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Boorman, US

Brian Boorman, Honeoye, NY US

Patent application numberDescriptionPublished
20090113201SCALEABLE ARCHITECTURE TO SUPPORT HIGH ASSURANCE INTERNET PROTOCOL ENCRYPTION (HAIPE) - A scalable internet protocol (IP) encryption system includes a cryptographic unit that processes sensitive data for packet encryption/decryption and data authentication. A first processing unit with an optional IP Layer hardware accelerator includes a data processing subsystem that processes sensitive data and forwards the data to the cryptographic unit for encryption and data authentication. A management subsystem is operative with the cryptographic unit for configuring IP networking functions and distributing network configuration information to the data processing subsystem through the cryptographic unit. Data processing is separated from management and control functions at the data processing and management subsystems. A second processing unit with an optional IP Layer hardware accelerator receives the encrypted data from the cryptographic unit and processes the encrypted data for IP packet routing, fragmentation and reassembly and receives network configuration information from the management subsystem via the cryptographic unit.04-30-2009

Daniel J. Boorman, Woodinville, WA US

Patent application numberDescriptionPublished
20100076627APPARATUSES AND METHODS FOR DISPLAYING AND RECEIVING TACTICAL AND STRATEGIC FLIGHT GUIDANCE INFORMATION - Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.03-25-2010
20100076628APPARATUSES AND METHODS FOR DISPLAYING AUTOFLIGHT INFORMATION - Apparatuses and methods for displaying autoflight information and controlling autoflight systems. In one embodiment, a flight deck for an aircraft having an autoflight system includes at least one pilot seat, at least one window positioned forward of the pilot seat, and a forward instrument panel positioned forward of the pilot seat. In one aspect of this embodiment, the forward window provides a forward field of view out of the aircraft for a pilot seated in the pilot seat. In another aspect of this embodiment, the flight deck further includes a display device configured to provide information related to one or more autoflight modes. The display device can be positioned at least approximately between the forward instrument panel and the forward window to provide the pilot with autoflight information at least proximate to the forward field of view. In a further aspect of this embodiment, the display device can be configured to provide information related to one or more target flight parameters.03-25-2010
20100262358APPARATUSES AND METHODS FOR DISPLAYING AND RECEIVING TACTICAL AND STRATEGIC FLIGHT GUIDANCE INFORMATION - Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.10-14-2010
20100305786METHOD AND SYSTEM FOR APPROACH DECISION DISPLAY - Approach Decision Display and associated methods and systems are disclosed. A method and system in accordance to one embodiment of the disclosure includes a display of operationally-relevant information for final approach and landing on a cockpit graphical display. Approach Decision Display System (ADDS) provides, in a graphical display, dynamic decision parameters as a function of the health of required equipment for the selected approach and the aircraft's ability to execute the approach and landing.12-02-2010
20110118908METHODS AND SYSTEMS FOR MANAGEMENT OF AIRPLANE SPEED PROFILE - Methods and systems for airplane speed profile management are disclosed. A method and system in accordance to one embodiment of the disclosure includes a graphical display of speed segments and constraints as well as controls for managing the speeds and associated constraints. Speed Profile Management System (SPMS) provides an integrated and interactive speed profile management tool where pilots can view, update, or change the speed profile of their airplane's current or subsequent phases of flight.05-19-2011
20110125347APPARATUSES AND METHODS FOR DISPLAYING AUTOFLIGHT INFORMATION - Apparatuses and methods for displaying autoflight information and controlling autoflight systems. In one embodiment, a flight deck for an aircraft having an autoflight system includes at least one pilot seat, at least one window positioned forward of the pilot seat, and a forward instrument panel positioned forward of the pilot seat. In one aspect of this embodiment, the forward window provides a forward field of view out of the aircraft for a pilot seated in the pilot seat. In another aspect of this embodiment, the flight deck further includes a display device configured to provide information related to one or more autoflight modes. The display device can be positioned at least approximately between the forward instrument panel and the forward window to provide the pilot with autoflight information at least proximate to the forward field of view. In a further aspect of this embodiment, the display device can be configured to provide information related to one or more target flight parameters.05-26-2011
20110224848APPARATUSES AND METHODS FOR DISPLAYING AND RECEIVING TACTICAL AND STRATEGIC FLIGHT GUIDANCE INFORMATION - Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.09-15-2011
20110295450APPARATUSES AND METHODS FOR DISPLAYING AND RECEIVING TACTICAL AND STRATEGIC FLIGHT GUIDANCE INFORMATION - Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.12-01-2011

Patent applications by Daniel J. Boorman, Woodinville, WA US

Daniel J. Boorman, Woodinvill, WA US

Patent application numberDescriptionPublished
20110313600INTEGRATED APPROACH NAVIGATION SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT - Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of non-precision flight modes are provided. Improved graphical depictions of navigation performance based flight path deviation information provide pilots and flight crew members with clear, concise displays of the dynamic relationship between ANP and RNP, mode and aspect of flight and related procedures, intersecting flight paths, and current actual flight path deviation from a predefined flight path during the final approach segment to a runway and during landing. For example, an enhanced IAN display may include NPS-type deviation scales to show RNP/ANP relationships and predetermined RNP markers to alert the pilots and flight crew members that the FMC has transitioned from an NPS display for RNAV (LNAV/VNAV) flight procedures to an enhanced IAN display for a non-precision (non-xLS) approach and/or landing.12-22-2011

Daniel J. Boorman, Seattle, WA US

Patent application numberDescriptionPublished
20090062972Systems and Methods for Presenting and Obtaining Flight Control Information - Systems and methods for presenting and obtaining flight control information are disclosed. In one embodiment, information corresponding to a vertical motion of the aircraft can be displayed between information corresponding to a lateral motion of the aircraft and information corresponding to an airspeed of the aircraft. The information displayed can include a current mode for controlling the motion of the aircraft, a current target to which the aircraft is being directed and, at least proximate to both the current mode and the current target, a subsequent target to which the aircraft will be directed after attaining the current target.03-05-2009

Patent applications by Daniel J. Boorman, Seattle, WA US

James Boorman, Greenacres, WA US

Patent application numberDescriptionPublished
20110253581Molten metal leakege confinement and thernal optimization in vessels used for containing molten metal - Exemplary embodiments of the invention relate to a vessel used for containing molten metal, e.g. a trough section for conveying molten metal from one location to another. The vessel has a refractory liner made of at least two refractory liner units positioned end to end, with a joint between the units, the units each having an exterior surface and a metal-contacting interior surface. A housing at least partially surrounds the exterior surfaces of the refractory liner units with a gap present between the exterior surfaces and the housing. Molten metal confinement elements, impenetrable by molten metal, are positioned on opposite sides of the joint within the gap, at least below a horizontal level corresponding to a predetermined maximum working height of molten metal held within the vessel in use, to partition the gap into a molten metal confinement region between the elements and at least one other region that may be used to hold equipment such as electrical heaters that may be damaged by contact with molten metal. Another embodiment employs refractory liner units of different thermal conductivity to maximize heat penetration into the molten metal from heaters in the gap, but to minimize heat loss at the inlet and outlet of the vessel where the end units contact the housing.10-20-2011

James E. Boorman, Greenacres, WA US

Patent application numberDescriptionPublished
20110139797Molten metal-containing vessel and methods of producing same - Exemplary embodiments of the invention provide a vessel for containing or conveying molten metal therein. At least part of the outer surface of the vessel incorporates a web of metal wires embedded in the surface, the wires being mutually overlaid with openings formed therebetween. The refractory material penetrates into the openings. The web may comprise woven metal wires or non-woven wires or both. The web imparts resistance to cracking (or containment of cracks, once formed) and/or resistance to molten metal leakage if cracks develop. The invention also provides metal containment structures containing such vessels, and methods of producing the same.06-16-2011
20110139799Method of forming sealed refractory joints in metal-containment vessels, and vessels containing sealed joints - An exemplary embodiment of the invention provides a method of preparing a reinforced refractory joint between refractory sections of a vessel used for containing or conveying molten metal, e.g. a metal-contacting trough. The method involves introducing a mesh body made of metal wires into a gap between metal-contacting surfaces of adjacent refractory sections of a vessel so that the mesh body is positioned beneath the metal conveying surfaces, and covering the mesh body with a layer of moldable refractory material to seal the gap between the metal-contacting surfaces. Other embodiments relate to a vessel formed by the method and a vessel section with a pre-positioned mesh body suitable for preparing a sealed joint with other such sections.06-16-2011
20110140322Compressive rod assembly for molten metal containment structure - Exemplary embodiments of the invention relate to a compressive rod assembly for applying force to a refractory vessel positioned within an outer metal casing. The assembly includes a rigid elongated rod having first and second opposed ends, a threaded bolt adjacent to the first opposed end of the elongated rod, and a compressive structure positioned operationally between the elongated rod and the bolt. Compressive force applied by the bolt to the elongated rod passes through the compressive structure which allows limited longitudinal movements of the elongated rod to be accommodated by the compressive structure without requiring corresponding longitudinal movements of the bolt. Exemplary embodiments also relate to rod structure forming a component of the assembly, and to a metal containment structure having a vessel supported and compressed by at least one such assembly.06-16-2011

Jim Boorman, Greenacres, WA US

Patent application numberDescriptionPublished
20090301683Method and apparatus for removal of cooling water from ingots by means of water jets - The exemplary embodiments relate to the removal of cooling water used to cool the surface of an ingot as it is formed during casting. The cooling water is removed from the surface by directing jets of water onto the surface at an angle, and with a momentum, that causes the cooling water to be stripped from the surface when contacted with the jets, and to follow a path that prevents the cooling water from again coming into contact with the ingot surface at a position beyond the point of removal. The apparatus for this includes nozzles to create the water jets, and equipment for supplying water under sufficient pressure and rate of flow to the nozzles.12-10-2009
20100025003Sequential casting of metals having similar freezing ranges - A method and apparatus is disclosed for sequentially direct chill casting a composite ingot made of metals having similar freezing ranges. Poor adhesion between the layers and low reliability of casting are addressed by adjusting the position of secondary cooling (created by applying water streams to the emerging ingot) relative to the upper surfaces of the molten metal pools compared to the conventional positions of first application of the secondary cooling. This can be achieved by moving one or more walls of the mold (when the secondary cooling emanates from the bottom of such walls), or adjusting the height of the molten metal pools within the mold and moving cooled divider walls between the pools. The relative temperatures and conditions of the metals at positions where they meet at the metal interface may therefore be optimized.02-04-2010

Mollie Boorman, Calabasas, CA US

Patent application numberDescriptionPublished
20110018901SYSTEM AND METHOD FOR FORMING A COMPOSITE IMAGE IN A PORTABLE COMPUTING DEVICE HAVING A DUAL SCREEN DISPLAY - A system and method for forming a composite image from a secondary image reflected on to the display of a primary image is disclosed. Furthermore, applications for using the composite image in a video gaming context are disclosed.01-27-2011