinity thereof, inconveniences such as failure of the inundated electronic equipment or the like may occur.

また、飛翔体が、撮影装置等の装置を収容した容器を備える場合がある。そのような容器においても、上述したキャビンと同様に、容器の壁面の内側に結露が生じると、発生した水により容器内の装置が故障する等の不都合が生じ得る。 Further, the projectile may include a container containing a device such as a photographing device. Even in such a container, as in the case of the above-mentioned cabin, if dew condensation occurs on the inside of the wall surface of the container, the generated water may cause inconvenience such as failure of the device in the container.

また、飛翔体が、撮影装置を収容した容器を備える場合、撮影装置の画角内に入る容器の壁面は光を透過する窓とする必要がある。この窓に結露が生じると、撮影装置が撮影する画像の焦点が合わなかったり、結露により生じた水滴が撮影した画像に写り込んだりする。 Further, when the flying object is provided with a container accommodating the photographing device, the wall surface of the container entering the angle of view of the photographing device needs to be a window through which light is transmitted. When dew condensation occurs on this window, the image captured by the photographing device may be out of focus, or water droplets generated by the dew condensation may be reflected in the captured image.

上記の事情に鑑み、本発明は、飛翔体が備える容器内で結露が生じる確率を低減する手段を提供する。 In view of the above circumstances, the present invention provides means for reducing the probability of dew condensation occurring in the container provided in the projectile.

本発明は、飛翔体が備える容器であって、器本体と、前記容器本体の内部の空間を、収容物を収容する第1の小空間と、前記第1の小空間とは異なる第2の小空間に仕切る仕切り板とを備え、前記仕切り板は、前記第1の小空間と前記第2の小空間の間に生じた圧力差を解消するように前記第1の小空間と前記第2の小空間の間に気体の出入りを生じさせるが、前記第1の小空間と前記第2の小空間の間に気体の対流を生じさせない大きさの1以上の孔を有し、前記第1の小空間内の気体が接する前記容器本体の面積に対する前記第1の小空間内の気体の容積は、前記第2の小空間内の気体が接する前記容器本体の面積に対する前記第2の小空間内の気体の容積より大きい容器を第1の態様として提案する。 The present invention is a container included in the flying object, and the space inside the container body and the container body is different from the first small space for accommodating the contained object and the first small space. The partition plate is provided with a partition plate for partitioning from the small space of the above, and the partition plate is provided with the first small space and the partition plate so as to eliminate a pressure difference generated between the first small space and the second small space. It has one or more holes of a size that causes gas in and out between the second small space but does not cause gas convection between the first small space and the second small space. The volume of the gas in the first small space with respect to the area of the container body in contact with the gas in the first small space is the second with respect to the area of the container body in contact with the gas in the second small space. A container larger than the volume of gas in a small space is proposed as the first aspect.

また、本発明は、飛翔体が備える容器であって、器本体と、前記容器本体の内部の空間を、収容物を収容する第1の小空間と、前記第1の小空間とは異なる第2の小空間に仕切る仕切り板とを備え、前記容器本体の前記第2の小空間を形成している部分、前記第2の小空間と前記容器本体の外部の空間の間に生じた圧力差を解消するように前記第2の小空間と前記容器本体の外部の空間の間に気体の出入りを生じさせるが、前記第2の小空間と前記容器本体の外部の空間の間に気体の対流を生じさせない大きさの1以上の孔を有する容器を第2の態様として提案する。 Further, the present invention is a container included in the flying object, and the space inside the container body and the container body is different from the first small space for accommodating the contained object and the first small space. A portion of the container body having a partition plate partitioning the second small space and forming the second small space is formed between the second small space and the space outside the container body. Gas enters and exits between the second small space and the space outside the container body so as to eliminate the pressure difference, but between the second small space and the space outside the container body. A container having one or more holes having a size that does not cause gas convection is proposed as a second embodiment.

第1又は第2の態様に係る容器において、前記第1の小空間に前記容器本体の外部から光が透過するように、前記容器本体の少なくとも一部と前記仕切り板の少なくとも一部が光を透過する、という構成が第3の態様として採用されてもよい。 In the container according to the first or second aspect, at least a part of the container body and at least a part of the partition plate emit light so that light is transmitted from the outside of the container body to the first small space. The configuration of being transparent may be adopted as the third aspect.

また、本発明は、飛翔体が備える容器であって、収容物を収容する第1の容器本体と、前記第1の容器本体を収容する第2の容器本体とを備え、前記第1の容器本体の内部の空間を第1の小空間とし、前記第1の容器本体と前記第2の容器本体の間の空間を第2の小空間とするとき、前記第1の容器本体は、前記第1の小空間と前記第2の小空間の間に生じた圧力差を解消するように前記第1の小空間と前記第2の小空間の間に気体の出入りを生じさせるが、前記第1の小空間と前記第2の小空間の間に気体の対流を生じさせない大きさの1以上の孔を有する容器を第4の態様として提案する。 Further, the present invention is a container included in the flying object, which includes a first container body for accommodating an object and a second container body for accommodating the first container body, and the first container. When the space inside the main body is defined as the first small space and the space between the first container body and the second container body is defined as the second small space, the first container body is the first container body . Gas enters and exits between the first small space and the second small space so as to eliminate the pressure difference generated between the small space 1 and the second small space, but the first As the fourth aspect, a container having one or more holes having a size that does not cause gas convection between the small space of No. 1 and the second small space is proposed.

また、本発明は、飛翔体が備える容器であって、収容物を収容する第1の容器本体と、前記第1の容器本体を収容する第2の容器本体とを備え、前記第1の容器本体と前記第2の容器本体の間の空間を小空間とするとき、前記第2の容器本体は、前記小空間と前記第2の容器本体の外部の空間の間に生じた圧力差を解消するように前記小空間と前記第2の容器本体の外部の空間の間に気体の出入りを生じさせるが、前記小空間と前記第2の容器本体の外部の空間の間に気体の対流を生じさせない大きさの1以上の孔を有する容器を第5の態様として提案する。 Further, the present invention is a container included in the flying object, which includes a first container body for accommodating an object and a second container body for accommodating the first container body, and the first container. When the space between the main body and the second container main body is a small space, the second container main body eliminates the pressure difference generated between the small space and the space outside the second container main body. As such, gas enters and exits between the small space and the space outside the second container body, but gas convection occurs between the small space and the space outside the second container body. A container having one or more holes having a size that does not allow it to be prevented is proposed as a fifth aspect.

第4又は第5の態様に係る容器において、前記第1の容器本体の内部の空間に前記第2の容器本体の外部から光が透過するように、前記第1の容器本体の少なくとも一部と前記第2の容器本体の少なくとも一部が光を透過する、という構成が第6の態様として採用されてもよい。 In the container according to the fourth or fifth aspect, with at least a part of the first container body so that light is transmitted from the outside of the second container body into the space inside the first container body. A configuration in which at least a part of the second container body transmits light may be adopted as the sixth aspect.

本発明によれば、容器内に形成される2つの空間における温度に差が生じる結果、結露が生じにくい。 According to the present invention, as a result of a difference in temperature between the two spaces formed in the container, dew condensation is unlikely to occur.

第1実施形態に係る飛翔体の全体構成を示した図。The figure which showed the whole composition of the flying object which concerns on 1st Embodiment. 第1実施形態に係る容器の構成を示した図。The figure which showed the structure of the container which concerns on 1st Embodiment. 第2実施形態に係る容器の構成を示した図。The figure which showed the structure of the container which concerns on 2nd Embodiment. 第3実施形態に係る容器の構成を示した図。The figure which showed the structure of the container which concerns on 3rd Embodiment. 第4実施形態に係る容器の構成を示した図。The figure which showed the structure of the container which concerns on 4th Embodiment. 一変形例に係る容器の構成を示した図。The figure which showed the structure of the container which concerns on one modification.

[第1実施形態]
図1は、本発明の第1実施形態に係る飛翔体1の全体構成を示した図である。飛翔体1は、ヘリウム等の空気より軽い気体を収容する球皮11と、球皮11に吊られて飛翔する容器12と、球皮11に一方の端部が連結され容器12に他方の端部が連結されて球皮11が容器12を吊るために設けられている複数の索体である吊索13を備える。
[First Embodiment]
FIG. 1 is a diagram showing the overall configuration of the flying object 1 according to the first embodiment of the present invention. The flying object 1 includes a bulb 11 that contains a gas lighter than air such as helium, a container 12 that is suspended from the bulb 11 and flies, and one end is connected to the bulb 11 and the other end is connected to the container 12. A hanging rope 13 which is a plurality of cords to which the portions are connected and the bulb 11 is provided for suspending the container 12 is provided.

図2は、容器12の構成を示した図である。容器12は、搭乗員H1等の収容物を収容する気密な中空の箱体である容器本体121と、容器本体121の内部の空間を小空間S1(第1の小空間の一例)と小空間S2(第2の小空間の一例)に仕切る仕切り板122を備える。 FIG. 2 is a diagram showing the configuration of the container 12. The container 12 has a container body 121 which is an airtight hollow box body for accommodating a crew member H1 and the like, and a small space S1 (an example of a first small space) and a small space inside the container body 121. A partition plate 122 for partitioning S2 (an example of a second small space) is provided.

小空間S1は、搭乗員H1等の収容物を収容する空間であり、搭乗員H1が快適に呼吸を行える濃度の酸素を含む空気が充填されている。 The small space S1 is a space for accommodating the contents such as the crew member H1 and is filled with air containing oxygen having a concentration that allows the crew member H1 to breathe comfortably.

仕切り板122の少なくとも一部は、光を透過する。図2の例では、仕切り板122のうち範囲Aの部分が、光を透過する素材(例えば、透明なポリカーボネートやアクリル樹脂等)で作られている。仕切り板122のうち範囲A以外の部分は、例えば、繊維強化プラスチック、繊維強化プラスチック以外のプラスチック、アルミ等の軽金属等で作られている。 At least a part of the partition plate 122 transmits light. In the example of FIG. 2, the portion of the partition plate 122 in the range A is made of a material that transmits light (for example, transparent polycarbonate or acrylic resin). The portion of the partition plate 122 other than the range A is made of, for example, a fiber reinforced plastic, a plastic other than the fiber reinforced plastic, a light metal such as aluminum, or the like.

また、容器本体121のうち、小空間S2を形成する部分の少なくとも一部は、光を透過する。図2の例では、容器本体121のうち範囲Bの部分が、光を透過する素材(例えば、透明なポリカーボネートやアクリル樹脂等)で作られている。容器本体121のうち範囲B以外の部分は、例えば、繊維強化プラスチック、繊維強化プラスチック以外のプラスチック、アルミ等の軽金属等で作られている。 Further, at least a part of the container body 121 that forms the small space S2 transmits light. In the example of FIG. 2, the portion of the container body 121 in the range B is made of a material that transmits light (for example, transparent polycarbonate or acrylic resin). The portion of the container body 121 other than the range B is made of, for example, fiber reinforced plastic, plastic other than fiber reinforced plastic, light metal such as aluminum, and the like.

上記のように、仕切り板122の範囲Aの部分及び容器本体121の範囲Bの部分が光を透過するため、小空間S1に収容される搭乗員H1は、小空間S1に容器12の外部から透過する光によって、容器12の外部を視認することができる。 As described above, since the portion A of the partition plate 122 and the portion B of the container body 121 transmit light, the crew member H1 accommodated in the small space S1 can enter the small space S1 from the outside of the container 12. The outside of the container 12 can be visually recognized by the transmitted light.

仕切り板122は、1以上の微細な孔Hを有する。孔Hは、小空間S1と小空間S2の間における緩やかな気体の出入りを生じさせる。孔Hは、小空間S1内の気体の温度と小空間S2内の気体の温度に差が生じた場合に、その温度差により生じた圧力差が短時間で解消するように小空間S1と小空間S2の間に気体の出入りを生じさせる。一方、孔Hは、小空間S1と小空間S2の間に気体の対流を生じさせるほどに大きくはない。従って、小空間S1内の気体の温度と小空間S2内の気体の温度の差が解消するには、数分乃至数十分程度の時間を要する。 The partition plate 122 has one or more fine holes H. The hole H causes a gentle gas inflow and outflow between the small space S1 and the small space S2. The hole H is small with the small space S1 so that when a difference occurs between the temperature of the gas in the small space S1 and the temperature of the gas in the small space S2, the pressure difference caused by the temperature difference is eliminated in a short time. Gas enters and exits between spaces S2. On the other hand, the hole H is not large enough to cause gas convection between the small space S1 and the small space S2. Therefore, it takes several minutes to several tens of minutes to eliminate the difference between the temperature of the gas in the small space S1 and the temperature of the gas in the small space S2.

一般的に、飛翔体1が飛翔により高度(地上からの高さ)を上げるに伴い、容器12の周囲の空気は希薄かつ低温となる。飛翔体1の飛翔により容器本体121が外部から急激に冷却された場合、容器本体121に内側から接触する気体内の水蒸気が容器本体121に冷却されて水となり、容器本体121の内側面に水滴として付着する、という現象、すなわち、容器本体121における結露が生じ易い。 Generally, as the flying object 1 rises in altitude (height from the ground) due to flight, the air around the container 12 becomes dilute and low in temperature. When the container body 121 is rapidly cooled from the outside by the flight of the flying object 1, the water vapor in the gas that comes into contact with the container body 121 from the inside is cooled by the container body 121 to become water, and water droplets are formed on the inner surface of the container body 121. That is, dew condensation is likely to occur in the container body 121.

しかしながら、小空間S1内の気体が接する容器本体121の面積に対する小空間S1内の気体の容積は、小空間S2内の気体が接する容器本体121の面積に対する小空間S2内の気体の容積より大きい。従って、小空間S1内の気体の温度が容器本体121により冷却される速度は、小空間S2内の気体の温度が容器本体121により冷却される速度より遅い。また、上述したように、小空間S1と小空間S2の間には対流による気体の出入りはほとんど生じない。 However, the volume of the gas in the small space S1 with respect to the area of the container body 121 in contact with the gas in the small space S1 is larger than the volume of the gas in the small space S2 with respect to the area of the container body 121 in contact with the gas in the small space S2. .. Therefore, the rate at which the temperature of the gas in the small space S1 is cooled by the container body 121 is slower than the rate at which the temperature of the gas in the small space S2 is cooled by the container body 121. Further, as described above, gas hardly flows in and out between the small space S1 and the small space S2 due to convection.

その結果、(小空間S1内の温度)>(小空間S2内の温度)>(容器本体121外の空間の温度)、という温度の関係が生じる。そのため、小空間S1と小空間S2の温度の差異、及び、小空間S2と容器本体121外の空間の温度の差異のいずれも、仮に仕切り板122がない場合に生じる容器本体121内の空間の温度と容器本体121外の空間の温度との差異よりも小さくなる。 As a result, there is a temperature relationship of (temperature in the small space S1)> (temperature in the small space S2)> (temperature in the space outside the container body 121). Therefore, both the temperature difference between the small space S1 and the small space S2 and the temperature difference between the small space S2 and the space outside the container body 121 are the differences in the temperature inside the container body 121 that occurs when the partition plate 122 is not present. It is smaller than the difference between the temperature and the temperature of the space outside the container body 121.

上記のような理由で、仮に仕切り板122がない場合に容器本体121において結露が発生する確率と比較し、本実施形態に係る容器12の仕切り板122において結露が発生する確率、及び、本実施形態に係る容器12の容器本体121のうち小空間S2を形成している部分において結露が発生する確率は低い。 For the above reasons, the probability that dew condensation will occur on the partition plate 122 of the container 12 according to the present embodiment, and the present implementation, as compared with the probability that dew condensation will occur on the container body 121 if there is no partition plate 122. There is a low probability that dew condensation will occur in the portion of the container body 121 of the container 12 according to the form that forms the small space S2.

なお、既述のように、小空間S1と小空間S2の間に生じる温度差の解消には長時間を要するが、小空間S1と小空間S2の間に生じる気圧差は速やかに解消する。従って、小空間S1と小空間S2の間に生じる気圧差により仕切り板122が強い力を受けて変形したり破損したりすることはない。 As described above, it takes a long time to eliminate the temperature difference between the small space S1 and the small space S2, but the pressure difference between the small space S1 and the small space S2 is quickly eliminated. Therefore, the partition plate 122 is not deformed or damaged by a strong force due to the pressure difference generated between the small space S1 and the small space S2.

以上のように、本実施形態に係る容器12によれば、少なくとも仕切り板122及び容器本体121のうち小空間S2を形成している部分において結露が発生しにくい。 As described above, according to the container 12 according to the present embodiment, dew condensation is unlikely to occur at least in the portion of the partition plate 122 and the container main body 121 that forms the small space S2.

[第2実施形態]
以下に、本発明の第2実施形態に係る容器12を説明する。第2実施形態に係る容器12は、第1実施形態に係る容器12と同様に、飛翔体1(図1参照)が備える容器であり、吊索13を介して球皮11に吊られて飛翔する。第2実施形態に係る容器12は第1実施形態に係る容器12と比較し、以下の点が異なっている。
(1)第2実施形態に係る容器12の仕切り板122は、第1実施形態に係る容器12の仕切り板122が有している孔Hを有しない。
(2)第2実施形態に係る容器12の容器本体121は、小空間S2を形成している部分に、第1実施形態に係る容器12の仕切り板122が有している孔Hと同様の孔Iを1以上、有している。
[Second Embodiment]
The container 12 according to the second embodiment of the present invention will be described below. Similar to the container 12 according to the first embodiment, the container 12 according to the second embodiment is a container included in the flying object 1 (see FIG. 1), and is suspended from the bulb 11 via the hanging rope 13 and flies. do. The container 12 according to the second embodiment is different from the container 12 according to the first embodiment in the following points.
(1) The partition plate 122 of the container 12 according to the second embodiment does not have the hole H that the partition plate 122 of the container 12 according to the first embodiment has.
(2) The container body 121 of the container 12 according to the second embodiment has the same hole H as the partition plate 122 of the container 12 according to the first embodiment in the portion forming the small space S2. It has one or more holes I.

図3は、本実施形態に係る容器12の構成を示した図である。 FIG. 3 is a diagram showing the configuration of the container 12 according to the present embodiment.

本実施形態に係る容器12においては、飛翔体1の飛翔の高度が上がるに伴い容器本体121の外部の空間における温度が急激に低下すると、小空間S2と容器本体121の外部の空間との間の圧力差は速やかに解消する一方、小空間S2と容器本体121の外部の空間との間の温度差の解消には時間を要する。その結果、第1実施形態に係る容器12における場合と同様に、(小空間S1内の温度)>(小空間S2内の温度)>(容器本体121外の空間の温度)、という温度の関係が生じる。 In the container 12 according to the present embodiment, when the temperature in the space outside the container body 121 suddenly drops as the flight altitude of the flying object 1 rises, between the small space S2 and the space outside the container body 121. While the pressure difference between the two is quickly eliminated, it takes time to eliminate the temperature difference between the small space S2 and the space outside the container body 121. As a result, as in the case of the container 12 according to the first embodiment, the temperature relationship of (temperature in the small space S1)> (temperature in the small space S2)> (temperature in the space outside the container body 121). Occurs.

その結果、第1実施形態において説明した理由と同様の理由で、仮に仕切り板122がない場合に容器本体121(孔Iを有さない)において結露が発生する確率と比較し、本実施形態に係る容器12の仕切り板122において結露が発生する確率、及び、本実施形態に係る容器12の容器本体121のうち小空間S2を形成している部分において結露が発生する確率は低い。 As a result, for the same reason as described in the first embodiment, the probability of dew condensation occurring in the container body 121 (without the hole I) when the partition plate 122 is not present is compared with the present embodiment. The probability that dew condensation will occur on the partition plate 122 of the container 12 and the probability that dew condensation will occur on the portion of the container body 121 of the container 12 according to the present embodiment that forms the small space S2 are low.

なお、既述のように、小空間S2と容器本体121の外部の空間の間に生じる温度差の解消には長時間を要するが、小空間S2と容器本体121の外部の空間の間に生じる気圧差は速やかに解消する。従って、小空間S2と容器本体121の外部の空間の間に生じる気圧差により容器本体121(小空間S2を形成する部分)が強い力を受けて変形したり破損したりすることはない。 As described above, it takes a long time to eliminate the temperature difference generated between the small space S2 and the space outside the container body 121, but it occurs between the small space S2 and the space outside the container body 121. The pressure difference disappears quickly. Therefore, the container body 121 (the portion forming the small space S2) is not deformed or damaged by the pressure difference generated between the small space S2 and the space outside the container body 121.

以上のように、本実施形態に係る容器12による場合も、少なくとも仕切り板122及び容器本体121のうち小空間S2を形成している部分において結露が発生しにくい。 As described above, even in the case of the container 12 according to the present embodiment, dew condensation is unlikely to occur at least in the portion of the partition plate 122 and the container main body 121 that forms the small space S2.

[第3実施形態]
以下に、本発明の第3実施形態に係る容器22を説明する。第3実施形態に係る容器22は、第1実施形態に係る容器12と同様に、飛翔体1(図1参照)が備える容器であり、吊索13を介して球皮11に吊られて飛翔する。
[Third Embodiment]
The container 22 according to the third embodiment of the present invention will be described below. Similar to the container 12 according to the first embodiment, the container 22 according to the third embodiment is a container included in the flying object 1 (see FIG. 1), and is suspended from the bulb 11 via the hanging rope 13 and flies. do.

図4は、容器22の構成を示した図である。容器22は、搭乗員H1を含む収容物を収容する第1容器本体221(第1の容器本体の一例)と、第1容器本体221を収容する気密な第2容器本体222(第2の容器本体の一例)と、第1容器本体221と第2容器本体222の間の空間の一部に充填された断熱材223を備える。なお、容器22は、断熱材223を備えなくてもよい。 FIG. 4 is a diagram showing the configuration of the container 22. The container 22 has a first container main body 221 (an example of a first container main body) for accommodating an inclusion including a crew member H1 and an airtight second container main body 222 (a second container) for accommodating the first container main body 221. An example of the main body) and a heat insulating material 223 filled in a part of the space between the first container main body 221 and the second container main body 222 are provided. The container 22 does not have to be provided with the heat insulating material 223.

以下、第1容器本体221の内部の空間を小空間S3と呼び、第1容器本体221と第2容器本体222の間の区間を小空間S4と呼ぶ。 Hereinafter, the space inside the first container main body 221 is referred to as a small space S3, and the section between the first container main body 221 and the second container main body 222 is referred to as a small space S4.

小空間S3及び小空間S4には、搭乗員H1が快適に呼吸を行える濃度の酸素を含む空気が充填されている。 The small space S3 and the small space S4 are filled with air containing oxygen having a concentration that allows the crew member H1 to breathe comfortably.

第1容器本体221の少なくとも一部は、光を透過する。図4の例では、第1容器本体221のうち範囲Cの部分が、光を透過する素材(例えば、透明なポリカーボネートやアクリル樹脂等)で作られている。第1容器本体221のうち範囲C以外の部分は、例えば、繊維強化プラスチック、繊維強化プラスチック以外のプラスチック、アルミ等の軽金属等で作られている。 At least a part of the first container body 221 transmits light. In the example of FIG. 4, the portion of the first container main body 221 in the range C is made of a material that transmits light (for example, transparent polycarbonate or acrylic resin). The portion of the first container main body 221 other than the range C is made of, for example, fiber reinforced plastic, plastic other than fiber reinforced plastic, light metal such as aluminum, and the like.

また、第2容器本体222の少なくとも一部は、光を透過する。図4の例では、第2容器本体222のうち範囲Dの部分が、光を透過する素材(例えば、透明なポリカーボネートやアクリル樹脂等)で作られている。第2容器本体222のうち範囲D以外の部分は、例えば、繊維強化プラスチック、繊維強化プラスチック以外のプラスチック、アルミ等の軽金属等で作られている。 Further, at least a part of the second container main body 222 transmits light. In the example of FIG. 4, the portion of the second container main body 222 in the range D is made of a material that transmits light (for example, transparent polycarbonate or acrylic resin). The portion of the second container main body 222 other than the range D is made of, for example, a fiber reinforced plastic, a plastic other than the fiber reinforced plastic, a light metal such as aluminum, or the like.

上記のように、第1容器本体221の範囲Cの部分及び第2容器本体222の範囲Dの部分が光を透過するため、第1容器本体221に収容される搭乗員H1は、第1容器本体221の内部の空間に第2容器本体222の外部から透過する光によって、容器22の外部を視認することができる。 As described above, since the portion of the range C of the first container main body 221 and the portion of the range D of the second container main body 222 transmit light, the crew member H1 housed in the first container main body 221 is the first container. The outside of the container 22 can be visually recognized by the light transmitted from the outside of the second container main body 222 into the space inside the main body 221.

第1容器本体221は、1以上の微細な孔Jを有する。孔Jは、小空間S3と、第1容器本体221と小空間S4との間における緩やかな気体の出入りを生じさせる。孔Jは、小空間S3内の気体の温度と小空間S4内の気体の温度に差が生じた場合に、その温度差により生じた圧力差が短時間で解消するように、小空間S3と小空間S4の間に気体の出入りを生じさせる。一方、孔Jは、小空間S3と小空間S4の間に気体の対流を生じさせるほどに大きくはない。従って、小空間S3内の気体の温度と小空間S4内の気体の温度の差が解消するには、数分乃至数十分程度の時間を要する。 The first container body 221 has one or more fine holes J. The hole J causes a gentle gas in and out between the small space S3 and the first container main body 221 and the small space S4. The hole J is provided with the small space S3 so that when a difference occurs between the temperature of the gas in the small space S3 and the temperature of the gas in the small space S4, the pressure difference caused by the temperature difference is eliminated in a short time. Gas enters and exits between the small spaces S4. On the other hand, the hole J is not large enough to cause gas convection between the small space S3 and the small space S4. Therefore, it takes several minutes to several tens of minutes to eliminate the difference between the temperature of the gas in the small space S3 and the temperature of the gas in the small space S4.

そのため、飛翔体1の飛翔の高度が上がり、容器22が外部から冷却される場合、(小空間S3内の温度)>(小空間S4内の温度)>(第2容器本体222外の空間の温度)、という温度の関係が生じる。そのため、小空間S3と小空間S4の温度の差異、及び、小空間S4と第2容器本体222外の空間の温度の差異のいずれも、仮に第1容器本体221がない場合に生じる第2容器本体222内の空間の温度と第2容器本体222外の空間の温度との差異よりも小さくなる。 Therefore, when the flight altitude of the flying object 1 rises and the container 22 is cooled from the outside, (temperature in the small space S3)> (temperature in the small space S4)> (in the space outside the second container body 222). Temperature), the relationship of temperature arises. Therefore, both the difference in temperature between the small space S3 and the small space S4 and the difference in the temperature between the small space S4 and the space outside the second container main body 222 occur when the first container main body 221 is absent. It is smaller than the difference between the temperature of the space inside the main body 222 and the temperature of the space outside the second container main body 222.

上記のような理由で、仮に第1容器本体221がない場合に第2容器本体222において結露が発生する確率と比較し、本実施形態に係る容器22の第1容器本体221において結露が発生する確率、及び、本実施形態に係る容器22の第2容器本体222において結露が発生する確率は低い。 For the above reasons, dew condensation occurs in the first container body 221 of the container 22 according to the present embodiment, as compared with the probability that dew condensation occurs in the second container body 222 if the first container body 221 is not present. The probability and the probability that dew condensation will occur in the second container main body 222 of the container 22 according to the present embodiment are low.

なお、既述のように、小空間S3と小空間S4の間に生じる温度差の解消には長時間を要するが、小空間S3と小空間S4の間に生じる気圧差は速やかに解消する。従って、小空間S3と小空間S4の間に生じる気圧差により第1容器本体221が強い力を受けて変形したり破損したりすることはない。 As described above, it takes a long time to eliminate the temperature difference between the small space S3 and the small space S4, but the atmospheric pressure difference between the small space S3 and the small space S4 is quickly eliminated. Therefore, the first container main body 221 is not deformed or damaged by a strong force due to the pressure difference generated between the small space S3 and the small space S4.

以上のように、本実施形態に係る容器22によれば、第1容器本体221及び第2容器本体222において結露が発生しにくい。 As described above, according to the container 22 according to the present embodiment, dew condensation is unlikely to occur in the first container main body 221 and the second container main body 222.

[第4実施形態]
以下に、本発明の第4実施形態に係る容器22を説明する。第4実施形態に係る容器22は、第1実施形態に係る容器12と同様に、飛翔体1(図1参照)が備える容器であり、吊索13を介して球皮11に吊られて飛翔する。第4実施形態に係る容器22は第3実施形態に係る容器22と比較し、以下の点が異なっている。
(1)第4実施形態に係る容器22の第1容器本体221は、第3実施形態に係る容器22の第1容器本体221が有している孔Jを有しない。
(2)第4実施形態に係る容器22の第2容器本体222は、第3実施形態に係る容器22の第1容器本体221が有している孔Jと同様の孔Kを1以上、有している。
(3)第4実施形態に係る小空間S4には、搭乗員H1が快適に呼吸を行える濃度の酸素を含む空気は充填されていない。
[Fourth Embodiment]
Hereinafter, the container 22 according to the fourth embodiment of the present invention will be described. The container 22 according to the fourth embodiment is a container included in the flying object 1 (see FIG. 1) like the container 12 according to the first embodiment, and is suspended from the bulb 11 via the hanging rope 13 and flies. do. The container 22 according to the fourth embodiment is different from the container 22 according to the third embodiment in the following points.
(1) The first container main body 221 of the container 22 according to the fourth embodiment does not have the hole J that the first container main body 221 of the container 22 according to the third embodiment has.
(2) The second container body 222 of the container 22 according to the fourth embodiment has one or more holes K similar to the holes J possessed by the first container body 221 of the container 22 according to the third embodiment. are doing.
(3) The small space S4 according to the fourth embodiment is not filled with air containing oxygen having a concentration at which the crew member H1 can comfortably breathe.

図5は、本実施形態に係る容器22の構成を示した図である。 FIG. 5 is a diagram showing the configuration of the container 22 according to the present embodiment.

本実施形態に係る容器22においては、飛翔体1の飛翔の高度が上がるに伴い第2容器本体222の外部の空間における温度が急激に低下すると、小空間S4と第2容器本体222の外部の空間との間の圧力差は速やかに解消する一方、小空間S4と第2容器本体222の外部の空間との間の温度差の解消には時間を要する。その結果、第3実施形態に係る容器22における場合と同様に、(小空間S3内の温度)>(小空間S4内の温度)>(第2容器本体222外の空間の温度)、という温度の関係が生じる。 In the container 22 according to the present embodiment, when the temperature in the space outside the second container body 222 sharply drops as the flight altitude of the flying object 1 rises, the outside of the small space S4 and the second container body 222 While the pressure difference between the space and the space is quickly eliminated, it takes time to eliminate the temperature difference between the small space S4 and the space outside the second container body 222. As a result, as in the case of the container 22 according to the third embodiment, the temperature (temperature in the small space S3)> (temperature in the small space S4)> (temperature in the space outside the second container main body 222). Relationship arises.

その結果、第3実施形態において説明した理由と同様の理由で、仮に第1容器本体221がない場合に第2容器本体222(孔Kを有さない)において結露が発生する確率と比較し、本実施形態に係る容器22の第1容器本体221において結露が発生する確率、及び、本実施形態に係る容器22の第2容器本体222において結露が発生する確率は低い。 As a result, for the same reason as described in the third embodiment, it is compared with the probability that dew condensation occurs in the second container body 222 (without the hole K) if the first container body 221 is not present. The probability that dew condensation will occur in the first container main body 221 of the container 22 according to the present embodiment and the probability that dew condensation will occur in the second container main body 222 of the container 22 according to the present embodiment are low.

なお、既述のように、小空間S4と第2容器本体222の外部の空間の間に生じる温度差の解消には長時間を要するが、小空間S4と第2容器本体222の外部の空間の間に生じる気圧差は速やかに解消する。従って、小空間S4と第2容器本体222の外部の空間の間に生じる気圧差により第2容器本体222が強い力を受けて変形したり破損したりすることはない。 As described above, it takes a long time to eliminate the temperature difference generated between the small space S4 and the space outside the second container body 222, but the space outside the small space S4 and the second container body 222. The pressure difference that occurs between the two is quickly eliminated. Therefore, the second container body 222 is not deformed or damaged by a strong force due to the pressure difference generated between the small space S4 and the space outside the second container body 222.

以上のように、本実施形態に係る容器22による場合も、第1容器本体221及び第2容器本体222において結露が発生しにくい。 As described above, even in the case of the container 22 according to the present embodiment, dew condensation is unlikely to occur in the first container main body 221 and the second container main body 222.

[変形例]
上述した実施形態に係る飛翔体1は、本発明の技術的思想の範囲内において様々に変形されてよい。以下にそれらの変形の例を示す。なお、以下の変形例の2以上が適宜、組み合わされてもよい。
[Modification example]
The flying object 1 according to the above-described embodiment may be variously modified within the scope of the technical idea of the present invention. An example of these variations is shown below. In addition, two or more of the following modified examples may be combined as appropriate.

(1)上述した第1実施形態又は第2実施形態における容器本体121、又は、上述した第3実施形態又は第4実施形態における第1容器本体221(又は第2容器本体222)は、人を収容するキャビンであるが、それらの容器本体の収容物は人でなくてもよい。図6は、例として、第1実施形態に係る容器12の容器本体121が撮影装置H2を収容する場合を例示した図である。 (1) The container body 121 in the above-mentioned first embodiment or the second embodiment, or the first container body 221 (or the second container body 222) in the above-mentioned third embodiment or the fourth embodiment is a person. Although it is a cabin to be housed, the container body of those containers does not have to be a person. FIG. 6 is a diagram illustrating, as an example, a case where the container body 121 of the container 12 according to the first embodiment accommodates the photographing apparatus H2.

(2)上述した実施形態において、飛翔体はガス気球であるものとしたが、飛翔体の種類はガス気球に限られず、熱気球や飛行船等の他の種類の飛行体であってもよい。 (2) In the above-described embodiment, the flying object is a gas balloon, but the type of the flying object is not limited to the gas balloon, and may be another type of flying object such as a hot air balloon or an airship.

1…飛翔体、11…球皮、12…容器、13…吊索、22…容器、121…容器本体、122…仕切り板、221…第1容器本体、222…第2容器本体、223…断熱材。 1 ... flying object, 11 ... bulb, 12 ... container, 13 ... hanging rope, 22 ... container, 121 ... container body, 122 ... partition plate, 221 ... first container body, 222 ... second container body, 223 ... heat insulating Material.

Claims (7)

飛翔体が備える容器であって、
器本体と、
前記容器本体の内部の空間を、収容物を収容する第1の小空間と、前記第1の小空間とは異なる第2の小空間に仕切る仕切り板と
を備え、
前記仕切り板は、前記第1の小空間と前記第2の小空間の間に生じた圧力差を解消するように前記第1の小空間と前記第2の小空間の間に気体の出入りを生じさせるが、前記第1の小空間と前記第2の小空間の間に気体の対流を生じさせない大きさの1以上の孔を有し、
前記第1の小空間内の気体が接する前記容器本体の面積に対する前記第1の小空間内の気体の容積は、前記第2の小空間内の気体が接する前記容器本体の面積に対する前記第2の小空間内の気体の容積より大きい
容器。
It is a container that the flying object has.
With the container body
A partition plate for partitioning the space inside the container body into a first small space for accommodating an object and a second small space different from the first small space is provided.
The partition plate allows gas to enter and exit between the first small space and the second small space so as to eliminate the pressure difference generated between the first small space and the second small space. It has one or more holes of a size that does not cause gas convection between the first small space and the second small space .
The volume of the gas in the first small space with respect to the area of the container body in contact with the gas in the first small space is the second with respect to the area of the container body in contact with the gas in the second small space. Larger than the volume of gas in the small space of
container.
飛翔体が備える容器であって、
器本体と、
前記容器本体の内部の空間を、収容物を収容する第1の小空間と、前記第1の小空間とは異なる第2の小空間に仕切る仕切り板と
を備え、
前記容器本体の前記第2の小空間を形成している部分、前記第2の小空間と前記容器本体の外部の空間の間に生じた圧力差を解消するように前記第2の小空間と前記容器本体の外部の空間の間に気体の出入りを生じさせるが、前記第2の小空間と前記容器本体の外部の空間の間に気体の対流を生じさせない大きさの1以上の孔を有する
容器。
It is a container that the flying object has.
With the container body
A partition plate for partitioning the space inside the container body into a first small space for accommodating an object and a second small space different from the first small space is provided.
The portion of the container body forming the second small space is the second small space so as to eliminate the pressure difference generated between the second small space and the space outside the container body. And one or more holes of a size that causes gas to flow in and out between the space outside the container body, but does not cause gas convection between the second small space and the space outside the container body. Container to have.
前記第1の小空間に前記容器本体の外部から光が透過するように、前記容器本体の少なくとも一部と前記仕切り板の少なくとも一部が光を透過する
請求項1又は2に記載の容器。
The container according to claim 1 or 2, wherein at least a part of the container body and at least a part of the partition plate transmit light so that light is transmitted from the outside of the container body to the first small space.
飛翔体が備える容器であって、
収容物を収容する第1の容器本体と、
前記第1の容器本体を収容する第2の容器本体と
を備え、
前記第1の容器本体の内部の空間を第1の小空間とし、前記第1の容器本体と前記第2の容器本体の間の空間を第2の小空間とするとき、
前記第1の容器本体は、前記第1の小空間と前記第2の小空間の間に生じた圧力差を解消するように前記第1の小空間と前記第2の小空間の間に気体の出入りを生じさせるが、前記第1の小空間と前記第2の小空間の間に気体の対流を生じさせない大きさの1以上の孔を有する
容器。
It is a container that the flying object has.
The first container body that houses the contents and
A second container body for accommodating the first container body is provided.
When the space inside the first container body is defined as the first small space and the space between the first container body and the second container body is defined as the second small space.
The first container body is a gas between the first small space and the second small space so as to eliminate the pressure difference generated between the first small space and the second small space. A container having one or more holes having a size that causes gas to flow in and out, but does not cause gas convection between the first small space and the second small space .
飛翔体が備える容器であって、
収容物を収容する第1の容器本体と、
前記第1の容器本体を収容する第2の容器本体と
を備え、
前記第1の容器本体と前記第2の容器本体の間の空間を小空間とするとき、
前記第2の容器本体は、前記小空間と前記第2の容器本体の外部の空間の間に生じた圧力差を解消するように前記小空間と前記第2の容器本体の外部の空間の間に気体の出入りを生じさせるが、前記小空間と前記第2の容器本体の外部の空間の間に気体の対流を生じさせない大きさの1以上の孔を有する
容器。
It is a container that the flying object has.
The first container body that houses the contents and
A second container body for accommodating the first container body is provided.
When the space between the first container body and the second container body is a small space,
The second container body is between the small space and the space outside the second container body so as to eliminate the pressure difference generated between the small space and the space outside the second container body. A container having one or more holes having a size that causes gas to flow in and out, but does not cause gas convection between the small space and the space outside the second container body .
前記第1の容器本体の内部の空間に前記第2の容器本体の外部から光が透過するように、前記第1の容器本体の少なくとも一部と前記第2の容器本体の少なくとも一部が光を透過する
請求項4又は5に記載の容器。
At least a part of the first container body and at least a part of the second container body are illuminated so that light is transmitted from the outside of the second container body to the space inside the first container body. The container according to claim 4 or 5.
前記収容物は人を含む
請求項1乃至6のいずれか1項に記載の容器。
The container according to any one of claims 1 to 6, wherein the contained item includes a person.
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