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公开(公告)号：US10585006B2
公开(公告)日：2020-03-10
申请号：US15600049
申请日：2017-05-19
Applicant: Kidde Technologies, Inc.
Inventor： Christopher Wilson , David William Frasure , Mark Thomas Kern , Mark Sherwood Miller , Scott Kenneth Newlin , Chris George Georgoulias , Stefan Coreth , Ken Bell
Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
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公开(公告)号：US20190151692A1
公开(公告)日：2019-05-23
申请号：US16261666
申请日：2019-01-30
Applicant: Kidde Technologies, Inc.
Inventor： David William Frasure , Doug John Baxendell , Christopher Wilson , Terry Simpson , John Wright Porterfield, JR. , Kevin R. Leitch , Michael Lee Davis
Abstract: A safety assembly provided with an automatic fire extinguisher system includes an engagement member, a blocking member, and an extension member. The engagement member is slidably received within an outlet port of a valve housing. A blocking member having a first blocking member portion and a second blocking member portion is at least partially received within a cavity defined by the valve housing. The extension member extends between the engagement member and the blocking member.
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公开(公告)号：US10226656B2
公开(公告)日：2019-03-12
申请号：US15076714
申请日：2016-03-22
Applicant: Kidde Technologies, Inc.
Inventor： David William Frasure , Doug John Baxendell , Christopher Wilson , Terry Simpson , John Wright Porterfield, Jr. , Kevin R. Leitch , Michael Lee Davis
Abstract: A safety assembly provided with an automatic fire extinguisher system includes an engagement member, a blocking member, and an extension member. The engagement member is slidably received within an outlet port of a valve housing. A blocking member having a first blocking member portion and a second blocking member portion is at least partially received within a cavity defined by the valve housing. The extension member extends between the engagement member and the blocking member.
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公开(公告)号：US20170274233A1
公开(公告)日：2017-09-28
申请号：US15076714
申请日：2016-03-22
Applicant: Kidde Technologies, Inc.
Inventor： David William Frasure , Doug John Baxendell , Christopher Wilson , Terry Simpson , John Wright Porterfield, JR. , Kevin R. Leitch , Michael Lee Davis
CPC classification number: A62C35/023 , A62C3/07 , A62C35/13 , A62C35/68
Abstract: A safety assembly provided with an automatic fire extinguisher system includes an engagement member, a blocking member, and an extension member. The engagement member is slidably received within an outlet port of a valve housing. A blocking member having a first blocking member portion and a second blocking member portion is at least partially received within a cavity defined by the valve housing. The extension member extends between the engagement member and the blocking member.
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公开(公告)号：US10436652B2
公开(公告)日：2019-10-08
申请号：US15600130
申请日：2017-05-19
Applicant: Kidde Technologies, Inc.
Inventor： Christopher Wilson , David William Frasure , Mark Thomas Kern , Mark Sherwood Miller , Scott Kenneth Newlin , Chris George Georgoulias , Stefan Coreth , Ken Bell
Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
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Patent Agency Ranking
公开(公告)号：US20170205286A1
公开(公告)日：2017-07-20
申请号：US15001372
申请日：2016-01-20
Applicant: Kidde Technologies, Inc.
Inventor： Mark T. Kern , Ken Bell , Terry Simpson , Christopher Wilson , David Frasure , Charles B. McLean , Clinton E. Piland
CPC classification number: G01J3/0297 , G01J3/10 , G01J3/501 , G01J5/0018 , G01J5/20 , G01J5/60 , G01J2003/102 , G01J2005/0048 , G08B29/145 , H05B33/0845
Abstract: A method for calibrating a test light to simulate a fire includes measuring a baseline resistance induced in a sensor cell of a two-color detector in response to a controlled fire. The method includes monitoring a test resistance induced in the sensor cell in response to exposure to emissions from a test light and adjusting the emissions of the test light until the test resistance of the sensor cell equals the baseline resistance of the sensor cell to achieve a calibration setting for the test light. A test light for a detector includes a housing and a first LED within the housing having a first emission wavelength. A second LED is within the housing. The second LED has a second emission wavelength. The second emission wavelength is different than the first emission wavelength.
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7.发明申请公开(公告)号：US20170336268A1
公开(公告)日：2017-11-23
申请号：US15600049
申请日：2017-05-19
Applicant: Kidde Technologies, Inc.
Inventor： Christopher Wilson , David William Frasure , Mark Thomas Kern , Mark Sherwood Miller , Scott Kenneth Newlin , Chris George Georgoulias , Stefan Coreth , Ken Bell
CPC classification number: G01K11/3206 , B64D2045/0085 , B64D2045/009 , G01K3/005 , G01K11/32 , G01K2011/322 , G01L1/246
Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
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公开(公告)号：US10987530B2
公开(公告)日：2021-04-27
申请号：US16261666
申请日：2019-01-30
Applicant: Kidde Technologies, Inc.
Inventor： David William Frasure , Doug John Baxendell , Christopher Wilson , Terry Simpson , John Wright Porterfield, Jr. , Kevin R. Leitch , Michael Lee Davis
Abstract: A safety assembly provided with an automatic fire extinguisher system includes an engagement member, a blocking member, and an extension member. The engagement member is slidably received within an outlet port of a valve housing. A blocking member having a first blocking member portion and a second blocking member portion is at least partially received within a cavity defined by the valve housing. The extension member extends between the engagement member and the blocking member.
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公开(公告)号：US10184831B2
公开(公告)日：2019-01-22
申请号：US15001372
申请日：2016-01-20
Applicant: Kidde Technologies, Inc.
Inventor： Mark T. Kern , Ken Bell , Terry Simpson , Christopher Wilson , David Frasure , Charles B. McLean , Clinton E. Piland
IPC: H01J40/14 , G01J3/02 , G01J3/10 , G01J3/50 , H05B33/08 , G01J5/00 , G08B29/14 , G01J5/20 , G01J5/60
Abstract: A method for calibrating a test light to simulate a fire includes measuring a baseline resistance induced in a sensor cell of a two-color detector in response to a controlled fire. The method includes monitoring a test resistance induced in the sensor cell in response to exposure to emissions from a test light and adjusting the emissions of the test light until the test resistance of the sensor cell equals the baseline resistance of the sensor cell to achieve a calibration setting for the test light. A test light for a detector includes a housing and a first LED within the housing having a first emission wavelength. A second LED is within the housing. The second LED has a second emission wavelength. The second emission wavelength is different than the first emission wavelength.
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公开(公告)号：US10112726B2
公开(公告)日：2018-10-30
申请号：US15600077
申请日：2017-05-19
Applicant: Kidde Technologies, Inc.
Inventor： Christopher Wilson , David William Frasure , Mark Thomas Kern , Mark Sherwood Miller , Scott Kenneth Newlin , Chris George Georgoulias , Stefan Coreth , Ken Bell
IPC: G01M17/00 , B64D45/00 , G08C23/04 , H04J14/08 , H04J14/02 , H04B10/071 , G07C5/08 , G01K11/32 , G02B6/42 , G02B6/34
Abstract: Overheat and fire detection for aircraft systems includes an optical controller and a fiber optic loop extending from the optical controller. The fiber optic loop extends through one or more zones of the aircraft. An optical signal is transmitted through the fiber optic loop from the optical controller and is also received back at the optical controller. The optical controller analyzes the optical signal to determine the temperature, strain, or both experienced within the zones.
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