Patents by Inventor Nobuaki HAYAKAWA
Nobuaki HAYAKAWA has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 9696726Abstract: An orbit attitude control device includes a plurality of nozzles for injecting combustion gas supplied from a combustion chamber, and a control section configured to calculate nozzle opening degree correction values so that a deviation between a detection value of the pressure of the combustion chamber and a command value becomes smaller. The control section is configured to calculate a total correction value so that the deviation between the detection value and the command values becomes smaller. A total value T1 for first group nozzles and a total value T2 for second group nozzles are calculated. The total correction value is distributed to the opening degree correction values for the first group nozzles with a ratio of T2/(T1+T2) and to the opening degree correction values for the second group nozzles with a ratio of T1/(T1+T2).Type: GrantFiled: February 26, 2016Date of Patent: July 4, 2017Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.Inventors: Toshiharu Fujita, Nobuaki Hayakawa
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Patent number: 9469419Abstract: An orbit attitude control device includes a plurality of nozzles and a control section. The nozzles inject a combustion gas supplied from a combustion chamber, opening degrees being controlled in accordance with opening degree command values. The control section calculates nozzle opening degree correction values for the opening degree command values in response to a detection value of a pressure of the combustion chamber and a command value for the pressure, and correct the opening degree command values by the nozzle opening degree correction values. Each nozzle opening degree correction value is determined based on each opening degree command value.Type: GrantFiled: September 5, 2013Date of Patent: October 18, 2016Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.Inventors: Toshiharu Fujita, Nobuaki Hayakawa
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Publication number: 20160179099Abstract: An orbit attitude control device includes a plurality of nozzles for injecting combustion gas supplied from a combustion chamber, and a control section configured to calculate nozzle opening degree correction values so that a deviation between a detection value of the pressure of the combustion chamber and a command value becomes smaller. The control section is configured to calculate a total correction value so that the deviation between the detection value and the command values becomes smaller. A total value T1 for first group nozzles and a total value T2 for second group nozzles are calculated. The total correction value is distributed to the opening degree correction values for the first group nozzles with a ratio of T2/(T1+T2) and to the opening degree correction values for the second group nozzles with a ratio of T1/(T1+T2).Type: ApplicationFiled: February 26, 2016Publication date: June 23, 2016Inventors: Toshiharu FUJITA, Nobuaki HAYAKAWA
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Patent number: 9365300Abstract: An orbit attitude control device includes a plurality of nozzles for injecting combustion gas supplied from a combustion chamber, and a control section configured to calculate nozzle opening degree correction values so that a deviation between a detection value of the pressure of the combustion chamber and a command value becomes smaller. The control section is configured to calculate a total correction value so that the deviation between the detection value and the command values becomes smaller. A total value T1 for first group nozzles and a total value T2 for second group nozzles are calculated. The total correction value is distributed to the opening degree correction values for the first group nozzles with a ratio of T2/(T1+T2) and to the opening degree correction values for the second group nozzles with a ratio of T1/(T1+T2).Type: GrantFiled: September 5, 2013Date of Patent: June 14, 2016Assignee: Mitsubishi Heavy Industries, Ltd.Inventors: Toshiharu Fujita, Nobuaki Hayakawa
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Patent number: 9302790Abstract: An orbit attitude control device includes a plurality of nozzles for injecting combustion gas supplied from a combustion chamber, and a control section configured to calculate nozzle opening degree correction values so that a deviation between a detection value of the pressure of the combustion chamber and a command value becomes smaller. The control section is configured to calculate a total correction value so that the deviation between the detection value and the command values becomes smaller. A total value T1 for first group nozzles and a total value T2 for second group nozzles are calculated. The total correction value is distributed to the opening degree correction values for the first group nozzles with a ratio of T2/(T1+T2) and to the opening degree correction values for the second group nozzles with a ratio of T1/(T1+T2).Type: GrantFiled: September 5, 2013Date of Patent: April 5, 2016Assignee: Mitsubishi Heavy Industries, Ltd.Inventors: Toshiharu Fujita, Nobuaki Hayakawa
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Patent number: 9242745Abstract: An orbit attitude control device includes a divert thruster including a plurality of nozzles. First group nozzles inject combustion gas in opposite directions along a first axis. Second group nozzles inject combustion gas in opposite directions along a second axis. A control section calculates correction values for opening degree commands based on a detection value of a pressure of the combustion chamber and a command value of the pressure, and corrects the opening degree command values by the correction values. The device further includes a first axis acceleration sensor for detecting acceleration along the first axis and a second axis acceleration sensor for detecting acceleration along the second axis. The correction values for the opening degrees of the first group nozzles are determined by a first axis acceleration, and the correction values for the opening degrees of the second group nozzles are determined by a second axis acceleration.Type: GrantFiled: September 5, 2013Date of Patent: January 26, 2016Assignee: MITSUBISHI HEAVY INDUSTRIES, LTD.Inventors: Toshiharu Fujita, Nobuaki Hayakawa
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Publication number: 20140145037Abstract: An orbit attitude control device includes a plurality of nozzles for injecting combustion gas supplied from a combustion chamber, and a control section configured to calculate nozzle opening degree correction values so that a deviation between a detection value of the pressure of the combustion chamber and a command value becomes smaller. The control section is configured to calculate a total correction value so that the deviation between the detection value and the command values becomes smaller. A total value T1 for first group nozzles and a total value T2 for second group nozzles are calculated. The total correction value is distributed to the opening degree correction values for the first group nozzles with a ratio of T2/(T1+T2) and to the opening degree correction values for the second group nozzles with a ratio of T1/(T1+T2).Type: ApplicationFiled: September 5, 2013Publication date: May 29, 2014Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.Inventors: Toshiharu FUJITA, Nobuaki HAYAKAWA
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Publication number: 20140145038Abstract: An orbit attitude control device includes a plurality of nozzles and a control section. The nozzles inject a combustion gas supplied from a combustion chamber, opening degrees being controlled in accordance with opening degree command values. The control section calculates nozzle opening degree correction values for the opening degree command values in response to a detection value of a pressure of the combustion chamber and a command value for the pressure, and correct the opening degree command values by the nozzle opening degree correction values. Each nozzle opening degree correction value is determined based on each opening degree command value.Type: ApplicationFiled: September 5, 2013Publication date: May 29, 2014Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.Inventors: Toshiharu FUJITA, Nobuaki HAYAKAWA
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Publication number: 20140145036Abstract: An orbit attitude control device includes a divert thruster including a plurality of nozzles. First group nozzles inject combustion gas in opposite directions along a first axis. Second group nozzles inject combustion gas in opposite directions along a second axis. A control section calculates correction values for opening degree commands based on a detection value of a pressure of the combustion chamber and a command value of the pressure, and corrects the opening degree command values by the correction values. The device further includes a first axis acceleration sensor for detecting acceleration along the first axis and a second axis acceleration sensor for detecting acceleration along the second axis. The correction values for the opening degrees of the first group nozzles are determined by a first axis acceleration, and the correction values for the opening degrees of the second group nozzles are determined by a second axis acceleration.Type: ApplicationFiled: September 5, 2013Publication date: May 29, 2014Applicant: MITSUBISHI HEAVY INDUSTRIES, LTD.Inventors: Toshiharu FUJITA, Nobuaki HAYAKAWA