JPS6053874A - Electronic timepiece with pressure sensor - Google Patents

Electronic timepiece with pressure sensor

Info

Publication number
JPS6053874A
JPS6053874A JP58161710A JP16171083A JPS6053874A JP S6053874 A JPS6053874 A JP S6053874A JP 58161710 A JP58161710 A JP 58161710A JP 16171083 A JP16171083 A JP 16171083A JP S6053874 A JPS6053874 A JP S6053874A
Authority
JP
Japan
Prior art keywords
circuit
atmospheric pressure
altitude
depth
memory circuit
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
JP58161710A
Other languages
Japanese (ja)
Inventor
Yukio Ikehata
池端 幸夫
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.)
Seiko Instruments Inc
Original Assignee
Seiko Instruments Inc
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 Seiko Instruments Inc filed Critical Seiko Instruments Inc
Priority to JP58161710A priority Critical patent/JPS6053874A/en
Publication of JPS6053874A publication Critical patent/JPS6053874A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G04HOROLOGY
    • G04GELECTRONIC TIME-PIECES
    • G04G9/00Visual time or date indication means
    • G04G9/0064Visual time or date indication means in which functions not related to time can be displayed

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Electric Clocks (AREA)
  • Indication And Recording Devices For Special Purposes And Tariff Metering Devices (AREA)

Abstract

PURPOSE:To make it possible to measure not only an absolute altitude and the absolute depth of water but also a relative altitude and the relative depth of water and to enable use as an atmospheric pressure meter, by using a readable memory circuit and a freely writable and readable memory circuit. CONSTITUTION:The standard atmospheric pressure at 0m above sea level of a readable memory circuit 7 is written in a freely readable memory citcuit 8. An absolute altitude is calculated by differential operation of the content of said circuit 8 and atmospheric pressure through a pressure sensor 1 and a count circuit 6 and displayed by a display part 15. On the ohter hand, when the content of the circuit 6 is written in the circuit 8 and set to a reference value, a relative altitude is similarily measured. The depth of water is also similarily measured and the measurement of atmospheric pressure is also similarily performed. By these mechanisms, an electronic timepiece with a pressure sensor functions not only as an absolute altitude and water-depth meter but also a relative altitude and water-depth meter of an atmospheric pressure meter.

Description

【発明の詳細な説明】 本発明は圧力センサーを有し、大気圧計または高度計ま
たは水深計の機能をもつ電子時計に関するもので、本発
明の目的とするところは大気圧。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an electronic watch that has a pressure sensor and functions as an atmospheric pressure gauge, an altimeter, or a water depth gauge, and the object of the present invention is to measure atmospheric pressure.

高度。水深の絶対的な値の測定だけでなく、外部操作に
よって外部操作時の計測値を基準にとることによって相
対的な値の測足ヲも可能にすることにおる。例えば高度
計や水深計の場合、出発点において外部操作を行なうこ
とによって出発点から何メートル高い所または低い所に
到達したかを測定することが可能になる。ま九人気圧計
の場合、ある時点で外部操作を行なうことによって、そ
の時点から天候が回復に向っているのか悪化しているの
かが一目で判別可能になる。
Altitude. It is possible not only to measure the absolute value of water depth, but also to measure relative values by using an external operation and using the measured value at the time of external operation as a reference. For example, in the case of an altimeter or a depth meter, by performing an external operation at the starting point, it is possible to measure how many meters higher or lower the user has reached from the starting point. In the case of a barometer, by operating it externally at a certain point, it is possible to determine at a glance whether the weather is improving or worsening from that point on.

以下、本発明の一実施例を図面にしたがって説明する。An embodiment of the present invention will be described below with reference to the drawings.

第1図r1本発明の一実施例を示すもので、1は圧力情
報を電圧に変換する圧力センサー、2は圧力センサーの
出力電圧を増幅する増幅回路、3は電源電流によシ発振
周波数を制御できる発振回路、4は発掘回路3の電源電
流を制御するためのMO日トリンジスタ、5は制御回路
からくる信号αがHとなる区間のみ発掘回路3の出力パ
ルスを通過させるためのANDゲート、6はANDゲー
ト5を通過したパルスの数を計数する計数回路、7は読
み出し可能な第一の記憶回路、8は曹き込み。読み出し
可能な第二の記憶回路、9.10.11は各々制御部か
らくる信号す、C,dによって制御さnるクロックド、
インバータ群、12は第二の記憶回路8の内容を基準と
して引数回路の計数値から予め設定さ2]、演算を行な
い高度差−1,fC,は大気圧差または水深差の情報を
出力する演算回路、13はデコーダ、14は駆動回路、
15は表示部である。第2図は圧力センサ1に加木ら1
Lる圧力Pと増幅回路2の出力電圧Vの関係を示す図で
あ)、第3図は増幅回路2の出力電圧すなわちMOS)
ランジスタ4のゲートに印加さnる電圧■とANDゲー
ト5を通力口するパルス数すなわち計数回路6の計数値
Hの関係を示す図、1?ある。以下高度計機能の場合を
例にさらに詳しく説明すると、第一の記憶回路7には標
高o 、mでの標準の大気圧P。
Figure 1 shows an embodiment of the present invention, in which 1 is a pressure sensor that converts pressure information into voltage, 2 is an amplifier circuit that amplifies the output voltage of the pressure sensor, and 3 is an oscillation frequency that is controlled by the power supply current. 4 is a MO transistor for controlling the power supply current of the excavation circuit 3; 5 is an AND gate for passing the output pulse of the excavation circuit 3 only in the section where the signal α coming from the control circuit is H; 6 is a counting circuit that counts the number of pulses that have passed through the AND gate 5; 7 is a readable first memory circuit; and 8 is a filler. The readable second storage circuits 9, 10 and 11 are clocked and controlled by signals C and d coming from the control section, respectively.
The inverter group 12 is set in advance from the count value of the argument circuit based on the contents of the second memory circuit 8, and performs calculations, and the altitude difference -1, fC, outputs information on the atmospheric pressure difference or water depth difference. an arithmetic circuit, 13 a decoder, 14 a drive circuit,
15 is a display section. Figure 2 shows pressure sensor 1 and Kagi et al.
Figure 3 shows the relationship between the output voltage V of the amplifier circuit 2 and the output voltage V of the amplifier circuit 2).
1 is a diagram showing the relationship between the voltage applied to the gate of the transistor 4 and the number of pulses output through the AND gate 5, that is, the count value H of the counting circuit 6. be. To explain in more detail below using the altimeter function as an example, the first memory circuit 7 stores the standard atmospheric pressure P at altitudes o and m.

に対応する値N、を予め設定しておく。高度の絶対値ヲ
引測する場合、信号0でクロックド。インバータ10を
一時的に動作させ第二の記憶回路8に第一の記憶回路7
の記憶内容N。全転送しておく。ある高度(大気圧P1
)で測定するときには、計数回路6の計数値N8 と、
信号dによシクロックド、インバータ群11ヲ一時的に
動作させ第二の記憶回路8の記憶内容Noとを演算回路
12に入力する。演算回路12ではN、を基準としてN
1 との差分をとり、この差分に予め定めら−nだ係数
を掛けて高度に換算する。したがって表示部には高度の
絶対値が表示さ扛る。次に大気圧PKの高度で相対的高
度を計測する几めに外部操作(例えばスイッチON)を
した場合、制御回路は信号すによってクロックド、イン
バータ9f、一時的K m、+作させて、l に対応す
る計数値N、を第二の記憶回路8に書き込む。次にある
高度(大気圧Pm)で測定するときには、計数回路6の
計数値N、と、信号dによシフ四ツクド。インバータ群
11全一時的に動作させ第二の記憶回路の記憶内容N1
とを演算回路12に入力する。演算回路12ではN1を
基準としてN、との差分をとり、この差分に前記係数を
掛けて高度に換算する。し几がって表示部には大気圧P
1の地膚を基準とした大気圧P8の地点の高度(相対普
度ンが表示さする。さらに大気圧P、の地点で絶対高度
全測定するために外部操作をした場合、制御回路は信号
0によってクロックド、インバータ群10を一時点に動
作させ、第二の記憶回路8にN@’を畳き込み、以後前
述と同様演算回路はNoを基準としてN、から高度を換
算し絶対高度を表示する。また、第4図に示す様に制御
部18は、外部操作入力と分周回路の分局信号を入力し
、各信号αebecmdk作る。第5図は前記各信号α
tbe’tdの概略タイミングチャートでちり、第5図
においてEはクロックドインバータを動作させる場合の
信号、Fはクロックドインバータを動作させない場合の
信号を示す。
A value N corresponding to is set in advance. When measuring the absolute value of altitude, clock with signal 0. The inverter 10 is temporarily operated so that the second memory circuit 8 is connected to the first memory circuit 7.
Memory contents N. Transfer everything. At a certain altitude (atmospheric pressure P1
), the count value N8 of the counting circuit 6 and
When the signal d is clocked, the inverter group 11 is temporarily operated and the stored content No. of the second storage circuit 8 is inputted to the arithmetic circuit 12. The arithmetic circuit 12 uses N as a reference.
1, and this difference is multiplied by a predetermined coefficient of -n to convert it into altitude. Therefore, the absolute value of altitude is displayed on the display. Next, when an external operation is performed (for example, turning on a switch) to measure the relative altitude at the altitude of atmospheric pressure PK, the control circuit is clocked by the signal, inverter 9f, and temporarily K m,+ are activated. A count value N corresponding to l is written into the second storage circuit 8. Next, when measuring at a certain altitude (atmospheric pressure Pm), the count value N of the counting circuit 6 and the signal d are shifted. The inverter group 11 is all temporarily operated to store the memory content N1 of the second memory circuit.
is input to the arithmetic circuit 12. The arithmetic circuit 12 calculates the difference between N1 and N1, and multiplies this difference by the coefficient to convert it into an altitude. Then, the display shows atmospheric pressure P.
The altitude (relative altitude) at a point with atmospheric pressure P8 with respect to the ground of 1 is displayed.Furthermore, when an external operation is performed to measure the absolute altitude at a point with atmospheric pressure P, the control circuit outputs a signal of 0. The clocked inverter group 10 is operated at a certain point, and the second memory circuit 8 is convolved with N@'. From then on, the arithmetic circuit uses No as a reference and converts the altitude from N to obtain the absolute altitude. Furthermore, as shown in FIG. 4, the control section 18 inputs an external operation input and a division signal of the frequency dividing circuit to create each signal αebecmdk.FIG.
In the schematic timing chart of tbe'td, in FIG. 5, E indicates a signal when the clocked inverter is operated, and F indicates a signal when the clocked inverter is not operated.

(なお、第2の記憶回路にWt1込まl’Lる値は、正
確にはNo −No e No等のクロックド、インバ
ータ9′i!たは10でインバートさnたものであるが
、演算回路に入力さ牡る時にクロックド、インバータ1
1で再度インバートさnN6− No −Nt等の値に
戻るので説明を簡単にするためインバートさすることに
ついての説明は省略した。)以下高度計機能の場合につ
いて詳細に説明した++ Q − が、大気圧計機能の場合はもちろん水深計機能の場合も
演算回路の演算を各々の機能に見合ったものにすnば高
度計機能の場合と同様に実現できる以上の様に本発明に
よしは、第二の記憶回路に第一の記憶回路の内容または
計数回路の計数値を外部操作により選択的に書き込み、
第二の記憶回路の内容を基準として大気圧ま7Cは高度
または水深に換算することで、絶対値。相対値が選択的
に測定可能となるという大きな効果がある。
(Accurately, the value Wt1 and l'L in the second storage circuit is clocked such as No - No e No, and is inverted by the inverter 9'i! or 10, but it is Clocked when input to the circuit, inverter 1
1, the value is inverted again to return to a value such as nN6-No-Nt, so for the sake of simplicity, a description of inverting is omitted. ) Below, we have explained in detail the case of the altimeter function ++ Q -, but in the case of the barometer function as well as the depth meter function, if the calculation of the calculation circuit is made appropriate for each function, then the altimeter function can be According to the present invention, the content of the first storage circuit or the count value of the counting circuit is selectively written into the second storage circuit by an external operation.
Based on the contents of the second memory circuit, the atmospheric pressure or 7C can be converted to altitude or water depth to give an absolute value. This has the great effect of allowing relative values to be measured selectively.

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

第1図は本発明の一実施例を示す回路説明図、第2図は
圧力Pと増幅回路出力電圧Vの関係を示す図、第3図は
増幅回路出力電圧■と計数回路の計数値Nの関係を示す
図、第4図は時計用回路の一部を示すブロック図、第5
図は信号αtbsC2dの概略を示すタイミングチャー
ドである。 1□田カセンサ 20.増幅回路 6一 3、。発振回路 4・・MOS)ランジスタ 5゜、ANDゲート 6、。計数回路 7.8第一の記憶回路 8、。第二の記憶回路 9 、10 、11 、 、クロックドインバータ群1
2 、。演算回路 16゜0時計用発振回路13゜。デ
コーダ 17.。分周回路 14゜、駆動回路 18゜、制御部 15、。表示部 ]90.スイッチ群 以上 出願人 株式会社第二精工舎 代理人 弁理士最上 務 7一
Fig. 1 is a circuit explanatory diagram showing an embodiment of the present invention, Fig. 2 is a diagram showing the relationship between pressure P and amplifier circuit output voltage V, and Fig. 3 is a diagram showing the relationship between amplifier circuit output voltage ■ and count value N of the counting circuit. Figure 4 is a block diagram showing a part of the clock circuit; Figure 5 is a block diagram showing a part of the clock circuit;
The figure is a timing chart schematically showing the signal αtbsC2d. 1□Taka sensor 20. Amplification circuit 6-3. Oscillation circuit 4...MOS) transistor 5°, AND gate 6. Counting circuit 7.8 First storage circuit 8,. Second memory circuit 9 , 10 , 11 , clocked inverter group 1
2. Arithmetic circuit 16°0 Clock oscillation circuit 13°. Decoder 17. . Frequency dividing circuit 14°, drive circuit 18°, control unit 15. Display section ]90. Applicant for switch group and above Daini Seikosha Co., Ltd. Attorney Mogami Mogami 71

Claims (1)

【特許請求の範囲】[Claims] 圧力を電圧teは電流に変換し検出する圧力センサーと
、電圧tたは電流により発振周波数が制御される発振回
路と、該発振回路の出力を計数する計数回路と、少(と
も読み出し可能な第1の記憶回路と、書き込み、読み出
し可能に第2の記憶回路とを有し、前記第1の記憶回路
の内容f7’cは前記計数回路の計数値を外部操作によ
シ選択的に前記第2の記憶回路に書き込み、第2の記憶
回路の内容を基準として大気圧または高度または水深に
換算し表示する圧力センサー付電子時計。
A pressure sensor that converts pressure into a current and detects it; an oscillation circuit whose oscillation frequency is controlled by the voltage t or current; a counting circuit that counts the output of the oscillation circuit; 1 memory circuit and a second memory circuit capable of writing and reading, and the content f7'c of the first memory circuit is determined by selectively changing the count value of the counting circuit by an external operation. An electronic watch with a pressure sensor that writes data into a second memory circuit and converts and displays atmospheric pressure, altitude, or water depth based on the contents of the second memory circuit.
JP58161710A 1983-09-02 1983-09-02 Electronic timepiece with pressure sensor Pending JPS6053874A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58161710A JPS6053874A (en) 1983-09-02 1983-09-02 Electronic timepiece with pressure sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58161710A JPS6053874A (en) 1983-09-02 1983-09-02 Electronic timepiece with pressure sensor

Publications (1)

Publication Number Publication Date
JPS6053874A true JPS6053874A (en) 1985-03-27

Family

ID=15740405

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58161710A Pending JPS6053874A (en) 1983-09-02 1983-09-02 Electronic timepiece with pressure sensor

Country Status (1)

Country Link
JP (1) JPS6053874A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020097356A (en) * 2001-06-20 2002-12-31 현대자동차주식회사 Atmospheric pressure display method in multimeter
JP2008082909A (en) * 2006-09-28 2008-04-10 Casio Comput Co Ltd Altimeter
JP2016114600A (en) * 2014-12-15 2016-06-23 ザ・スウォッチ・グループ・リサーチ・アンド・ディベロップメント・リミテッド External element with pressure sensor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020097356A (en) * 2001-06-20 2002-12-31 현대자동차주식회사 Atmospheric pressure display method in multimeter
JP2008082909A (en) * 2006-09-28 2008-04-10 Casio Comput Co Ltd Altimeter
JP2016114600A (en) * 2014-12-15 2016-06-23 ザ・スウォッチ・グループ・リサーチ・アンド・ディベロップメント・リミテッド External element with pressure sensor

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