WO2011067835A1 - 空中超音波センサ - Google Patents
空中超音波センサ Download PDFInfo
- Publication number
- WO2011067835A1 WO2011067835A1 PCT/JP2009/070221 JP2009070221W WO2011067835A1 WO 2011067835 A1 WO2011067835 A1 WO 2011067835A1 JP 2009070221 W JP2009070221 W JP 2009070221W WO 2011067835 A1 WO2011067835 A1 WO 2011067835A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- ultrasonic sensor
- case
- closed surface
- aerial ultrasonic
- aerial
- Prior art date
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/52—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S15/00
- G01S7/521—Constructional features
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/18—Methods or devices for transmitting, conducting or directing sound
- G10K11/26—Sound-focusing or directing, e.g. scanning
- G10K11/28—Sound-focusing or directing, e.g. scanning using reflection, e.g. parabolic reflectors
Definitions
- the present invention relates to an aerial ultrasonic sensor that detects the presence or absence of an obstacle by radiating ultrasonic waves into the air and receiving reflected waves from surrounding objects.
- This type of aerial ultrasonic sensor uses a piezoelectric element to radiate ultrasonic waves into the air. By receiving reflected waves reflected from an obstacle or the like with the aerial ultrasonic sensor, the obstacle is detected. It is used in obstacle detection systems that detect it. For example, it is used in a detection system mounted on a vehicle such as an automobile (see, for example, Patent Documents 1 and 2).
- patent document 1 it has the box-shaped case body opened on one surface, a piezoelectric element is arrange
- a metal case that has a rectangular vibration part and a piezoelectric element is attached to the vibration part, and a storage recess that houses the metal case is opened on one side, and the metal case vibrates from a window hole provided at the bottom of the storage recess. It is characterized by comprising a synthetic resin resin case in which a metal case is disposed in the housing recess with the portion exposed to the outside.
- the vibration part of the metal case to which the piezoelectric element is attached is exposed to the outside through a window hole provided in the bottom of the storage recess, and the aspect ratio of the vibration part is set to a predetermined ratio, so that the ultrasonic wave An aerial ultrasonic sensor capable of adjusting directivity is obtained.
- a unimorph vibration is comprised by bonding a piezoelectric element inside the bottomed cylindrical case provided with a dug that is relatively long in one direction and relatively short in another direction
- the ultrasonic transducer that transmits and receives ultrasonic waves on the outer surface of the case of the vibrating body, an opening that does not exceed this width is provided on the relatively short side surface of the bottomed cylindrical case.
- the directivity is narrowed. Therefore, when these aerial ultrasonic sensors are attached to a bumper of an automobile, it is possible to obtain a directivity with a different directionality that is wide in the direction parallel to the road surface and narrow in the vertical direction.
- the directivity in the direction parallel to or perpendicular to the road surface becomes a symmetrical directivity pattern with the aerial ultrasonic sensor as the center.
- the directivity characteristics in the direction perpendicular to the road surface need to be wide on the road surface side, but there are no detection targets in the direction opposite to the road surface, that is, the sky side. May be narrow. Therefore, when performing such detection, an aerial ultrasonic sensor having an asymmetric directional pattern is desired.
- the conventional aerial ultrasonic sensor has a problem that the directivity pattern in a predetermined direction cannot be asymmetrical.
- the present invention has been made to solve the above-described problems, and an object thereof is to obtain an aerial ultrasonic sensor capable of making a directivity pattern in a predetermined direction asymmetric with a simple configuration. is there.
- the aerial ultrasonic sensor comprises a case having one end opened, the other end serving as a closed surface, and having a hollow portion, and a piezoelectric element disposed inside the closed surface, wherein the closed surface is a vibrating surface.
- the side surface of the case is provided with a region at least partially removed from the opening surface side.
- the region removed from the opening surface side is provided in at least a part of the side surface of the case, no ultrasonic wave is radiated when the side surface of the case vibrates, and therefore the sensor structure As a result, the directivity pattern in a predetermined direction can be made asymmetric with a simple configuration.
- FIG. 3 is a diagram showing the structure of an aerial ultrasonic sensor used in the simulation shown in FIG. 2, wherein (a) is a cross-sectional view cut along AA ′ in (b), and (b) is a side view showing a two-dimensional plane model.
- FIG. It is a figure which shows the directivity characteristic simulation result of the airborne ultrasonic sensor equivalent to a prior art example.
- FIG. 5A and 5B are diagrams showing the structure of the aerial ultrasonic sensor used in the simulation shown in FIG. 4, wherein FIG. 5A is a cross-sectional view taken along line AA ′ in FIG. 4B, and FIG. 5B is a side view showing a two-dimensional plane model.
- FIG. FIG. 2 is a diagram illustrating an example in which the shape of the closed surface of the case 1 is substantially circular in the aerial ultrasonic sensor shown in FIG. 1.
- FIG. 2 is a diagram illustrating an example in which the shape of a closed surface of a case 1 is substantially oval in the aerial ultrasonic sensor illustrated in FIG. 1.
- FIG. 2 is a diagram illustrating an example in which the shape of a closed surface of a case 1 is substantially square in the aerial ultrasonic sensor illustrated in FIG. 1.
- FIG. 2 is a diagram illustrating an example in which the shape of a closed surface of a case 1 is substantially rectangular in the aerial ultrasonic sensor illustrated in FIG. 1.
- FIG. 1A and 1B are schematic views showing an aerial ultrasonic sensor according to Embodiment 1 of the present invention.
- FIG. 1A is a side view and FIG. 1B is a top view.
- This aerial ultrasonic sensor is composed of a case 1 having one end opened and the other end being a closed surface, and a circular flat plate-shaped piezoelectric element 2 provided inside the closed surface of the case 1.
- the piezoelectric element 2 is a case. 1 is fixed to the center position inside the closed surface by an adhesive or the like.
- the input / output terminal 3 a is connected to the case 1, and the input / output terminal 3 b is connected to the surface opposite to the bonding surface of the piezoelectric element 2 with the case 1.
- the case 1 is made of, for example, a relatively rigid resin reinforced by a glass cloth or a metal such as aluminum, and the side surface 1a of the case 1 is provided with a region 1b that is removed at least partially from the opening surface side.
- the opposing surfaces are asymmetrically shaped.
- the piezoelectric element 2 is made of a piezoelectric ceramic such as PZT or barium titanate. In the aerial ultrasonic sensor according to the first embodiment, the piezoelectric element 2 can be vibrated and ultrasonic waves can be generated by applying drive signals from the input / output terminals 3a and 3b.
- FIG. 2 is a directional characteristic simulation result of the aerial ultrasonic sensor according to the first embodiment
- FIG. 3 is a diagram illustrating a structure of the aerial ultrasonic sensor used in the simulation
- FIG. A cross section taken along line AA ′ of FIG. 3 (b) is shown.
- the two-dimensional plane model shown in FIG. 3A is used as a simulation model.
- FIG. 4 is a directional characteristic simulation result of an aerial ultrasonic sensor corresponding to the conventional example
- FIG. 5 is a diagram showing a structure of the aerial ultrasonic sensor used in the simulation
- the two-dimensional plane model shown in FIG. 5A is used as the simulation model.
- 2 and 4 show the sound pressure distribution within a radius of 20 cm when the sensor is arranged at the center of the semicircle, showing the intensity of the sound pressure by the color shading, and the light color.
- the region indicates a region where the sound pressure is strong, that is, a region where ultrasonic waves are radiated strongly.
- the ultrasonic wave radiated by the vibration of the side surface of the case is provided. Sound waves are not generated. Therefore, as shown in FIG. 2, the region where the ultrasonic wave is strongly emitted in the front direction is changed from about ⁇ 30 ° to about 40 ° as shown in FIG. 2, and the sensor structure is asymmetric around 0 °. It becomes directional characteristics.
- the region 1b removed from the side surface 1a of the case 1 does not exist, ultrasonic waves radiated are generated when the side surface of the case vibrates. Therefore, since the sensor structure is symmetric, as shown in FIG. 4, the region where the ultrasonic wave is strongly emitted in the front direction is from -20 ° to 20 °, and the directional characteristics are symmetrical around 0 °. Become.
- the aerial ultrasonic sensor As described above, according to the aerial ultrasonic sensor according to the first embodiment, it is possible to obtain a directional characteristic that is asymmetrical with respect to the left and right of the aerial ultrasonic sensor. Therefore, when the aerial ultrasonic sensor is attached to a bumper of an automobile.
- the narrow side of the directional characteristic on the sky side and the wide side of the directional characteristic on the road surface side the directional characteristic on the road surface side is wide, and the directional characteristic on the opposite side to the road surface is narrow. be able to.
- the directivity characteristic of the aerial ultrasonic sensor according to the first embodiment can be adjusted by the area removed from the case 1. That is, in the above description, the narrow side of the directivity is the side where the region 1b is removed from the side surface of the case 1 in FIG. 1, and in the directivity simulation result shown in FIG. The directivity characteristics contributed by the area where the area 1b exists, and the positive angle side becomes directivity characteristics contributed by the area where the area 1b does not exist.
- the vibration on the closed surface the surface opposite to the side where the piezoelectric element 2 is provided in the case 1 is dominant and the ultrasonic wave is radiated. Contributes to the emission of sound waves.
- the directivity characteristics of the aerial ultrasonic sensor according to the first embodiment can be adjusted by the area removed from the case 1.
- the shape of the closed surface of the case 1 has been described as being substantially circular.
- the shape is not limited to this, and the region 1b has a substantially oval shape as shown in FIG. A similar effect can be obtained even with the configuration provided with.
- the shape of the closed surface of the case 1 has been described as being substantially circular.
- the present invention is not limited to this, and the region 1b is a substantially oval shape as shown in FIG. A similar effect can be obtained even with the configuration provided with.
- the shape of the closed surface of the case 1 has been described as a substantially circular shape.
- the shape is not limited to this, and the region 1b in which the side surface of the case 1 is removed has a substantially square shape as shown in FIG. Similar effects can be obtained with the provided configuration.
- the shape of the closed surface of the case 1 has been described as a substantially circular shape.
- the shape is not limited to this, and the region 1b from which the side surface of the case 1 is removed has a substantially rectangular shape as shown in FIG. Similar effects can be obtained with the provided configuration.
- the present invention is used in an obstacle detection system for detecting an obstacle, and is particularly useful for a detection system mounted on a vehicle such as an automobile.
- case 1 case, 1a side surface of case 1, 1b area removed from opening side, 2 piezoelectric elements, 3a, 3b input / output terminals.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Multimedia (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Transducers For Ultrasonic Waves (AREA)
- Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
Abstract
Description
この発明の実施の形態1に係る空中超音波センサについて図を参照しながら説明する。図1は、この発明の実施の形態1に係る空中超音波センサを示す概略図であり、図1(a)は側面図、図1(b)は上面図である。この空中超音波センサは、一端が開口し、他端が閉塞面となるケース1と、ケース1の閉塞面の内側に設けられた円形平板形状の圧電素子2とからなり、圧電素子2はケース1の閉塞面の内側の中心位置に接着剤等により固着されている。入出力端子3aは、ケース1に接続され、入出力端子3bは、圧電素子2のケース1との接着面とは反対面に接続されている。
Claims (6)
- 一端が開口し、他端が閉塞面となり、中空部を有するケースと、
前記閉塞面の内側に配置された圧電素子と
からなり、前記閉塞面が振動面となる空中超音波センサであって、
前記ケースの側面は、少なくとも一部に開口面側から取り除いた領域が設けられている
ことを特徴とする空中超音波センサ。 - 請求項1に記載の空中超音波センサにおいて、
前記閉塞面は円形でなる
ことを特徴とする空中超音波センサ。 - 請求項1に記載の空中超音波センサにおいて、
前記閉塞面は楕円形でなる
ことを特徴とする空中超音波センサ。 - 請求項1に記載の空中超音波センサにおいて、
前記閉塞面は長円形でなる
ことを特徴とする空中超音波センサ。 - 請求項1に記載の空中超音波センサにおいて、
前記閉塞面は正方形でなる
ことを特徴とする空中超音波センサ。 - 請求項1に記載の空中超音波センサにおいて、
前記閉塞面は長方形でなる
ことを特徴とする空中超音波センサ。
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/512,043 US20120269039A1 (en) | 2009-12-02 | 2009-12-02 | Airborne ultrasonic sensor |
CN2009801626895A CN102667523A (zh) | 2009-12-02 | 2009-12-02 | 空中超声波传感器 |
DE112009005416T DE112009005416T5 (de) | 2009-12-02 | 2009-12-02 | In der luft befindlicher ultraschallsensor |
PCT/JP2009/070221 WO2011067835A1 (ja) | 2009-12-02 | 2009-12-02 | 空中超音波センサ |
JP2011544143A JPWO2011067835A1 (ja) | 2009-12-02 | 2009-12-02 | 空中超音波センサ |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/JP2009/070221 WO2011067835A1 (ja) | 2009-12-02 | 2009-12-02 | 空中超音波センサ |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2011067835A1 true WO2011067835A1 (ja) | 2011-06-09 |
Family
ID=44114700
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2009/070221 WO2011067835A1 (ja) | 2009-12-02 | 2009-12-02 | 空中超音波センサ |
Country Status (5)
Country | Link |
---|---|
US (1) | US20120269039A1 (ja) |
JP (1) | JPWO2011067835A1 (ja) |
CN (1) | CN102667523A (ja) |
DE (1) | DE112009005416T5 (ja) |
WO (1) | WO2011067835A1 (ja) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014027516A (ja) * | 2012-07-27 | 2014-02-06 | Nippon Ceramic Co Ltd | 超音波送受波器 |
WO2017141402A1 (ja) * | 2016-02-18 | 2017-08-24 | 三菱電機株式会社 | 超音波送受信装置、壁部材、および、壁部材への超音波センサの取付方法 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012077224A1 (ja) * | 2010-12-10 | 2012-06-14 | 三菱電機株式会社 | 空中超音波センサ |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2005072771A (ja) * | 2003-08-21 | 2005-03-17 | Nippon Soken Inc | 超音波センサ |
JP2006345271A (ja) * | 2005-06-09 | 2006-12-21 | Nippon Ceramic Co Ltd | 超音波送受波器 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3137745A1 (de) * | 1981-09-23 | 1983-04-07 | Egon 5000 Köln Gelhard | Sensor fuer die durchfuehrung der distanzmessung nach dem ultraschalll-echoprinzip |
JP4023061B2 (ja) | 2000-02-24 | 2007-12-19 | 松下電工株式会社 | 超音波振動子 |
EP1906383B1 (en) * | 2006-09-29 | 2013-11-13 | Tung Thih Electronic Co., Ltd. | Ultrasound transducer apparatus |
JP4367534B2 (ja) * | 2007-06-12 | 2009-11-18 | 株式会社デンソー | 超音波センサ |
CN201072444Y (zh) * | 2007-07-20 | 2008-06-11 | 成都汇通西电电子有限公司 | 超声波传感器探头 |
DE102008040905A1 (de) * | 2008-07-31 | 2010-02-04 | Robert Bosch Gmbh | Ultraschallsensor |
-
2009
- 2009-12-02 CN CN2009801626895A patent/CN102667523A/zh active Pending
- 2009-12-02 US US13/512,043 patent/US20120269039A1/en not_active Abandoned
- 2009-12-02 DE DE112009005416T patent/DE112009005416T5/de not_active Withdrawn
- 2009-12-02 WO PCT/JP2009/070221 patent/WO2011067835A1/ja active Application Filing
- 2009-12-02 JP JP2011544143A patent/JPWO2011067835A1/ja active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2005072771A (ja) * | 2003-08-21 | 2005-03-17 | Nippon Soken Inc | 超音波センサ |
JP2006345271A (ja) * | 2005-06-09 | 2006-12-21 | Nippon Ceramic Co Ltd | 超音波送受波器 |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2014027516A (ja) * | 2012-07-27 | 2014-02-06 | Nippon Ceramic Co Ltd | 超音波送受波器 |
WO2017141402A1 (ja) * | 2016-02-18 | 2017-08-24 | 三菱電機株式会社 | 超音波送受信装置、壁部材、および、壁部材への超音波センサの取付方法 |
JPWO2017141402A1 (ja) * | 2016-02-18 | 2018-02-22 | 三菱電機株式会社 | 超音波送受信装置、壁部材、および、壁部材への超音波センサの取付方法 |
Also Published As
Publication number | Publication date |
---|---|
DE112009005416T5 (de) | 2012-12-13 |
US20120269039A1 (en) | 2012-10-25 |
JPWO2011067835A1 (ja) | 2013-04-18 |
CN102667523A (zh) | 2012-09-12 |
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