Patents Assigned to Honeywell International Inc.
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Patent number: 7713653Abstract: Improved portable power sources such as batteries, fuel cells, power generators and the like can include structure or apparatus that are adapted to provide an indication of the power capacity remaining within the portable power source. In some cases, these power sources may be configured to accommodate remote communication regarding their remaining power capacity.Type: GrantFiled: October 6, 2006Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventors: Steven J. Eickhoff, Chunbo Zhang
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Patent number: 7714880Abstract: Combining one or more spatio-temporal sensors with a personal digital assistant or similar small electronic device and with sliding window (roaming and stabilization) software and memory management and user interface functions, to enable a user to see documents and objects that appear to be fixed in space. This may allow the user to navigate using his or her eidetic memory. Navigation of images, documents or other objects substantially bigger than the display is made easier and faster. Using the invention, the user scrolls and views larger documents or objects as if they were affixed in space to a selected viewing platform. The viewing platform can correspond to, for example, the ground, a building, a wall, an arbitrary reference point, or any other suitable fixed or substantially fixed position or object. The invention uses and adjusts for the body-arm-hand-finger motion of the user so that the imagery appears affixed to the selected reference platform.Type: GrantFiled: April 18, 2002Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventor: Michael J. Johnson
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Patent number: 7714774Abstract: A false lock filter circuit for a pulsed altimeter is provided. The circuit includes a low pass filter having a relatively low bandwidth (LBW LPF), a low pass filter having a relatively high bandwidth (HBW LPF) and a false lock controller. The LBW LPF has an input that is coupled to receive a detector output. The HBW LPF has an input that is coupled to receive the detector output. The false lock controller is coupled to receive outputs from the LBW LPF and HBW LPF. Moreover, the false lock controller is configured to sample an output of the HBW LPF and apply a statistical analysis on the samples to determine if a valid target has been detected.Type: GrantFiled: September 6, 2007Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventor: Benjamin J. Winstead
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Patent number: 7713425Abstract: An oil management system and oil filter utilized in association with an internal combustion engine. The oil filter comprises high-efficiency filtration media for filtering engine oil associated with the internal combustion engine. At least one type of time release additive can be impregnated into the filtration media, wherein the time release additives are automatically released into the engine oil filter from filtration media in order to replenish additives already present in the engine oil. Additionally, a sensor module can be provided that monitors oil quality and oil filter efficiency through detecting one or more attributes of the engine oil filtered through the filtration media of oil filter in order to efficiently conserve and manage the oil and reduce the interval of oil changes thereof by extending the life of the engine oil through the replenishment of the additives present in the engine oil and higher filtration effectiveness of the filter.Type: GrantFiled: May 11, 2005Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventors: Todd Hanson, Gary B. Zulauf
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Patent number: 7716480Abstract: In one embodiment, a network comprises a plurality of nodes that communicate with one another. A first node included in the plurality of nodes generates a plan comprising a plurality of marker states. Each marker state comprises a value for a property associated with the first node. When the first node broadcasts information indicative of a given marker state included in the plan, at least one node other than the first node verifies the value of the property included in the given marker state.Type: GrantFiled: July 15, 2005Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventor: Subhas Kumar Ghosh
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Patent number: 7715308Abstract: A wireless network comprises a plurality of nodes that communicate over wireless communication links. A virtual site is established at a primary node included in the plurality of nodes. A backup node is selected for the virtual site from the plurality of nodes. When the primary node is able to do so, the primary node performs predetermined processing for the virtual site and replicates at the backup node data related to the processing. When the primary node is unable to perform the processing, the backup node performs the processing for the virtual site using at least some of the data replicated at the backup node.Type: GrantFiled: December 9, 2004Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventor: Lakshmi Ramaswamy
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Patent number: 7712677Abstract: An improved heater and method of controlling the same is provided. The water heater has the combination of a tank for holding water, a heater for heating the water, a controller having logic to regulate the heater, and first and second sensors. Each of the sensors detects the water temperature at different areas within the water heater. The sensors also provide the controller with signals corresponding to the detected water temperature. In response to these signals, the controller regulates the heater when at least one of the signals of the first and second sensors satisfies at least one predetermined state condition.Type: GrantFiled: August 3, 2004Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventors: Sybrandus B. V. Munsterhuis, Brent Chian, Timothy J. Nordberg
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Patent number: 7712842Abstract: A method of mounting a hubcap on a wheel that involves providing a wheel having an annular hub surrounding an axis of rotation, the hub including a first periphery extending along the circumference of a circle surrounding the axis of rotation and a second periphery spaced from the circumference of the circle, providing a hubcap having a top wall and a cylindrical sidewall extending from the top wall, the cylindrical sidewall having an end edge spaced from the top wall and a circumferential flange projecting from the cylindrical side wall, the circumferential flange having a sidewall and an alignment tab projecting from the sidewall, aligning the hubcap alignment tab with the second periphery, placing the hubcap sidewall against the hub and the alignment tab over the second periphery, and clamping the hubcap to the wheel. Also a wheel (10, 80) including a hubcap (30, 90) and a clamp (50).Type: GrantFiled: October 30, 2006Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventors: Charles A. Parker, Matthew D. Spray, David D. McAfee, Andrew S. Haynes, Todd R. Auel, Steve Hodge
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Patent number: 7714770Abstract: A method and apparatus for dealing with noise spikes in a radar system is provided. The method includes monitoring a noise channel in the radar system. Controlling gain with a control loop based at least in part on the monitored noise channel and ignoring noise spikes detected in the noise channel when controlling gain with the control loop.Type: GrantFiled: July 16, 2007Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventor: Benjamin J. Winstead
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Patent number: 7715014Abstract: Systems and methods for performing vibration error suppression in a fiber optic gyro sensor. An example system includes a light source, a sensing loop assembly, a photo detector, and a processing component. The light source generates a light signal that is then modulated by the sensing loop assembly and applied to a fiber optic coil in the assembly. The photo detector receives a modulated light signal that is an output of the sensing loop assembly (coil) and generates an analog signal. The processing component converts the generated analog signal into a modulated digital signal, determines an average of the modulated digital signal, determines an intensity modulation amplitude based on the determined average of the modulated digital signal, and re-scales the modulated digital phase signal based on the determined intensity modulation amplitude.Type: GrantFiled: March 6, 2007Date of Patent: May 11, 2010Assignee: Honeywell International Inc.Inventor: Chung-Jen Chen
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Publication number: 20100110447Abstract: A system and method includes a tunable light source and a gas cell configured to detect the presence of gases at terahertz frequencies. The light source is operable to emit a light signal at terahertz frequencies. The gas cell includes at least two high frequency mirrors adapted to reflect signals at terahertz frequencies. The gas cell is adapted to be tuned based on the frequency of the emitted light to obtain a Fabry-Perot resonance of the reflected light signal. A pair of detectors are operable to detect the original light signal and the light signal reflected through absorption paths in the gas cell. The system and method are operable to determine a presence and identity of a gas present in the gas cell.Type: ApplicationFiled: October 30, 2008Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: James Allen Cox, Barrett E. Cole
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Publication number: 20100113322Abstract: An azeotrope-like composition consisting essentially of 1,1,2,3-tetrachloropropene and hydrogen fluoride is provided, as well as methods that involve such an azeotrope-like composition.Type: ApplicationFiled: October 28, 2009Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: HSUEH S. TUNG, HANG T. PHAM, RAJIV R. SINGH, DANIEL C. MERKEL, ROBERT JOHNSON
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Publication number: 20100114408Abstract: The present invention provides methods and systems for adjusting video quality outputted by an aerial vehicle to manage the data stream bandwidth to match the needs of each mission segment. A mission segment is monitored in order to determine a preferred video quality of service. A quality of service is set based on the monitored mission segment. The quality of service is selectively altered based on a change of at least one of a mission segment or an environmental condition.Type: ApplicationFiled: October 31, 2008Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventor: Emray R. Goossen
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Publication number: 20100107737Abstract: Sensor apparatus includes a housing, a probe mounted to the housing, the probe including an elongate first part and a helical coil second part conductively coupled to each in series with first and second terminals at opposite ends thereof, the probe to be inserted into an exhaust stream in an exhaust corridor; and a circuit coupled to the first and second terminals of the sensor probe, to selectively operate the probe as a temperature sensor in a first mode and as a PM sensor in a second mode.Type: ApplicationFiled: November 5, 2008Publication date: May 6, 2010Applicant: Honeywell International Inc.Inventors: Brian C. Krafthefer, Gregory E. Stewart, Jeff Boehler, Matthew Below, Michael L. Rhodes
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Publication number: 20100107591Abstract: Methods and apparatus are provided for detecting a flameout of an operating turbomachine that is configured to receive a controlled flow of bleed air from a bleed air source and a controlled flow of fuel from a fuel source. A value of an operational parameter within the turbomachine is detected and a determination is made as to whether it has varied by a predetermined amount. If the operational parameter has varied by the predetermined amount, a flameout confirmation test is triggered. The flameout confirmation test includes holding the controlled flow of bleed air constant, commanding an increase in turbomachine speed, and confirming that a flameout has occurred by detecting that the controlled fuel flow to the turbomachine is at a maximum fuel flow limit and that actual turbomachine speed differs from the commanded turbomachine speed by a predetermined speed error.Type: ApplicationFiled: November 6, 2008Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Matthew Christopher, Hanif Vhora
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Publication number: 20100111691Abstract: A turbine engine component includes a shaft and two sets of hollow radial plates. The shaft includes an axial section forming a portion of a main passage having a substantially uniform diameter. The axial section has two ends and a center located substantially halfway between the two ends. The first set of hollow radial plates extends radially outwardly from the shaft at a first axial location between the center and a first end of the axial section. Each hollow radial plate is hollow and has an interior surface defining annular chambers surrounding and in flow communication with the main passage. The second set of hollow radial plates extends radially outwardly from the shaft at a second axial location between the center and a second end of the axial section. Each hollow radial plate has an interior surface defining annular chambers surrounding and in flow communication with the main passage.Type: ApplicationFiled: November 6, 2008Publication date: May 6, 2010Applicant: Honeywell International Inc.Inventors: Thomas D. Heywood, Edward S. Wright, James D. Prost
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Publication number: 20100108353Abstract: Methods are provided for producing an attrition-resistant, flexible, insulated wire well-suited for use in a high temperature operating environment. In one embodiment, the method includes the steps of providing a conductor, preparing a dielectric coating, applying the dielectric coating over the conductor, and curing the coated conductor. The dielectric coating includes an organic binder, a dielectric material, and an inorganic lubricant.Type: ApplicationFiled: November 3, 2008Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Mark Kaiser, Devlin M. Gualtieri, Mariola Jolanta Proszowski, Alexander Bershitsky
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Publication number: 20100109975Abstract: Methods and system for operating a near-to-eye (NTE) display movably coupled to a headset are provided. Information representative of at least one spatial degree of freedom of the NTE display relative to at least one spatial degree of freedom of the headset is received. Spatial coordinates of the NTE display are determined based on said received information. The NTE display is controlled based on the spatial coordinates of the NTE display.Type: ApplicationFiled: October 30, 2008Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventor: Brent D. Larson
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Publication number: 20100113149Abstract: Embodiments include methods and apparatus for displaying images of an external environment, such as an external environment of an aircraft during flight. An embodiment of a display system includes an image sensor and a processing subsystem. The image sensor is adapted to produce sensed image data based on detected electromagnetic energy from a field of view of the external environment. The sensed image data registers within a first area of a display matrix, and the processing subsystem is adapted to identify a feature that registers within the first area. The processing subsystem is also adapted to determine parameters defining a second, smaller area of the display matrix that is positioned in proximity to the feature, and to generate a display signal to include information representing a sensor-based image corresponding to the sensed image data that registers within the second area.Type: ApplicationFiled: October 31, 2008Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: John G. Suddreth, Thea L. Feyereisen
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Publication number: 20100108809Abstract: A strut support system for a ducted fan unmanned aerial vehicle to suppress noise comprising: a ducted fan fuselage that defines an opening; an engine that extends longitudinally through the opening in the fuselage; a drive mechanism rotatably mounted to the engine, wherein a fan is mounted on the drive mechanism within a duct defined by the opening; and a plurality of struts extending between the ducted fan fuselage and the engine each comprising a first leg and a second leg joined together by a curvilinear junction, wherein the first leg is attached to the ducted fan fuselage and the second leg is attached to the engine, wherein the plurality of struts are positioned upstream of the fan, wherein the junction between the first leg of each of the plurality of struts and the ducted fan fuselage is outside the highlight of the ducted fan fuselage's leading edge.Type: ApplicationFiled: October 31, 2008Publication date: May 6, 2010Applicant: HONEYWELL INTERNATIONAL INC.Inventors: Bruce Dan Bouldin, Ricardo Burdisso