JPH042595A - Anti-icing device - Google Patents
Anti-icing deviceInfo
- Publication number
- JPH042595A JPH042595A JP9923890A JP9923890A JPH042595A JP H042595 A JPH042595 A JP H042595A JP 9923890 A JP9923890 A JP 9923890A JP 9923890 A JP9923890 A JP 9923890A JP H042595 A JPH042595 A JP H042595A
- Authority
- JP
- Japan
- Prior art keywords
- face
- icing
- heat pipe
- temperature
- heated air
- 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
- 238000010438 heat treatment Methods 0.000 claims abstract description 10
- 230000002265 prevention Effects 0.000 claims description 3
- 239000012530 fluid Substances 0.000 abstract description 2
- 239000002184 metal Substances 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000004078 waterproofing Methods 0.000 description 2
- 238000007664 blowing Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Landscapes
- Road Paving Structures (AREA)
Abstract
Description
【発明の詳細な説明】
（産業上の利用分野）
本発明は航空機、自動車、船舶、建築物等の着氷防止装
置に関する。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to an anti-icing device for aircraft, automobiles, ships, buildings, etc.
（従来の技術）
従来の着氷防止装置の１例が第４図及び第５図に示され
ている。(Prior Art) An example of a conventional icing prevention device is shown in FIGS. 4 and 5.
外板１とこれに固着された桁２とによって限界される腔
所３の内部にマニホールド４が内臓され、このマニホー
ルド４はそのサポート５を桁２にリベット６によって締
結することによって固定されている。このマニホールド
４の１端はダクト７を介して加熱空気源８に連結され、
このダクト７に介装されたシャフトオフバルブ９はスイ
ッチ１０を操作することによって開閉される。A manifold 4 is housed inside a cavity 3 bounded by the outer plate 1 and a spar 2 fixed thereto, and this manifold 4 is fixed by fastening its support 5 to the spar 2 with rivets 6. . One end of this manifold 4 is connected to a heated air source 8 via a duct 7,
A shaft off valve 9 installed in the duct 7 is opened and closed by operating a switch 10.
しかして、外板１の外面、即ち、防氷面１ａに氷が付着
するおそれがあるときは、スイッチ１０を操作してシャ
フトオフバルブ９を開とする。すると、加熱空気源８内
の加熱空気がダクト７及びシャットオフバルブ９を通っ
てマニホールド４内に入り、このマニホールド４に穿設
された多数のノズル１１から外板１の内面に噴射されて
この外板１を加熱する。Therefore, when there is a possibility that ice may adhere to the outer surface of the outer panel 1, that is, the anti-icing surface 1a, the shaft off valve 9 is opened by operating the switch 10. Then, the heated air in the heated air source 8 enters the manifold 4 through the duct 7 and the shut-off valve 9, and is injected onto the inner surface of the outer panel 1 from the many nozzles 11 provided in the manifold 4. Heat the outer panel 1.
外板１を加熱することによって陣温した空気は桁２に穿
設された多数の排気ボー目２を経て腔所３の外部に排出
される。The air heated by heating the outer panel 1 is discharged to the outside of the cavity 3 through a large number of exhaust holes 2 formed in the girder 2.
（発明が解決しようとする課題）
上記従来の装置においては、防表面１ａに氷が均一に付
着しないのにも拘らず防氷面１ａの全面をこれに付着し
た氷を融解又は蒸発させるのに十分な温度、即ち、氷点
以上に加熱していたため、多量の加熱エネルギを要し、
また、着氷の少ない所では防氷面１ａが必要以上に高温
となると言う問題があった・
これに対処するため、着氷の分布に合致するように防氷
面１ａを加熱しようとすると装置が複雑、かつ、高価と
なるという不具合があった。(Problems to be Solved by the Invention) In the above-mentioned conventional device, although the ice does not adhere uniformly to the anti-icing surface 1a, it is difficult to melt or evaporate the ice adhering to the entire surface of the anti-icing surface 1a. Because it was heated to a sufficient temperature, that is, above the freezing point, a large amount of heating energy was required.
In addition, there was a problem in that the anti-icing surface 1a would reach a higher temperature than necessary in areas with little icing.To deal with this, the device The problem was that it was complicated and expensive.
（課題を解決するための手段）
本発明は上記課題を解決するために発明されたものであ
って、その要旨とするところは、 防氷面の内側にその
全面に亘る面状のヒートパイプを配設し、このヒートパ
イプの内面を加熱する手段を設けたことを特徴とする着
氷防止装置にある。(Means for Solving the Problems) The present invention was invented to solve the above problems, and its gist is to provide a planar heat pipe that extends over the entire surface inside the anti-icing surface. The icing prevention device is characterized in that it is provided with a means for heating the inner surface of the heat pipe.
（作用）
本発明においては、上記構成を具えているため、防氷面
の熱負荷が不均一となっても防氷面は面状のヒートパイ
プによって加熱されるため防氷面の温度分布が均一化さ
れる。(Function) Since the present invention has the above configuration, even if the heat load on the anti-icing surface is uneven, the anti-icing surface is heated by the planar heat pipe, so the temperature distribution on the anti-icing surface is maintained. Equalized.
（実施例）
本発明の１実施例が第１図ないし第３図に示されている
。Embodiment One embodiment of the invention is shown in FIGS. 1-3.
外板１の内面にはその全面に亘る面状のヒートパイプ２
０が張設されている。このヒートパイプ２０の内部には
、第２図に示すように、多孔質金属２１と金網ウィフク
２２が内臓されるとともに作動流体が封入されている。A planar heat pipe 2 is provided on the inner surface of the outer panel 1 over the entire surface.
0 is set. As shown in FIG. 2, inside the heat pipe 20, a porous metal 21 and a wire mesh wire 22 are built in, and a working fluid is sealed therein.
外板１の外面、即ち、防氷面１ａには、第３図に示すよ
うに、温度センサ２３が取り付けられ、この温度センサ
２３の出力はコントローラ２４に入力される。そして、
このコントローラ２４からの指令によってダクト７に介
装された流量制御弁２５の開度が制御されるようになっ
ている。As shown in FIG. 3, a temperature sensor 23 is attached to the outer surface of the outer panel 1, that is, the anti-icing surface 1a, and the output of this temperature sensor 23 is input to a controller 24. and,
The opening degree of a flow control valve 25 installed in the duct 7 is controlled by a command from the controller 24.
他の構成は第４図及び第５図に示す従来のものと同様で
あり対応する部材には同し符号が付されている。The rest of the structure is similar to the conventional one shown in FIGS. 4 and 5, and corresponding members are given the same reference numerals.
しかして、温度センサ２３によって検出された防氷面１
ａの温度が所定値例えば２℃以下に低下すると、コント
ローラ２４からの指令によって流量制御弁２５が開とさ
れ、加熱空気源ｓ内の加熱空気がダクト７及び流量制御
弁２５を経てマニホールド４内に入り、ノズル１１から
面状のヒートパイプ２０の内面に噴射される。Therefore, the anti-icing surface 1 detected by the temperature sensor 23
When the temperature of a drops to a predetermined value, for example, 2° C. or less, the flow control valve 25 is opened by a command from the controller 24, and the heated air in the heated air source s passes through the duct 7 and the flow control valve 25 into the manifold 4. The heat enters and is injected from the nozzle 11 onto the inner surface of the planar heat pipe 20.
ヒートパイプ２０の内面が加熱されると、この熱はヒー
トパイプ２０内に封入された作動媒体を介してヒートパ
イプ２０の外面に伝達され、次いで、外４５．１内を通
ってその外面、即ち、防氷面１ａに伝達され、これを加
熱する。ヒートパイプ２０を加熱することによって降温
した空気は排気ボー目２を経て腔所３の外部に排出され
る。When the inner surface of the heat pipe 20 is heated, this heat is transferred to the outer surface of the heat pipe 20 via the working medium enclosed within the heat pipe 20 and then through the outer surface 45.1 to its outer surface, i.e. , is transmitted to the anti-icing surface 1a and heats it. The air whose temperature has been lowered by heating the heat pipe 20 is discharged to the outside of the cavity 3 through the exhaust hole 2.
防氷面１ａの温度は温度センサ２３によって常時検出さ
れ、この温度に応じて流量制御弁２５の開度を自動的に
制御することにより防氷面１ａの温度を常時一定の温度
例えば２℃に維持できる。The temperature of the anti-icing surface 1a is constantly detected by the temperature sensor 23, and by automatically controlling the opening degree of the flow rate control valve 25 according to this temperature, the temperature of the anti-icing surface 1a is always kept at a constant temperature, for example, 2°C. Can be maintained.
防氷面１ａ上に氷が不均一に付着した場合等、防氷面１
ａの熱負荷が不均一になった場合であっても、面状のヒ
ートパイプ２０は熱負荷の少ない個所の熱を熱負荷の大
きい個所に移送するので、防氷面１ａの全てを防水でき
るともに防氷面１ａの温度が防水に必要にして充分な最
低の温度となるように加熱空気を供給すれば良いので、
エネルギの浪費を防止できる。When ice adheres unevenly on anti-icing surface 1a,
Even if the heat load on surface a becomes uneven, the planar heat pipe 20 transfers the heat from areas with low heat load to areas with high heat load, so that the entire anti-icing surface 1a can be waterproofed. It is only necessary to supply heated air so that the temperature of the anti-icing surface 1a reaches the minimum temperature necessary and sufficient for waterproofing.
Energy waste can be prevented.
上記実施例においては、外板１の内面に面状のヒートパ
イプ２０を取り付けたが、面状のヒートパイプ２０の外
面を防氷面１ａとすることもできる。In the above embodiment, the planar heat pipe 20 is attached to the inner surface of the outer panel 1, but the outer surface of the planar heat pipe 20 can also be used as the anti-icing surface 1a.
また、上記実施例においては、ヒートパイプ２０の内面
に加熱空気を吹き付けることによって加熱しているが、
電気ヒータ等によって加熱することもできる。Furthermore, in the above embodiment, heating is performed by blowing heated air onto the inner surface of the heat pipe 20.
Heating can also be done with an electric heater or the like.
更に、防氷面１ａが小さい場合や、防氷面ｌａ上の熱負
荷の分布が比較的均一である場合には、温度本発明にお
いては、防氷面の内側にその全面ムこ亘る面状のビート
パイプを配設し、このヒートパイプの内面を加熱する手
段を設けたため、防氷面の熱負荷が不均一となってもこ
れを面状のヒートパイプによって加熱することによって
防氷面の温度分布を均一化することができる。Furthermore, when the anti-icing surface 1a is small or when the distribution of heat load on the anti-icing surface la is relatively uniform, the present invention can reduce the temperature inside the anti-icing surface over its entire surface. Since the heat pipe is equipped with a beat pipe and a means for heating the inner surface of the heat pipe, even if the heat load on the anti-icing surface is uneven, the heat load on the anti-icing surface can be heated by the planar heat pipe. Temperature distribution can be made uniform.
この結果、防氷面に局部的加熱不足部分や局部的高温部
分の発生を防止して防氷面の全面を確実に防水できると
ともにエネルギの浪費を防止できる。As a result, it is possible to prevent the occurrence of locally underheated areas or locally high temperature areas on the anti-icing surface, thereby making it possible to reliably waterproof the entire surface of the anti-icing surface and to prevent wastage of energy.
第１図ないし第３図は本発明の１実施例を示し、第１図
は縦断面図、第２図は第１図のｎ −ｎ線に沿う断面図
、第３図は略示的系統図である。第４図及び第５図は従
来の防水装置の１例を示し、第４図は縦断面図、第５図
は略示的系統図である。
防氷面一４ａ、ヒートパイプ−２０、加熱手段−８、第
４図1 to 3 show one embodiment of the present invention, FIG. 1 is a longitudinal sectional view, FIG. 2 is a sectional view taken along line n-n in FIG. 1, and FIG. 3 is a schematic system diagram. It is a diagram. FIGS. 4 and 5 show an example of a conventional waterproofing device, with FIG. 4 being a longitudinal sectional view and FIG. 5 being a schematic system diagram. Anti-icing surface 4a, heat pipe 20, heating means 8, Fig. 4
Claims (1)
設し、このヒートパイプの内面を加熱する手段を設けた
ことを特徴とする着氷防止装置。An icing prevention device comprising: a planar heat pipe that extends over the entire surface of an anti-icing surface; and means for heating the inner surface of the heat pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9923890A JPH042595A (en) | 1990-04-17 | 1990-04-17 | Anti-icing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9923890A JPH042595A (en) | 1990-04-17 | 1990-04-17 | Anti-icing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH042595A true JPH042595A (en) | 1992-01-07 |
Family
ID=14242112
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9923890A Pending JPH042595A (en) | 1990-04-17 | 1990-04-17 | Anti-icing device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH042595A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2470043A (en) * | 2009-05-06 | 2010-11-10 | Gkn Aerospace Services Ltd | Heating an aerodynamic component of an aircraft |
| CN101962076A (en) * | 2010-09-15 | 2011-02-02 | 北京航空航天大学 | Gas film ice prevention structure of leading edge of nacelle of airplane |
| WO2011111405A1 (en) * | 2010-03-08 | 2011-09-15 | 三菱重工業株式会社 | Deicing device for leading edge of wing of aircraft, and aircraft main wing |
| KR20160071840A (en) * | 2014-12-12 | 2016-06-22 | 한국항공우주산업 주식회사 | Apparatus for testing a helicopter in the freezing environment |
| EP3640139A1 (en) * | 2018-10-19 | 2020-04-22 | Airbus Operations (S.A.S.) | Aircraft engine nacelle equipped with an ice protection system |
-
1990
- 1990-04-17 JP JP9923890A patent/JPH042595A/en active Pending
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2470043A (en) * | 2009-05-06 | 2010-11-10 | Gkn Aerospace Services Ltd | Heating an aerodynamic component of an aircraft |
| GB2470043B (en) * | 2009-05-06 | 2011-06-08 | Gkn Aerospace Services Ltd | Heating system |
| WO2011111405A1 (en) * | 2010-03-08 | 2011-09-15 | 三菱重工業株式会社 | Deicing device for leading edge of wing of aircraft, and aircraft main wing |
| JP2011183922A (en) * | 2010-03-08 | 2011-09-22 | Mitsubishi Heavy Ind Ltd | Anti-icing and deicing device at wing leading edge part in aircraft and main wing of aircraft |
| CN101962076A (en) * | 2010-09-15 | 2011-02-02 | 北京航空航天大学 | Gas film ice prevention structure of leading edge of nacelle of airplane |
| KR20160071840A (en) * | 2014-12-12 | 2016-06-22 | 한국항공우주산업 주식회사 | Apparatus for testing a helicopter in the freezing environment |
| EP3640139A1 (en) * | 2018-10-19 | 2020-04-22 | Airbus Operations (S.A.S.) | Aircraft engine nacelle equipped with an ice protection system |
| FR3087420A1 (en) * | 2018-10-19 | 2020-04-24 | Airbus Operations (S.A.S.) | AIRCRAFT ENGINE CARRIER INCLUDING A FROST PROTECTION SYSTEM. |
| US11518526B2 (en) | 2018-10-19 | 2022-12-06 | Airbus Operations Sas | Aircraft engine nacelle comprising an anti-icing protection system |
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