| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 急减速状态传感器及其信号控制电路及急刹车灯 | CN98814167.1 | 1998-09-04 | CN1107873C | 2003-05-07 | 李捷逵 |
| 本发明提出了一种急减速状态传感器，包括一个由绝缘材料制成的内部为一个密闭的空心弧面槽的绝缘外壳，在所述的空心弧面槽中注有少许水银，在车辆行驶当中随着车速的变化，水银可以沿着所述的弧面在弧面槽中前后自由地移动，从而导通和断开相邻的金属触点，产生相应的状态信号。本发明还提出了采用这种急减速状态传感器的急刹车灯。它的启动与关闭，不受司机的过失、伤亡所制约，全部实现自动化，有效地避免了车辆追尾事故。 | ||||||
| 2 | 急减速状态传感器及其信号控制电路及急刹车灯 | CN98814167.1 | 1998-09-04 | CN1301348A | 2001-06-27 | 李捷逵 |
| 本发明提出了一种急减速状态传感器,包括一个由绝缘材料制成的内部为一个密闭的空心弧面槽的绝缘外壳,在所述的空心弧面槽中注有少许水银,在车辆行驶当中随着车速的变化,水银可以沿着所述的弧面在弧面槽中前后自由地移动,从而导通和断开相邻的金属触点,产生相应的状态信号。本发明还提出了采用这种急减速状态传感器的急刹车灯。它的启动与关闭,不受司机的过失、伤亡所制约,全部实现自动化,有效地避免了车辆追尾事故。 | ||||||
| 3 | Acceleration actuated switch and a method of manufacturing the same | JP3173789 | 1989-02-12 | JP2543759B2 | 1996-10-16 | UBUKATA SUSUMU; MIZUTANI YASUKAZU; SHIBATA MOICHI |
| 4 | Acceleration responsive switch and manufacture thereof | JP3173789 | 1989-02-12 | JPH02213017A | 1990-08-24 | UBUKATA SUSUMU; MIZUTANI YASUKAZU; SHIBATA MOICHI |
| PURPOSE: To maintain stability and high reliability for years for a switch by providing a portion where an amalgam is surely formed with quicksilver, on the point of an electrode inside the metallic container, inner surface of which is made rough. CONSTITUTION: A conductive liquid 3 such as quicksilver that is inertial and works as an electric contact point is sealed air-tight in a hard metallic container 2A, whose inner atmosphere is so formed as not to contaminate quicksilver such as inert gas. On the point of an electrode 2F provided a portion where an amalgam with the quicksilver is surely formed, while the inner surface of the metallic container 2A is made rough so as not to generate the state of short-circuit even when an insulating distance between the amalgam portion of the electrode 2F and the container 2A is shorter than that between the amalgam portion of each electrode. Malfunction does not occur for the oscillatory acceleration, especially the vertical one that is received by a switch during normal running. For the acceleration, primarily the horizontal big one that is generated during collision, the contact is closed in a short period of time, and through the time necessary for the actuation of an air bag, etc., the contact is surely held in a closed state. COPYRIGHT: (C)1990,JPO&Japio | ||||||
| 5 | JPS4984340A - | JP12008373 | 1973-10-26 | JPS4984340A | 1974-08-13 | |
| 6 | BLUNT IMPACT INDICATOR METHODS | EP17206396.8 | 2015-06-26 | EP3312580A2 | 2018-04-25 | GEORGESON, Gary E.; TAPIA, William Joseph |
Systems and methods using fluid-filled hollow microspheres to assist in monitoring or indicating high-energy blunt impacts on structures such as aircraft. A multiplicity of microspheres may be adhered to or embedded in a coating applied on a surface of a substrate (e.g., a tape or an appliqué), which substrate in turn can be adhered to a surface of a structure to be monitored. The microspheres are designed to rupture at one or more specified pressure thresholds. In some embodiments, the microspheres are filled with electrically conductive fluid which, if released from ruptured microsphere, changes the electromagnetic state of the substrate. In response to the detection of a sufficiently large change in the electromagnetic state of the substrate, a blunt impact indication is generated. The impact site may then undergo nondestructive inspection.
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| 7 | Light-emitting deceleration and stopping indicator for motor vehicles | EP88830297.3 | 1988-07-12 | EP0299933A2 | 1989-01-18 | Plozner, Lisio |
The transducer (10) includes a casing (12) which defines an essentially L-shaped cavity having a substantially horizontal lower arm (16) and a substantially vertical ascending arm (18); a volume of mercury (A) which, in the rest condition, occupies the lower arm (16) and essentially does not occupy the ascending arm (18); an input electrode (30) which penetrates the lower arm (16) from the outside and is permanently immersed in the mercury (A), and a series of separate output electrodes (28₁ ... 28₇) which are spaced along the ascending arm (18) and can be reached in succession by the mercury (A) when it rises in the ascending arm (18) due to an inertial force directed along the lower arm (16) towards the ascending arm (18). The indicator (50) includes an elongate hollow body (52) provided with means (58) for fixing to the bodywork of a motor vehicle and carrying an array of electrical light units (921S...926S, 921D...926D) spaced along its length. These units are aligned transverse the vehicle and face rearwardly with respect to the direction of travel. An inertial transducer such as that defined above is mounted in the hollow body (52) and its output electrodes are each connected to at least one of the light units. |
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| 8 | Acceleration sensor | JP27948889 | 1989-10-26 | JPH03140875A | 1991-06-14 | TANAKA HIROSHI |
| PURPOSE: To make an acceleration sensor conduct an accurate switching operation even in a cryogenic environment by putting a conductive substance in an insulative hermetically-sealed container and by heating the conductive substance. CONSTITUTION: A mercury grain 2 as a conductive substance is put movably in an insulative hermetically-sealed container 1, which is fitted and fixed on a horizontal surface 5a of a fitting body 5 so that it is inclined at a prescribed angle θ to the surface. A heating body 4 is fitted to the fitting body 5 so that it is in proximity to the lower end part of the container 1, and two lead wires 8 are extended from the heating body 4 and connected to an electric circuit not shown in the figure. The electric circuit 5 electrifies the heating body 4 through the lead wires 8 at all times in a cryogenic temperature, so as to heat the mercury grain 2 in the container 1. Thereby the mercury grain 2 can be kept at the temperature of a melting point or above, even in the cryogenic temperature. Accordingly, the mercury grain 2 in the container 1 is kept in a state of liquid even when an acceleration sensor is employed in a cryogenic environment, and therefore the acceleration sensor conducts a reliable switching operation. COPYRIGHT: (C)1991,JPO&Japio | ||||||
| 9 | JPH0223811B2 - | JP10457683 | 1983-06-10 | JPH0223811B2 | 1990-05-25 | UBUKATA SUSUMU; MIZUTANI YASUKAZU |
| 10 | Impact switch | JP22709383 | 1983-12-02 | JPS6050830A | 1985-03-20 | RICHIYAADO II IEOMAN |
| 11 | JPS5247826B2 - | JP12008373 | 1973-10-26 | JPS5247826B2 | 1977-12-05 | |
| 12 | 감속 및 정지를 나타내는 자동차용 발광인디케이터 | KR1019880008962 | 1988-07-16 | KR1019960013177B1 | 1996-09-30 | 리시오플로즈네르 |
| 내용없음 | ||||||
| 13 | 블런트 충격 표시 방법 | KR1020150093198 | 2015-06-30 | KR1020160098002A | 2016-08-18 | 게리이.조지슨; 윌리암조셉타피아 |
| 항공기와같은구조물상의고에너지블런트충격을모니터링하거나표시하는것을돕기위하여유체로채워진할로우마이크로스피어를이용하는시스템및 방법. 복수의마이크로스피어가서브스트레이트(예컨대, 테이프또는아플리케)의표면상에적용된코팅에부착되거나내장될수 있으며, 서브스트레이트는모니터링될구조물의표면에부착될수 있다. 마이크로스피어는하나이상의특정된압력한계값에서파열되도록설계된다. 몇몇실시예에서, 마이크로스피어는전기전도성유체로채워지는데, 이전기전도성유체는파열된마이크로스피어로부터유출되면서브스트레이트의전자기상태를변화시킨다. 서브스트레이트의전자기상태의충분히큰 변화의검출에반응하여, 블런트충격표시가생성된다. 이후, 충격지점은비파괴검사를거칠수 있다. | ||||||
| 14 | BLUNT IMPACT INDICATOR METHODS | EP15174164.2 | 2015-06-26 | EP2977737A2 | 2016-01-27 | GEORGESON, Gary E.; TAPIA, William Joseph |
Systems and methods using fluid-filled hollow microspheres to assist in monitoring or indicating high-energy blunt impacts on structures such as aircraft. A multiplicity of microspheres may be adhered to or embedded in a coating applied on a surface of a substrate (e.g., a tape or an appliqué), which substrate in turn can be adhered to a surface of a structure to be monitored. The microspheres are designed to rupture at one or more specified pressure thresholds. In some embodiments, the microspheres are filled with electrically conductive fluid which, if released from ruptured microsphere, changes the electromagnetic state of the substrate. In response to the detection of a sufficiently large change in the electromagnetic state of the substrate, a blunt impact indication is generated. The impact site may then undergo nondestructive inspection.
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| 15 | Light-emitting deceleration and stopping indicator for motor vehicles | EP88830297.3 | 1988-07-12 | EP0299933B1 | 1994-08-31 | Plozner, Lisio |
| 16 | Light-emitting deceleration and stopping indicator for motor vehicles | EP88830297.3 | 1988-07-12 | EP0299933A3 | 1990-06-20 | Plozner, Lisio |
The transducer (10) includes a casing (12) which defines an essentially L-shaped cavity having a substantially horizontal lower arm (16) and a substantially vertical ascending arm (18); a volume of mercury (A) which, in the rest condition, occupies the lower arm (16) and essentially does not occupy the ascending arm (18); an input electrode (30) which penetrates the lower arm (16) from the outside and is permanently immersed in the mercury (A), and a series of separate output electrodes (28₁ ... 28₇) which are spaced along the ascending arm (18) and can be reached in succession by the mercury (A) when it rises in the ascending arm (18) due to an inertial force directed along the lower arm (16) towards the ascending arm (18). The indicator (50) includes an elongate hollow body (52) provided with means (58) for fixing to the bodywork of a motor vehicle and carrying an array of electrical light units (921S...926S, 921D...926D) spaced along its length. These units are aligned transverse the vehicle and face rearwardly with respect to the direction of travel. An inertial transducer such as that defined above is mounted in the hollow body (52) and its output electrodes are each connected to at least one of the light units. |
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| 17 | Schalteinrichtung für eine rotierende Zahnbürste | EP84101612.4 | 1984-02-16 | EP0121695B1 | 1987-05-20 | Benz, Dieter Dr. |
| 18 | Schalteinrichtung für eine rotierende Zahnbürste | EP84101612.4 | 1984-02-16 | EP0121695A1 | 1984-10-17 | Benz, Dieter Dr. |
Die Erfindung betrifft eine Schalteinrichtung für eine von einem Elektromotor angetriebene, rotierende Zahnbürste, die ein rechteckiges Gehäuse aufweist, wobei im Gehäuse ein Quecksilberschwerkraftschalter und außen auf dem Gehäuse ein manuell zu betätigender Schalter vorgesehen sind. Als Quecksilberschwerkraftschalter wird mindestens ein Sensor (1) verwendet, der auf einem beidendig geschlossenen Röhrchen (3) mit Böden (4, 5) besteht, wobei den Boden (4) seitlich ein Leiterdraht (6) und in gleicher Weise den Boden (5) ein Leiterdraht (7) durchgreift und wobei den Boden (5) ein weiterer Leiterdraht (8) durchgreift, dessen Bereich (8a) im Röhrchen (3) im Abstand von der Wandung (3a) und vom Leiterdraht (7) sowie zu diesem parallel verlaufend angeordnet ist und der länger als der Leiterdraht (7) ausgeführt ist dergestalt, daß er das Ende des Bereichs (6a) zum Boden (4) hin überragt. |
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| 19 | BLUNT IMPACT INDICATOR METHODS | EP17206396.8 | 2015-06-26 | EP3312580A3 | 2018-06-13 | GEORGESON, Gary E.; TAPIA, William Joseph |
Systems and methods using fluid-filled hollow microspheres to assist in monitoring or indicating high-energy blunt impacts on structures such as aircraft. A multiplicity of microspheres may be adhered to or embedded in a coating applied on a surface of a substrate (e.g., a tape or an appliqué), which substrate in turn can be adhered to a surface of a structure to be monitored. The microspheres are designed to rupture at one or more specified pressure thresholds. In some embodiments, the microspheres are filled with electrically conductive fluid which, if released from ruptured microsphere, changes the electromagnetic state of the substrate. In response to the detection of a sufficiently large change in the electromagnetic state of the substrate, a blunt impact indication is generated. The impact site may then undergo nondestructive inspection.
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| 20 | BLUNT IMPACT INDICATOR METHODS | EP15174164.2 | 2015-06-26 | EP2977737B1 | 2018-02-14 | GEORGESON, Gary E.; TAPIA, William Joseph |
| Systems and methods using fluid-filled hollow microspheres to assist in monitoring or indicating high-energy blunt impacts on structures such as aircraft. A multiplicity of microspheres may be adhered to or embedded in a coating applied on a surface of a substrate (e.g., a tape or an appliqué), which substrate in turn can be adhered to a surface of a structure to be monitored. The microspheres are designed to rupture at one or more specified pressure thresholds. In some embodiments, the microspheres are filled with electrically conductive fluid which, if released from ruptured microsphere, changes the electromagnetic state of the substrate. In response to the detection of a sufficiently large change in the electromagnetic state of the substrate, a blunt impact indication is generated. The impact site may then undergo nondestructive inspection. | ||||||
