Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JP4232147B2 - Non-self-luminous switch structure - Google Patents
[go: Go Back, main page]

JP4232147B2 - Non-self-luminous switch structure - Google Patents

Non-self-luminous switch structure Download PDF

Info

Publication number
JP4232147B2
JP4232147B2 JP2003008327A JP2003008327A JP4232147B2 JP 4232147 B2 JP4232147 B2 JP 4232147B2 JP 2003008327 A JP2003008327 A JP 2003008327A JP 2003008327 A JP2003008327 A JP 2003008327A JP 4232147 B2 JP4232147 B2 JP 4232147B2
Authority
JP
Japan
Prior art keywords
push button
light
hole
pushed
panel
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.)
Expired - Fee Related
Application number
JP2003008327A
Other languages
Japanese (ja)
Other versions
JP2004220969A (en
Inventor
清孝 新井
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.)
Tamagawa Seiki Co Ltd
Original Assignee
Tamagawa Seiki Co Ltd
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 Tamagawa Seiki Co Ltd filed Critical Tamagawa Seiki Co Ltd
Priority to JP2003008327A priority Critical patent/JP4232147B2/en
Publication of JP2004220969A publication Critical patent/JP2004220969A/en
Application granted granted Critical
Publication of JP4232147B2 publication Critical patent/JP4232147B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Push-Button Switches (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、非自発光型スイッチ構造に関し、特に、ライティングパネルの貫通孔内に押ボタンを移動自在とし、押ボタンを押入した時に押ボタンの表面に光が照射されて押ボタンの押入動作を確認することができるようにするための新規な改良に関する。
【0002】
【従来の技術】
従来、用いられていた航空機等の分野で使用する非自発光型スイッチ構造としては、社内製作であるために、特許文献及び非特許文献を開示していないが、非自発光型で自発光型と同様の機能を有し、かつ、MIL規格等の規格をクリアできるものは未開発であった。
【0003】
【発明が解決しようとする課題】
従来のスイッチ構造においては、自発光型のスイッチ構造は開発されていたが、非自発光型の開発はなく、業界においてはその開発が切望されていた。
【0004】
本発明は、以上のような課題を解決するためになされたもので、特に、ライティングパネルの貫通孔内に押ボタンを移動自在とし、押ボタンを押入した時に押ボタンの表面に光が照射されて押ボタンの押入動作を確認することができるようにした非自発光型スイッチ構造を提供することを目的とする。
【0005】
【課題を解決するための手段】
本発明による非自発光型スイッチ構造は、貫通孔を有し光を導光するため航空機の計器盤に固定された板状のライティングパネルと、前記ライティングパネルの両側に配設された発光体と、前記貫通孔内に押入自在に位置すると共に正面側からみて全体形状が円盤形をなすと共にその表面の周縁に輪状のテーパ部を有する押ボタンと、前記押ボタンに軸を介して接続されると共に前記計器盤に固定され前記押ボタンの押入動作に連動して作動するスイッチ又はブレーカからなる切換え機能部とを備え、前記発光体からの光は前記ライティングパネル内をその面と平行な状態で導光され、前記貫通孔の内周は塗料等を施すことなく前記光が前記貫通孔内へ入光するように構成され、前記押ボタンを押入した場合、前記テーパ部は前記ライティングパネルの前面より内方へ押入され、前記ライティングパネル内の光は前記テーパ部に照射されて反射することにより、前記押ボタンの光の変化によって前記押ボタンが押入されたことを認識できる構成である。
【0006】
【発明の実施の形態】
以下、図面と共に本発明による非自発光型スイッチ構造の好適な実施の形態について説明する。
図1において符号1で示されるものはアクリル等の透明性の導光性部材からなる板状のライティングパネルであり、このライティングパネルは航空機等の操縦室の計器盤に固定されている。
【0007】
前記ライティングパネル1の側部位置には、その両側に発光体2が配設され、この発光体2からの光2aは前記ライティングパネル1内をその面と平行な状態で導光されるように構成されている。
【0008】
前記ライティングパネル1には、その厚さ方向に貫通して形成された貫通孔3が形成され、この貫通孔3内には押ボタン4が実線及び点線で示される位置に沿って押入自在すなわち移動自在に位置して配設されている。
前記貫通孔3の内周は塗料等を施すことなく前記光2aが貫通孔3内へ入光するように構成されている。
【0009】
前記押ボタン4は、正面側からみると全体形状が円盤形すなわち丸形をなしていると共に、その表面4aの周縁には、輪状に形成されたテーパ部5が設けられている。
【0010】
前記押ボタン4には、軸6を介して切換え機能部7が接続されており、この切換え機能部7は前記計器盤側に固定されている。
前記切換え機能部7は、周知のスイッチ又はブレーカ等の切換え機能を有しており、押ボタン4を実線から点線の状態に押すことにより、前記スイッチ又はブレーカの切換えが行われるように構成されている。
【0011】
前記押ボタン4が実線の位置から点線の位置まで押入されることにより、前記テーパ部5はライティングパネル1の前面1aより内方へ押入され、ライティングパネル1内の光はこのテーパ部5に照射されて反射することにより、押ボタン4の光の変化によって押ボタン4が押入されたことを認識することができる。
【0012】
【発明の効果】
本発明による非自発光型スイッチ構造は、以上のように構成されているため、次のような効果を得ることができる。
すなわち、導光性のライティングパネルに形成された貫通孔内に切換え機能部の押ボタンを押入自在に設け、押ボタン押入時の押ボタンに照射する光の変化を利用して、スイッチの作動状態を認識することができる。
また、従来の照光式(自発光式)押ボタンでない非自発光式の押ボタンスイッチを用いることができ、スイッチ採用の選択の幅を広げることができ、さらに、自発光式のスイッチに比べると、大幅にコストダウンが可能で、かつ、消費電力を少なくすることができる。
【図面の簡単な説明】
【図1】 本発明による非自発光型スイッチ構造を示す構成図である。
【符号の説明】
1 ライティングパネル
1a 前面
2 発光体
2a 光
3 貫通孔
4 押ボタン
4a 表面
5 テーパ部
6 軸
7 切換え機能部
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a non-self-luminous switch structure, and in particular, allows a push button to move freely in a through-hole of a lighting panel, and when the push button is pushed in, light is irradiated on the surface of the push button, thereby pushing the push button in. It relates to a new improvement so that it can be confirmed.
[0002]
[Prior art]
Conventionally, as a non-self-luminous switch structure used in the field of aircraft and the like that has been used, since it is manufactured in-house, patent literature and non-patent literature are not disclosed, but non-self-luminous and self-luminous type Those that have the same function and can clear the standards such as the MIL standard have not been developed yet.
[0003]
[Problems to be solved by the invention]
In the conventional switch structure, a self-luminous switch structure has been developed. However, there has been no development of a non-self-luminous type, and its development has been eagerly desired.
[0004]
The present invention has been made to solve the above-described problems. In particular, the push button can be freely moved into the through hole of the lighting panel, and when the push button is pushed, the surface of the push button is irradiated with light. It is an object of the present invention to provide a non-self-luminous switch structure that can confirm the push-in operation of the push button.
[0005]
[Means for Solving the Problems]
Non-self-luminous switch structure according to the present invention, the aircraft instrument panel to a fixed plate-shaped lighting panel for guiding light has a through hole, and the both sides disposed the emitters of the lighting panel , a push button having a tapered portion of the looped periphery of the surface along with the whole seen from the front side shape forms a disc-shaped with positioned freely pushed into the through-hole, Ru is connected via a shaft to said push button And a switching function unit comprising a switch or a breaker that is fixed to the instrument panel and operates in conjunction with the push-in operation of the push button, and the light from the light emitter is in a state parallel to the surface of the lighting panel. It is guided, an inner periphery of the through hole is configured such that the light without applying the paint or the like is incident to the through hole, when pushed the push button, the tapered portion is the other writing Is pushed from the front surface of the panel inwardly, light within said lighting panel by reflecting is irradiated to the tapered portion, the structure can be recognized in that the push button is pushed by a change in the light of the push button is there.
[0006]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, preferred embodiments of a non-self light emitting switch structure according to the present invention will be described with reference to the drawings.
1 is a plate-like lighting panel made of a transparent light-guiding member such as acrylic, and this lighting panel is fixed to a dashboard of a cockpit of an aircraft or the like.
[0007]
On a side position of the lighting panel 1, the light emitting element 2 on both sides of that is disposed, light 2a from the light emitting element 2 is guided through the lighting panel 1 in parallel with its plane It is configured as follows.
[0008]
The lighting panel 1 is formed with a through-hole 3 formed so as to penetrate in the thickness direction, and the push button 4 can be pushed in or moved along the position indicated by a solid line and a dotted line in the through-hole 3. Arranged freely.
The inner periphery of the through hole 3 is configured such that the light 2a enters the through hole 3 without applying paint or the like.
[0009]
The push button 4 has a disc shape, that is, a round shape as viewed from the front side, and a tapered portion 5 formed in a ring shape is provided on the periphery of the surface 4a.
[0010]
A switching function unit 7 is connected to the push button 4 via a shaft 6, and this switching function unit 7 is fixed to the instrument panel side.
The switching function unit 7 has a switching function such as a known switch or breaker, and is configured to switch the switch or breaker by pressing the push button 4 from a solid line to a dotted line. Yes.
[0011]
When the push button 4 is pushed from the position of the solid line to the position of the dotted line, the tapered portion 5 is pushed inward from the front surface 1a of the lighting panel 1, and light in the lighting panel 1 is irradiated to the tapered portion 5. By being reflected, it is possible to recognize that the push button 4 has been pushed in by a change in the light of the push button 4.
[0012]
【The invention's effect】
Since the non-self light emitting switch structure according to the present invention is configured as described above, the following effects can be obtained.
In other words, the push button of the switching function section is freely inserted into the through hole formed in the light guide lighting panel, and the switch operating state is utilized by utilizing the change in the light emitted to the push button when the push button is pressed. Can be recognized.
In addition, a non-self-lighting pushbutton switch that is not a conventional illuminated (self-lighting) pushbutton can be used, and the range of selection of adopting the switch can be widened. The cost can be greatly reduced and the power consumption can be reduced.
[Brief description of the drawings]
FIG. 1 is a configuration diagram illustrating a non-self-luminous switch structure according to the present invention.
[Explanation of symbols]
1 Writing panel
1a front
2 Light Emitter 2a Light 3 Through Hole 4 Push Button 4a Surface 5 Tapered Part
6 Axis 7 switching function part

Claims (1)

貫通孔(3)を有し光(2a)を導光するため航空機の計器盤に固定された板状のライティングパネル(1)と、前記ライティングパネル (1) の両側に配設された発光体 (2) と、前記貫通孔(3)内に押入自在に位置すると共に正面側からみて全体形状が円盤形をなすと共にその表面 (4a) の周縁に輪状のテーパ部 (5) を有する押ボタン(4)と、前記押ボタン(4)に (6) を介して接続されると共に前記計器盤に固定され前記押ボタン(4)の押入動作に連動して作動するスイッチ又はブレーカからなる切換え機能部(7)とを備え、前記発光体 (2) からの光 (2a) は前記ライティングパネル (1) 内をその面と平行な状態で導光され、前記貫通孔 (3) の内周は塗料等を施すことなく前記光 (2a) が前記貫通孔 (3) 内へ入光するように構成され、前記押ボタン(4)を押入した場合、前記テーパ部 (5) は前記ライティングパネル (1) の前面 (1a) より内方へ押入され、前記ライティングパネル (1) 内の光は前記テーパ部 (5) に照射されて反射することにより、前記押ボタン (4) の光の変化によって前記押ボタン (4) が押入されたことを認識できることを特徴とする非自発光型スイッチ構造。 A plate-like lighting panel (1) having a through hole (3) and fixed to an aircraft instrument panel for guiding light (2a), and a light emitter disposed on both sides of the lighting panel (1) (2) and a pushbutton which is positioned so as to be freely pressable into the through hole (3) and has a disk shape as a whole when viewed from the front side, and has a ring-shaped taper portion (5) on the periphery of the surface (4a). and (4), consisting of the push button switch or circuit breaker operates in conjunction with the pushed operation (4) is fixed to the shaft (6) is connected via a Rutotomoni the instrument panel the push button (4) switching and a function unit (7), the light from the light emitter (2) (2a) is guided through the lighting panel (1) in a parallel state and the surface, the inner periphery of the through hole (3) thus constructed the light without applying the paint or the like (2a) is incident to the through hole (3) in, when pushed the push button (4), the tapered portion (5) is the Rye Is pushed inwardly from the front surface (1a) of the coating panel (1), light in the lighting panel (1) is by reflecting is irradiated to the tapered portion (5), the light of the push button (4) A non-self-luminous switch structure characterized in that it can be recognized that the push button (4) has been pushed in by a change in the angle .
JP2003008327A 2003-01-16 2003-01-16 Non-self-luminous switch structure Expired - Fee Related JP4232147B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2003008327A JP4232147B2 (en) 2003-01-16 2003-01-16 Non-self-luminous switch structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2003008327A JP4232147B2 (en) 2003-01-16 2003-01-16 Non-self-luminous switch structure

Publications (2)

Publication Number Publication Date
JP2004220969A JP2004220969A (en) 2004-08-05
JP4232147B2 true JP4232147B2 (en) 2009-03-04

Family

ID=32898157

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003008327A Expired - Fee Related JP4232147B2 (en) 2003-01-16 2003-01-16 Non-self-luminous switch structure

Country Status (1)

Country Link
JP (1) JP4232147B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6510224B2 (en) * 2014-03-24 2019-05-08 能美防災株式会社 Indicator light
JP6398083B2 (en) * 2015-03-13 2018-10-03 パナソニックIpマネジメント株式会社 Cooker

Also Published As

Publication number Publication date
JP2004220969A (en) 2004-08-05

Similar Documents

Publication Publication Date Title
JP4985444B2 (en) Operating device with illumination function
CN104380414B (en) Illumination display switch device
JP4278002B2 (en) Illuminated push switch unit
RU2411141C2 (en) Automotive multifunction data display and control device
JP2017134985A (en) Start switch device
JP2008192407A (en) Operation switch
TWM535390U (en) Light control button switch
JP4232147B2 (en) Non-self-luminous switch structure
JP4668867B2 (en) Operating device
US10397995B2 (en) Input device
EP2487672B1 (en) Indicator device
US10564777B2 (en) Display device and input device
JP2003249142A (en) Lighted push-button device
JP2002319324A (en) Button device
JPH0356972Y2 (en)
JP2022137900A (en) Illumination device
JPH0236176Y2 (en)
JP4992749B2 (en) Elastic material for pressure switch and operation device provided with the same
JPH11185558A (en) Switch device
JPH0548697A (en) Keyboard
CN117953618A (en) Key with glowing icon
WO2020071900A1 (en) A light display assembly
JPH06175744A (en) Knob guide
JP2014225382A (en) Display light-emitting switch
JP2005243253A (en) Push-button device

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20051227

RD04 Notification of resignation of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7424

Effective date: 20070821

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20080701

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20080812

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20081118

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20081127

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20111219

Year of fee payment: 3

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20121219

Year of fee payment: 4

LAPS Cancellation because of no payment of annual fees