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1.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：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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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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4.发明授权公开(公告)号：US09355542B2
公开(公告)日：2016-05-31
申请号：US14164409
申请日：2014-01-27
Applicant: KIDDE TECHNOLOGIES, INC.
Inventor： Ken Bell , Robert Thebert
CPC classification number: G08B17/12 , G01J5/0014 , G01J5/04 , G01J5/0803 , G01J5/0896 , G01J5/10 , G01J5/522 , G01J5/54 , G08B17/113 , G08B29/145
Abstract: An integral testing system for testing OFDs is provided. The OFD may comprise a body, a detector, and an infrared source. The detector and the infrared source may be housed with the body. The infrared source may be configured to generate emissions having one or more infrared wavelengths that are detectable by the detector. The infrared source may be configured to produce infrared emissions to simulate flaming fire.
Abstract translation: 提供了一个用于测试OFD的集成测试系统。 OFD可以包括身体，检测器和红外源。 检测器和红外源可以与身体一起容纳。 红外源可以被配置为产生具有可被检测器检测的一个或多个红外波长的发射。 红外源可以被配置为产生红外发射以模拟火焰发射。
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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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Patent Agency Ranking
6.发明授权公开(公告)号：US09410849B2
公开(公告)日：2016-08-09
申请号：US14160269
申请日：2014-01-21
Applicant: Kidde Technologies, Inc.
Inventor： Ken Bell , Robert Thebert
CPC classification number: G01J5/0265 , G01J5/0014 , G01J5/028 , G01J5/0806 , G01J5/084 , G01J5/0896 , G01J5/522 , G08B17/12 , G08B29/145
Abstract: A testing device for testing infrared OFDs is provided. The testing device may comprise a body, an infrared source, a controller and a user input. The infrared source may be housed with the body. The controller may be operatively coupled to the infrared source. The controller may also be integral to the infrared source. The user input may be operatively coupled to at least one of the controller and the infrared source. The testing device may be configured to produce infrared emissions to simulate flaming fire.
Abstract translation: 提供了一种用于测试红外线OFD的测试设备。 测试装置可以包括主体，红外源，控制器和用户输入。 红外源可以与身体一起容纳。 控制器可以可操作地耦合到红外源。 控制器也可以与红外源成一体。 用户输入可以可操作地耦合到控制器和红外源中的至少一个。 测试装置可以被配置为产生红外发射以模拟火焰发射。
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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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公开(公告)号：US20150336681A1
公开(公告)日：2015-11-26
申请号：US14285304
申请日：2014-05-22
Applicant: Kidde Technologies, Inc.
Inventor： Mark T. Kern , Ken Bell , Aaron Stanley Rogers
IPC: B64D45/00
CPC classification number: B64D45/00 , A62C3/08 , B64D2045/0085 , B64D2045/009 , F01D17/085 , F01D21/003 , F01D21/12 , F05D2260/80 , F05D2260/83 , G01J5/0014 , G01J5/025
Abstract: An overheat sensor system is provided. A controller may create an aircraft temperature profile and may compare temperature sensor data to the profile. The system may provide an output indicating temperatures or fires.
Abstract translation: 提供过热传感器系统。 控制器可以创建飞机温度曲线，并且可以将温度传感器数据与轮廓进行比较。 系统可以提供指示温度或火灾的输出。
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公开(公告)号：US20170336269A1
公开(公告)日：2017-11-23
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
IPC: G01K11/32
CPC classification number: G01K11/3206 , G01K11/32 , G01K2011/322 , G01L1/242
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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