Patents Assigned to Systems Control, Inc.
  • Patent number: 9857822
    Abstract: A continuous, always on, high accuracy AC reference signal is added to an AC voltage of interest to calibrate the AC voltage of interest. The AC reference voltage has a first frequency. The AC voltage of interest has a second frequency. A control system having calibration.
    Type: Grant
    Filed: October 15, 2015
    Date of Patent: January 2, 2018
    Assignee: BAE Systems Controls Inc.
    Inventors: Russell M. Petrosky, Stephen J. Gabaly, Patrick Nee
  • Patent number: 9771154
    Abstract: Various embodiments of the present invention relate to an intelligent seat power system in which a plurality of seat nodes are embedded in respective aircraft seats. The seat nodes receive power and commands from a plurality of power supply units, each of which is connected to a cabin management system. The seat nodes are able to monitor and control functionality at the seat, and communicate their status back to the cabin management system.
    Type: Grant
    Filed: February 28, 2014
    Date of Patent: September 26, 2017
    Assignee: BAE Systems Controls Inc.
    Inventor: Robert A. Hess
  • Publication number: 20170219657
    Abstract: A method, battery module, an energy storage device and a power management system is provided. The capacity of the module and energy storage device is determined during current balancing between cells of the module. The capacity is subsequently used to control power to and from the energy storage device to maintain the energy storage device within a predetermined range of the maximum capacity of the energy storage device. The determined capacity is used as a maximum capacity for the energy storage device.
    Type: Application
    Filed: January 28, 2016
    Publication date: August 3, 2017
    Applicant: BAE SYSTEMS Controls Inc.
    Inventor: Robert J. Vovos
  • Patent number: 9705357
    Abstract: A portable generator system provides power to a load source including an engine and a generator. The engine drives the generator to provide a generator alternating current (AC) electrical power output. An energy storage system (ESS) provides an ESS direct current (DC) electrical power output. A first inverter is connected to the generator for receiving the generator AC electrical power output and for providing a DC power output. A second inverter is connected to the first inverter and the ESS for receiving the DC power output from the first inverter and the ESS DC electrical power output for providing an AC power output. A first power mode includes the generator maintaining a first generator power output level corresponding to a specified power requirement of a load source, and the ESS providing an additional first ESS power output level for satisfying the specified power requirement of the load source.
    Type: Grant
    Filed: March 27, 2015
    Date of Patent: July 11, 2017
    Assignee: BAE Systems Controls Inc.
    Inventors: Thomas Apalenek, Gordon Lu, Stephen Pasterski, Thomas Quigley
  • Patent number: 9699841
    Abstract: A full color LED light for aircraft interiors is described, comprising a housing containing at least three differently colored groups of light emitting diodes, a controller for the groups of light emitting diodes and an alternating current power source. The controller distributes the alternating current to LED groups, providing a desired intensity of each differently colored group, producing a desired blended output color. At least one switching circuit receives input current from the power source, via the controller, and directs current to LED subgroups such that a near optimal voltage drop is maintained, given the varied voltage drops of the LED subgroups, regardless of the input voltage, in light of the voltage rating of the LEDs. Embodiments provide for measurement or estimation of current profiles, thermal profiles, and series resistance, allowing accurate measurement of lumen depreciation over time. Additional embodiments include a feedback circuit to temper input power fluctuations.
    Type: Grant
    Filed: April 9, 2015
    Date of Patent: July 4, 2017
    Assignee: BAE Systems Controls Inc.
    Inventor: Felix O. Heimes
  • Patent number: 9689318
    Abstract: An equilibrating flow distributor for a gas turbine engine includes a balancing valve and multiple flow dividers, each with a movable valve or divider member. The balancing valve has an inlet receiving media at a first pressure area and an outlet defining a plurality of first metering orifices. The valve member defines at least one second metering orifice receiving the media at a second pressure area. Each flow divider has an inlet receiving the media through an associated one of the first metering orifices at a third pressure area and an outlet defining one of a plurality of third metering orifices receiving the media at a fourth pressure area. Each flow divider has a second pressure area in communication with second pressure area of the balancing valve. Flow through the fourth pressure area of each flow divider is substantially the same.
    Type: Grant
    Filed: December 2, 2015
    Date of Patent: June 27, 2017
    Assignee: JANSEN'S AIRCRAFT SYSTEMS CONTROLS, INC.
    Inventors: Jerame James Powell, Harvey B. Jansen
  • Patent number: 9645865
    Abstract: One embodiment of the present invention relates to a discrete time method for detection of oscillations in continuous data. Another embodiment of the present invention relates to a discrete time system for detection of oscillations in continuous data. Another embodiment of the present invention relates to a discrete time software program for detection of oscillations in continuous data.
    Type: Grant
    Filed: August 27, 2015
    Date of Patent: May 9, 2017
    Assignee: BAE Systems Controls Inc.
    Inventor: Christopher M. Blain
  • Patent number: 9459300
    Abstract: Various embodiments for detecting a high Intensity radiated field (HIRF) in a line replaceable unit are provided. For example, an internal detector includes at least one antenna attached to a chassis. The at least one antenna is configured and dimensioned to pick up an electromagnetic field. The electromagnetic field induces a current in the at least one antenna proportional to a magnitude of the electromagnetic field. The internal detector also includes a circuit configured to generate a DC signal based on the induced current in the at least one antenna and a processing section configured to compare the DC signal with a threshold and output a result of the comparison to a built-in test section. The internal detector may be used to test EMI filter pin connectors of a closed line replaceable unit.
    Type: Grant
    Filed: February 20, 2015
    Date of Patent: October 4, 2016
    Assignee: BAE Systems Controls Inc.
    Inventors: Paul Hart Heiland, Jr., Richard P. Quinlivan, Thomas Edward Guth, Zain Adam Horning, Peter Joseph Watson, Gustavo Enrique Melendez Velazquez
  • Patent number: 9410523
    Abstract: An inventive system and method for managing vehicle power is presented. The novel technology provides a means to automatically shutdown a vehicle's engine when conditions are such that engine power is not needed, reducing fuel consumption as well as lowering noise and emissions. A series of conditions are examined to determine whether engine power is needed and hence whether shutdown can be safely performed. The inventive system and method can also determine when power is again needed by the engine and can re-start the engine automatically at such times.
    Type: Grant
    Filed: October 9, 2015
    Date of Patent: August 9, 2016
    Assignee: BAE SYSTEMS CONTROLS INC.
    Inventor: James A. Dupuy
  • Patent number: 9354141
    Abstract: A turbine liquid fuel simulator exposes the components of a liquid fuel system in a turbine engine to the same fuel flows and pressures that the liquid fuel system would endure in an actual startup and run sequence, without burning or otherwise emitting the liquid fuel from the system. A fuel porting mechanism, such as a direction control valve, is installed in each combustor of the turbine engine. The fuel porting mechanism is movable from a first position, wherein liquid fuel is delivered to the combustor nozzle to be burned in normal operation, to a second position, wherein the liquid fuel is diverted to return lines that deliver the liquid fuel back to the fuel tank. To simulate the actual pressures and flows, pressure differential orifices can be installed in the return fuel lines. The orifices includes structures that modify the liquid fuel flow to mimic delivery to the nozzle.
    Type: Grant
    Filed: June 17, 2014
    Date of Patent: May 31, 2016
    Assignee: JANSEN'S AIRCRAFT SYSTEMS CONTROLS, INC.
    Inventor: Schuyler V. McElrath
  • Publication number: 20160115930
    Abstract: An inventive system and method for managing vehicle power is presented. The novel technology provides a means to automatically shutdown a vehicle's engine when conditions are such that engine power is not needed, reducing fuel consumption as well as lowering noise and emissions. A series of conditions are examined to determine whether engine power is needed and hence whether shutdown can be safely performed. The inventive system and method can also determine when power is again needed by the engine and can re-start the engine automatically at such times.
    Type: Application
    Filed: October 9, 2015
    Publication date: April 28, 2016
    Applicant: BAE SYSTEMS CONTROLS INC.
    Inventor: James A. Dupuy
  • Publication number: 20160109897
    Abstract: A continuous, always on, high accuracy AC reference signal is added to an AC voltage of interest to calibrate the AC voltage of interest. The AC reference voltage has a first frequency. The AC voltage of interest has a second frequency. A control system having calibration.
    Type: Application
    Filed: October 15, 2015
    Publication date: April 21, 2016
    Applicant: BAE SYSTEMS Controls Inc.
    Inventors: Russell M. Petrosky, Stephen J. Gabaly, Patrick Nee
  • Publication number: 20160069942
    Abstract: Various embodiments for detecting a High Intensity Radiated Field (HIRF) in a Line Replaceable Unit (LRU) are provided. The internal detector may be used to test EMI filter pin connectors of a closed LRU. For example, a method comprises setting a selecting switch to a test connector position, thereby connecting a RF signal generator to a testing connection cable. The method further comprises causing the generator to generate a test signal as input into the testing connection cable, and determining if an internal HIRF detector has detected the signal. If the signal is detected, the method further comprises, for each EMI filter pin connector in the LRU, switching the selecting switch to a corresponding test cable coupled to an EMI filter pin connector, causing the generator to generate the test signal as input into the corresponding test cable; and determining if the detector has detected the signal.
    Type: Application
    Filed: February 20, 2015
    Publication date: March 10, 2016
    Applicant: BAE SYSTEMS CONTROLS INC.
    Inventors: Paul Hart Heiland, JR., Richard P. Quinlivan, Thomas Edward Guth, Zain Adam Horning, Peter Joseph Watson, Gustavo Enrique Melendez Velazquez
  • Publication number: 20160061684
    Abstract: A multiple channel control system, pressure detection system, a method and a program are provided. A pressure detection system may include first and second pressure transducers having a common pressure source as an input. The first pressure transducer is a different type than the second pressure transducer. The system also includes a storage device configured to store a look up table having a calibrated relationship between temperature and pressure for the second pressure transducer. The system also includes a processor configured to periodically update the look up table based on pressure detected by the first pressure transducer when a condition is met.
    Type: Application
    Filed: September 2, 2015
    Publication date: March 3, 2016
    Applicant: BAE SYSTEMS CONTROLS INC.
    Inventor: William J. Gehm
  • Patent number: 9263948
    Abstract: Various embodiments of the present invention relate to an input output balanced bidirectional buck-boost converter and associated system and method. In one example, a DC/DC bidirectional buck-boost power converter has both input and output voltages centered around chassis. This converter allows for overlapping input and output voltages, and allows for use of offset based leakage fault detection.
    Type: Grant
    Filed: September 25, 2014
    Date of Patent: February 16, 2016
    Assignee: BAE SYSTEMS CONTROLS INC.
    Inventors: Robert J. Vovos, Peter A. Carruthers, Arthur P. Lyons
  • Patent number: 9254738
    Abstract: A hybrid electric drive system for a hybrid powered vehicle which includes a combustion engine, and a transmission. An electric machine and the combustion engine are coupled to the transmission in the hybrid electric drive system providing engine and/or electric machine drive power for the vehicle. A clutch is mechanically communicating with and positioned between the combustion engine and the transmission to decouple the combustion engine from the transmission. An energy storage system is configured to transfer and receive power with the electric machine, and is configured to recharge using power from the electric machine. A hybrid system controller is configured to respond to a regenerative braking mode of the vehicle. While the hybrid electric drive system is in the regenerative braking mode, the hybrid system controller is configured to initiate shifting of the transmission into one or more selected gears relating to one or more selected electric machine speeds.
    Type: Grant
    Filed: August 31, 2012
    Date of Patent: February 9, 2016
    Assignee: BAE SYSTEMS CONTROLS, INC.
    Inventors: Jurgen Schulte, Fillippo Muggeo, Derek Matthws, Brendan Pancheri
  • Patent number: 9206921
    Abstract: A sealed solenoid provides an improved actuator for valves and other devices, particular such devices used in extreme environments and/or with corrosive media. For example, the improved solenoid construction can be used to drive a precision flow control valve used in air and space applications, such as to control fuel and oxidizer combustion media in rocket and other thrust components. The solenoid is retained in a solenoid retainer to which is attached a rigid barrier that isolates the solenoid pole piece and coil from the media. A clapper disposed outside the barrier from the solenoid serves as the armature, receiving magnetic flux from the solenoid through the barrier without interference from the barrier. The barrier may be extremely thin and magnetically inert.
    Type: Grant
    Filed: December 31, 2013
    Date of Patent: December 8, 2015
    Assignee: JANSEN'S AIRCRAFT SYSTEMS CONTROLS, INC.
    Inventors: Harvey B. Jansen, David G. Hayward
  • Patent number: 9181915
    Abstract: An inventive system and method for managing vehicle power is presented. The novel technology provides a means to automatically shutdown a vehicle's engine when conditions are such that engine power is not needed, reducing fuel consumption as well as lowering noise and emissions. A series of conditions are examined to determine whether engine power is needed and hence whether shutdown can be safely performed. The inventive system and method can also determine when power is again needed by the engine and can re-start the engine automatically at such times.
    Type: Grant
    Filed: November 1, 2011
    Date of Patent: November 10, 2015
    Assignee: BAE SYSTEMS CONTROLS INC.
    Inventor: James A. Dupuy
  • Patent number: 9139078
    Abstract: A hybrid electric drive system including a hydraulic power system for a hybrid powered vehicle which includes a transmission, and a combustion engine and an electric motor both mechanically coupled to the transmission to provide engine and/or motor drive power for the vehicle. A plurality of hydraulic circuits communicate with an electrically driven hydraulic pump. The hydraulic pump is configured to provide fluid circulation to the plurality of hydraulic circuits. The hydraulic circuits are each connected to the transmission and other corresponding vehicle components. An electrical power supply is configured to power the electrically driven hydraulic pump, and the electrical power supply is electrically communicating with a rechargeable high voltage (HV) battery system. The electrically driven hydraulic pump communicates with the plurality of hydraulic circuits to provide fluid pressure in the hydraulic circuits.
    Type: Grant
    Filed: August 31, 2012
    Date of Patent: September 22, 2015
    Assignee: BAE SYSTEMS CONTROLS, INC.
    Inventors: Jurgen Schulte, Filippo Muggeo, Derek Matthws, Brendan Pancheri
  • Patent number: 9086168
    Abstract: A pressure regulator includes a pressurized fluid, direct-drive, balanced dual poppet valve assembly that requires no dynamic seals and is pressure balanced. Each poppet has a knife edge that creates a bubble-tight seal against a cooperating seat. The sealing knife edge of one poppet faces into the pressure, and the sealing knife edge of the other poppet faces away from the pressure. The pressure balance negates performance impact of high or low fluid pressure. Furthermore, the design provides for a controlled depth of deformation by the sealing knife edges of the poppets into the soft surfaces of the seats. With this arrangement, no dynamic seals are required, reducing the friction to a very low value. The valve assembly is actuated by solenoid that is optimized for light weight, high speed response, and low power consumption. The solenoid is designed to be immersed and operated within the pressurized fluid.
    Type: Grant
    Filed: August 28, 2013
    Date of Patent: July 21, 2015
    Assignee: Jansen's Aircraft Systems Controls, Inc.
    Inventor: Harvey B. Jansen