JPH01278900A - Deicer - Google Patents
DeicerInfo
- Publication number
- JPH01278900A JPH01278900A JP10784688A JP10784688A JPH01278900A JP H01278900 A JPH01278900 A JP H01278900A JP 10784688 A JP10784688 A JP 10784688A JP 10784688 A JP10784688 A JP 10784688A JP H01278900 A JPH01278900 A JP H01278900A
- Authority
- JP
- Japan
- Prior art keywords
- icing
- plate
- piezoelectric element
- ice
- prevention device
- 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.)
- Granted
Links
- 230000002265 prevention Effects 0.000 claims description 16
- 238000010586 diagram Methods 0.000 description 3
Landscapes
- Materials Applied To Surfaces To Minimize Adherence Of Mist Or Water (AREA)
- General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)
Abstract
Description
【発明の詳細な説明】
A1発明の目的
(]) 産業上の利用分野
本発明は板体の表面に氷が付着するのを防止する着氷防
止装置に関し、特に、航空機、自動車等の外板表面の着
氷を防止するのに適した着氷防止装置に関する。Detailed Description of the Invention A1 Object of the Invention (]) Industrial Field of Application The present invention relates to an icing prevention device that prevents ice from adhering to the surface of a plate, particularly for the outer panels of aircraft, automobiles, etc. The present invention relates to an icing prevention device suitable for preventing icing on surfaces.
(2)従来の技術
航空機等は周囲の環境によりその外表面に氷が付着する
ことがある。たとえば航空機で氷が付着し易い箇所は、
第3図に示すように、胴体の前部Aまたは翼前縁B等の
機体表面の前側部分である。(2) Conventional Technology Ice may adhere to the outer surface of aircraft etc. depending on the surrounding environment. For example, the areas where ice tends to accumulate on airplanes are
As shown in FIG. 3, this is the front part of the fuselage surface such as the front part A of the fuselage or the leading edge B of the wing.
このような機体表面への着氷は機体の重量増加、空気抵
抗の増大等を引き起こし、特に翼前縁の着氷は揚力が不
安定となるので危険である。Icing on the surface of the aircraft causes an increase in the weight of the aircraft, an increase in air resistance, etc. Icing on the leading edges of the wings is especially dangerous because it makes lift unstable.
したがって、従来から翼前縁B等には着氷防止装置が配
設されている。Therefore, icing prevention devices have been conventionally provided at the leading edge B of the blade and the like.
従来の着氷防止装置としては、第4図に示すようにエン
ジンからの高温ガスを導管02および開閉制御されるア
ンチアイスバルブ°03等によって翼前縁Bの外板01
内側に導くようにしたものや、翼前縁Bの外板01の表
面に張付けたヒータ(図示せず)等が知られている。そ
して、これらの着氷防止装置は、前記高温ガスやヒータ
によって外板01を加熱し、外板01表面に接触してい
る着氷を溶融し、脱落させるようにしている。As shown in Fig. 4, a conventional icing prevention device uses a conduit 02 and an anti-ice valve 03 to control the opening and closing of the high-temperature gas from the engine to the outer plate 01 of the leading edge B of the wing.
Heaters that are guided inward, heaters that are attached to the surface of the outer plate 01 of the leading edge B of the blade (not shown), and the like are known. These icing prevention devices heat the outer panel 01 using the high-temperature gas or heater to melt the ice that is in contact with the surface of the outer panel 01 and cause it to fall off.
(3) 発明が解決しようとする課題ところが、高温
ガスで外板Ofを加熱する着氷防止装置では導管02、
アンチアイスバルブ03等により機体重量が増加すると
いう問題点があり、また、前記ヒータで外板01を加熱
する着氷防止装置では、氷を熔融するのに必要な消費電
力が多過ぎるという問題点があった。(3) Problem to be solved by the invention However, in the icing prevention device that heats the outer plate Of with high-temperature gas, the conduit 02,
There is a problem that the weight of the machine increases due to the anti-ice valve 03, etc., and the problem is that the icing prevention device that heats the outer panel 01 with the heater consumes too much power to melt the ice. was there.
本発明は前述の事情に鑑みてなされたもので、軽量で消
費エネルギの少ない着氷防止装置を提供することを課題
とする。The present invention has been made in view of the above-mentioned circumstances, and an object of the present invention is to provide an icing prevention device that is lightweight and consumes less energy.
B0発明の構成
(1)課題を解決するための手段
前記課題を解決するために、本発明の着氷防止装置は、
板体の着氷面の反対側の面に交流電圧が印加される圧電
素子が配設されたことを特徴とする。B0 Structure of the Invention (1) Means for Solving the Problems In order to solve the above problems, the icing prevention device of the present invention includes:
It is characterized in that a piezoelectric element to which an alternating current voltage is applied is disposed on the surface of the plate opposite to the icing surface.
(2)作用
前述の構成を備えた本発明の着氷防止装置は、板体の着
氷面の反対側の面に配設された圧電素子に交流電圧が印
加されると、その圧電素子が振動し、この圧電素子の振
動によって前記板体も振動し、その振動によって氷が振
るい落とされる。(2) Effect The icing prevention device of the present invention having the above-described configuration is such that when an alternating current voltage is applied to the piezoelectric element disposed on the opposite side of the icing surface of the plate, the piezoelectric element The piezoelectric element vibrates, and the plate also vibrates, and the vibration shakes off the ice.
(3)実施例
以下、図面にもとすいて本発明による着氷防止装置の第
1実施例について説明する。(3) Embodiment A first embodiment of the icing prevention device according to the present invention will be described below with reference to the drawings.
第1図において、航空機の翼前縁Bを形成する外板(す
なわち、板体)■の内面には上下方向に間隔を置いて複
数の圧電素子2,3,4.5が張付けられている。前記
圧電素子2.3.4.5は、図示されていないが、翼長
方向(第1図において紙面に垂直な方向)にも所定間隔
で配設されており、各圧電素子2.2.・・・、3.3
.・・・、4.4・・・、および5,5.・・・はそれ
ぞれ同一の交流電源り、、D、、D、、およびり、に接
続されている。In Fig. 1, a plurality of piezoelectric elements 2, 3, 4.5 are pasted at intervals in the vertical direction on the inner surface of an outer plate (i.e., a plate body) (i) forming the leading edge B of an aircraft wing. . Although not shown, the piezoelectric elements 2.3.4.5 are also arranged at predetermined intervals in the blade span direction (direction perpendicular to the plane of paper in FIG. 1), and each piezoelectric element 2.2. ..., 3.3
.. ..., 4.4..., and 5,5. . . are connected to the same AC power source, , D, , D, and , respectively.
次に、前述の構成を備えた本発明の第1実施例の作用に
ついて説明する。Next, the operation of the first embodiment of the present invention having the above-described configuration will be explained.
前記外板1表面に着氷が生じた場合には、前記交流電源
D t+ D 1.D 4+およびり、により前記圧電
素子2,3,4.および5を駆動する。その際各文流電
aD、、D、、D、、およびり、の位相をずらせておく
と、各圧電素子2,3,4.および5は、前記位相に応
じて振動する。そうすると、外板1は各圧電素子2,3
,4.および5が配設されている部分ごとに位相がずれ
た状態で振動する。この振動により前記外板1表面に付
着した氷は脱落する。When icing occurs on the surface of the outer panel 1, the AC power source D t+ D 1. D 4+ and the piezoelectric elements 2, 3, 4 . and drive 5. At that time, if the phases of the electric currents aD, , D, , D, and RI are shifted, each piezoelectric element 2, 3, 4, . and 5 vibrate according to the phase. Then, the outer plate 1 is connected to each piezoelectric element 2, 3.
,4. and 5 vibrate in a state where the phase is shifted for each part. This vibration causes the ice attached to the surface of the outer plate 1 to fall off.
次に、第2図に基づいて本発明による着氷防止装置の第
2実施例について説明する。Next, a second embodiment of the icing prevention device according to the present invention will be described based on FIG.
第2図に示した第2実施例は、外板1の内側面に、その
外板1よりも剛性の大きな支持板6がリベット7.7に
より連結されている。そして、支持板6と外板1との間
に圧電素子8,9が上下方向に間隔を置いて配設されて
いる。前記圧電素子8.9は、図示されていないが、翼
長方向(第2図において紙面に垂直な方向)にも所定間
隔で配設されており、各圧電素子8,8.・・・および
9゜9、・・・はそれぞれ交流電源D8およびり、に接
続されている。In the second embodiment shown in FIG. 2, a support plate 6 having greater rigidity than the outer panel 1 is connected to the inner surface of the outer panel 1 by rivets 7.7. Piezoelectric elements 8 and 9 are arranged between the support plate 6 and the outer plate 1 at intervals in the vertical direction. Although not shown, the piezoelectric elements 8.9 are also arranged at predetermined intervals in the blade span direction (direction perpendicular to the plane of the paper in FIG. 2), and each piezoelectric element 8, 8. ... and 9°9, ... are connected to AC power sources D8 and 9, respectively.
次に、前述の構成を備えた本発明の第2実施例の作用に
ついて説明する。Next, the operation of the second embodiment of the present invention having the above-described configuration will be explained.
前記外板1表面に着氷が生じた場合には、前記交流電源
D11およびり、により前記圧電素子8および9を駆動
する。その際各文流電源Dsおよびり、の位相をずらせ
ておくと、各圧電素子8および9は、前記位相に応じて
振動する。そうすると、支持板6の方が外板1よりも剛
性が大きいので、外板1の方が大きく振動する。このと
き、外板1は各圧電素子8および9が配設されている部
分ごとに位相がずれた状態で振動する。この振動により
前記外板1表面に付着した氷は脱落する。When ice builds up on the surface of the outer plate 1, the piezoelectric elements 8 and 9 are driven by the AC power source D11 and the AC power source D11. At this time, if the phases of the power sources Ds and R are shifted, each piezoelectric element 8 and 9 will vibrate according to the phase. In this case, since the support plate 6 has greater rigidity than the outer plate 1, the outer plate 1 vibrates more. At this time, the outer plate 1 vibrates with the phases shifted for each portion where the piezoelectric elements 8 and 9 are disposed. This vibration causes the ice attached to the surface of the outer plate 1 to fall off.
以上、本発明による着氷防止装置の実施例を詳述したが
、本発明は、前述の実施例に限定されるものではなく、
特許請求の範囲に記載された本発明を逸脱することなく
、種々の設計変更を行うことが可能である。Although the embodiments of the icing prevention device according to the present invention have been described in detail above, the present invention is not limited to the above-mentioned embodiments.
Various design changes can be made without departing from the scope of the invention as set forth in the claims.
たとえば、圧電素子2.3.4.5または8゜9の配設
位置と個数および印加電圧の位相を調整して外板1に上
方から下方への進行波を発生させたり、共振定常波を発
生させることにより、外板1外表面の着氷乞励課釣に下
方へ移動させて脱落させることも可能である。また、前
記圧電素子を支持する支持板6は外板1の裏面に連結す
るのではなく、翼桁等に連結することも可能である。さ
らに、前記圧電素子を実施例のようにブロンク形にする
代わりに、板状に張り合わせる形にしてもよい。また、
本発明は航空機の翼前縁Bだけでなく、表面に氷が付着
する板体であれば適用できる。For example, by adjusting the placement position and number of piezoelectric elements 2.3.4.5 or 8°9 and the phase of the applied voltage, a traveling wave from above to below can be generated on the outer plate 1, or a resonant standing wave can be generated. By doing so, it is also possible to move the icing on the outer surface of the outer panel 1 downward and cause it to fall off. Further, the support plate 6 that supports the piezoelectric element may be connected to a wing spar or the like instead of being connected to the back surface of the outer plate 1. Furthermore, instead of forming the piezoelectric element into a bronc shape as in the embodiment, it may be formed into a form laminated into a plate shape. Also,
The present invention can be applied not only to the leading edge B of an aircraft wing but also to any plate body on which ice adheres.
C0発明の効果
前述の本発明の着氷防止装置によれば、消費電力の少な
い圧電素子の振動により板体を振動させて、板体表面の
着氷を効果的に脱落させることができる。C0 Effects of the Invention According to the above-described icing prevention device of the present invention, the plate is vibrated by the vibration of the piezoelectric element that consumes less power, and ice on the surface of the plate can be effectively removed.
第1図は本発明による着氷防止装置の第1実施例の説明
図、第2図は同第2実施例の説明図、第3図および第4
図は従来技術の説明図、である。FIG. 1 is an explanatory diagram of the first embodiment of the icing prevention device according to the present invention, FIG. 2 is an explanatory diagram of the second embodiment, and FIGS.
The figure is an explanatory diagram of the prior art.
Claims (1)
素子が配設された着氷防止装置。An icing prevention device that includes a piezoelectric element to which an alternating current voltage is applied to the surface of a plate opposite to the icing surface.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63107846A JP2692134B2 (en) | 1988-04-30 | 1988-04-30 | Anti-icing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63107846A JP2692134B2 (en) | 1988-04-30 | 1988-04-30 | Anti-icing device |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH01278900A true JPH01278900A (en) | 1989-11-09 |
JP2692134B2 JP2692134B2 (en) | 1997-12-17 |
Family
ID=14469542
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63107846A Expired - Fee Related JP2692134B2 (en) | 1988-04-30 | 1988-04-30 | Anti-icing device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2692134B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009214873A (en) * | 2008-03-05 | 2009-09-24 | Hutchinson Sa | Anti-icing/de-icing system and method and aircraft structure incorporating this system |
JP2013545061A (en) * | 2010-09-28 | 2013-12-19 | サーブ アクティエボラーグ | Method and apparatus for deicing structural parts |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2908738B1 (en) * | 2006-11-16 | 2009-12-04 | Airbus France | AIRCRAFT ATTACK RIDGE. |
KR101838596B1 (en) * | 2017-07-13 | 2018-04-27 | 한국철도기술연구원 | Deicing device using piezoelectric element |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61119498A (en) * | 1984-11-15 | 1986-06-06 | 三菱重工業株式会社 | Icing preventive device |
-
1988
- 1988-04-30 JP JP63107846A patent/JP2692134B2/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS61119498A (en) * | 1984-11-15 | 1986-06-06 | 三菱重工業株式会社 | Icing preventive device |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009214873A (en) * | 2008-03-05 | 2009-09-24 | Hutchinson Sa | Anti-icing/de-icing system and method and aircraft structure incorporating this system |
JP2013545061A (en) * | 2010-09-28 | 2013-12-19 | サーブ アクティエボラーグ | Method and apparatus for deicing structural parts |
Also Published As
Publication number | Publication date |
---|---|
JP2692134B2 (en) | 1997-12-17 |
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Legal Events
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LAPS | Cancellation because of no payment of annual fees |