序号 | 专利名 | 申请号 | 申请日 | 公开(公告)号 | 公开(公告)日 | 发明人 |
---|---|---|---|---|---|---|
121 | Gas flow type angular velocity sensor | EP95120416.3 | 1993-04-07 | EP0713098A2 | 1996-05-22 | Yamakawa, Hiroshi, c/o K.K. Honda Gijyutsu; Ikegami, Masayuki, c/o K.K. Honda Gijyutsu; Hano, Tsuyoshi, c/o K.K. Honda Gijyutsu |
The specification discloses an angular velocity sensor of the type wherein a flow of gas forced by a pump into a gas path in the sensor body through a nozzle hole and directed toward a pair of thermosensitive resistance elements provided in the gas path is deflected by the action of an angular velocity and the deflection of the gas flow is sensed by means of the thermosensitive resistance elements, and which is further provided with a thermostatically--controlled gas path with heating means for keeping the gas flow at a constant temperature with no affection of ambient temperature variations and also provided with a gas path for absorbing pulsations of the gas flow caused by pumping operations. |
||||||
122 | Procédé et dispositif pour minimiser dans un système de mesures inertielles l'erreur due à un mouvement perturbant dans la restitution de la vitesse | EP95402045.9 | 1995-09-11 | EP0704705A1 | 1996-04-03 | Benes, Christian |
La présente invention concerne un procédé et un dispositif (16) pour minimiser dans un système de mesures inertielles à composants liés l'erreur due à un mouvement perturbant quelconque dans la restitution de la vitesse. Selon l'invention, ledit dispositif (16) est relié à un ensemble d'accéléromètres et à un ensemble de gyromètres et il comporte :
|
||||||
123 | Semiconductor type gas rate sensor | EP95103509.6 | 1995-03-10 | EP0672907A2 | 1995-09-20 | Hosoi, Takashi, c/o Kabushiki Kaisha Honda; Inaba, Atsushi, c/o Kabushiki Kaisha Honda; Doi, Mizuho, c/o Kabushiki Kaisha Honda |
A semiconductor type gas rate sensor which is capable of accurately sensing with a sufficient sensitivity an angular velocity acting on its body made of semiconductor substrates having a nozzle port and a gas path etched therein with a pair of heat wires (heat-sensitive resistance elements) provided in the gas path, wherein an optimal flow of gas injected into the gas path through the nozzle port is ensured by designing the nozzle port of 300 to 1000 microns in width and of not less than 2 mm in length and providing the gas path at its inner most position with an outlet allowing the gas to straight flow out from the gas path therethrough. |
||||||
124 | Gas flow type angular velocity sensor | EP95102183.1 | 1995-02-16 | EP0669536A1 | 1995-08-30 | Doi, Mizuho, c/o Kabushiki Kaisha Honda; Nishio, Tomoyuki, c/o Kabushiki Kaisha Honda; Fueki, Nobuhiro, c/o Kabushiki Kaisha Honda |
A gas flow type angular velocity sensor which is capable of reliably sensing an angular velocity while accurately controlling the working gas flow with temperature compensation by using a pair of heat wires as a gas flow sensor without providing any additional gas flow sensor in the sensor body wherein a an angular velocity sensing bridge circuit is provided at its current supply source with a connected in series therewith temperature compensating circuit which is composed of a pair of series or parallel resistance elements: one is a thermosensitive resistance element disposed in a gas path and the other is a reference resistance element disposed outside the gas path. |
||||||
125 | Gas flow type angular velocity sensor | EP92110159.8 | 1992-06-16 | EP0519404B1 | 1995-08-30 | Hosoi, Takashi, c/o K.K. Honda Gijyutsu Kenkyusho; Doi, Mizuho, c/o K.K. Honda Gijyutsu Kenkyusho; Nishio, Tomoyuki, c/o K.K Honda Gijyutsu Kenkyusho; Hiyama, Satoshi, c/o K.K. Honda Gijyutsu Kenkyusho |
126 | LOW FREQUENCY ANGULAR VELOCITY SENSOR | EP92901295 | 1991-11-22 | EP0560880A4 | 1994-11-17 | LAUGHLIN DARREN R |
127 | LOW FREQUENCY ANGULAR VELOCITY SENSOR | EP92901295.0 | 1991-11-22 | EP0560880A1 | 1993-09-22 | LAUGHLIN, Darren, R. |
L'invention décrit un détecteur de vitesse angulaire magnétohydrodynamique. Un boîtier (30) soutient une première et une deuxième masse-étalon de fluide situées dans des passages annulaires coaxiaux respectifs (11, 17), permettant un mouvement relatif entre les masses-étalon et le boîtier. Un premier et un deuxième aimant (12, 18), associés à chaque passage annulaire (11, 17), provoquent la génération d'un potentiel électrique dans chaque passage, proportionnel à la vitesse circulaire relative entre les masses-étalon et le boîtier. Les passages annulaires sont reliés entre eux pour former un circuit de fluide à pompage continu, introduisant une vitesse d'écoulement radial dans chaque passage. A des fréquences de rotation faibles, une composante de vitesse circulaire est induite dans les masses-étalon par accélération de Coriolis, ce qui produit une tension électrique mesurable dans les passages annulaires. La réaction à basse fréquence du détecteur s'étend, de ce fait, à des fréquences inférieures. | ||||||
128 | Gyro apparatus employing a semiconductor device | EP91307677.4 | 1991-08-21 | EP0481594A1 | 1992-04-22 | Kumagai, Hideo, c/o Tamagawa Seiki K. K.; Shiozawa, Tatsuo, Tamagawa Seiki K. K. |
A semiconductor gyro apparatus includes a current supply device (23) for supplying electrical current to a semiconductor device (20) consitituted by a solid-state device, and a voltage detection (26) connected to the semiconductor device (20). The coriolis force exerted on the flow of electrons within the semiconductor device when an angular velocity is imposed on the semiconductor device is detected by the voltage detection device (26) as an electrical voltage. |
||||||
129 | ANGULAR RATE SENTOR. | EP90909764 | 1990-07-05 | EP0486503A4 | 1992-03-30 | DWYER DOUGLAS FRANK GEORGE |
130 | Angular rate sensor nozzle | EP89630021.7 | 1989-02-02 | EP0331602A3 | 1992-03-18 | Lopiccolo, Mario Thomas; Swarts, Richard Ellis |
An angular rate sensor is provided having a specially shaped nozzle (28) which shapes the velocity profile of a gas stream passing through a nozzle so that a linear portion of the profile impinges upon the resistive elements (53,54) of the sensor even when large angular rates of turn in a plane of sensitivity are encountered. The nozzle (28) is generally rectangularly shaped having a pair of parallel sides arranged perpendicularly to the resistive elements (53,54) of the sensor and a pair of connecting sides. |
||||||
131 | Angular velocity sensor | EP89300266.7 | 1989-01-12 | EP0324620B1 | 1992-01-02 | Takahashi, Tsuneo; Nishio, Tomoyuki; Ikegami, Masayuki; Gunji, Takahiro |
132 | Gas flow type angular velocity sensor | EP90112140.0 | 1990-06-26 | EP0405452A2 | 1991-01-02 | Takahashi, Tsuneo; Ikegami, Masayuki; Nishio, Tomoyuki; Gunji, Takahiro |
A gas flow type angular velocity sensor comprising two semiconductor substrates with all components formed thereon by use of a semiconductor technology and an IC technology, which are coupled with each other to form therein a pair of heat wires, a gas path and a nozzle holes for injecting a gas flow toward the paired heat wires in the gas path. Two heat wires of the pair changes their resistance-temperature characteristics in accordance with a deflection of the gas flow due to the action of angular velocity and a difference between two changed values is picked up and amplified by a resistance bridge circuit and an amplifier circuit formed on the semiconductor substrates to produce an output signal proportional to the angular velocity to be measured. A miniature pump formed on semiconductor substrates and drivable by a piezoelectric element provides a stabilized gas flow in the sensor. Thus constructed sensor is compact, accurate and suitable for mass-production and free from disadvantages of conventional sensors. |
||||||
133 | Angular rate sensor nozzle | EP89630021.7 | 1989-02-02 | EP0331602A2 | 1989-09-06 | Lopiccolo, Mario Thomas; Swarts, Richard Ellis |
An angular rate sensor is provided having a specially shaped nozzle (28) which shapes the velocity profile of a gas stream passing through a nozzle so that a linear portion of the profile impinges upon the resistive elements (53,54) of the sensor even when large angular rates of turn in a plane of sensitivity are encountered. The nozzle (28) is generally rectangularly shaped having a pair of parallel sides arranged perpendicularly to the resistive elements (53,54) of the sensor and a pair of connecting sides. |
||||||
134 | Method of manufacturing fluidic angular rate sensor | EP88108523.7 | 1988-05-27 | EP0292999A2 | 1988-11-30 | Takahashi, Fumitaka; Okazaki, Kunio; Shiraishi, Masaru; Takahashi, Masayuki |
A method of manufacturing a fluidic angular rate sensor of the type that fine wires such as tungsten wires are tensely spread over the heads of two pairs of metal supports which are mounted on a ceramic disc having fluid passage apertures, includes the steps of: plating a gold on the wires and fixedly spreading the wires over the metal supports by means of thermocompression bonding or the like; and heating the wires in a predetermined atmosphere which allows the plated gold to be removed and the wires to be crystalized. |
||||||
135 | Angular rate sensor with integrated impulse jet pump assembly | EP81630028.9 | 1981-04-02 | EP0037794B1 | 1985-10-09 | Moffatt, Marston E. |
136 | Angular rate sensor with symmetrical diaphragm impulse pump assembly | EP81630029.7 | 1981-04-02 | EP0037795B1 | 1985-09-18 | Swarts, Richard E. |
137 | Verfahren zur Bestimmung der Drehgeschwindigkeit | EP83111055.6 | 1983-11-05 | EP0111715A1 | 1984-06-27 | Müller, Paul, Dr. rer.nat. |
Gegenstand der Anmeldung ist ein Verfahren zur Messung von Drehgeschwindigkeiten um wenigstens zwei zueinander senkrecht stehende Aschen. Hierzu wird z.B. ein Laserkreisel (1) mit der Drehgeschwindigkeit ωo um eine Hilfsdrehachse (3) gedreht und bei Drehstellungen ωo des Kreisels (1), bei denen eine der Komponenten des Ausgangssignals des Kreisels (1) 0 wird, der Ausgangswert des Kreiselsignals bestimmt. Aus einem sich dabei ergebenden Gleichungssystem lassen sich die Komponenten der gesuchten Drehung errechnen. |
||||||
138 | Angular rate sensor with symmetrical diaphragm impulse pump assembly | EP81630029 | 1981-04-02 | EP0037795A3 | 1982-01-06 | Swarts, Richard E. |
An angular rate sensor includes an improved impulse pump structure (70) for providing fluid under pressure to a nozzle (28) disposed at one end of a jet chamber (29) to form a constant flow fluid jet, the jet chamber (29) including a pair of temperature sensitive elements (53, 54) disposed at the other end in such a manner as to be differentially cooled by the fluid jet in dependence on the angular rotation of the sensor. |
||||||
139 | ゴルフ用具のためのインパクトおよび音響の分析 | JP2016502770 | 2014-03-14 | JP6235692B2 | 2017-11-22 | ハッデン ジェフリー; ソーントン ダグラス エイ.; グレン ブラッドリー シー. |
140 | Recession determination method and vehicle control apparatus for a vehicle | JP33789798 | 1998-11-27 | JP3649007B2 | 2005-05-18 | 裕 川口; 伸芳 杉谷 |