John Bucknell, PE

John Bucknell, PE

Troy, Michigan, United States
3K followers 500+ connections

About

Serial entrepreneur and technical founder.

Highly innovative systems level…

Activity

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Experience

  • Virtus Solis Technologies Graphic

    Virtus Solis Technologies

    Michigan, United States

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    Torrance, California, United States

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    Greater Los Angeles Area

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    Auburn Hills, MI

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Education

  • University of Michigan-Dearborn Graphic

    University of Michigan-Dearborn

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    Activities and Societies: Masters Thesis - Design Synthesis of 1300cc Racing V8 Engine Partner: Eric Leonhardt - Director of Vehicle Research Institute, Western Washington University

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    Activities and Societies: Formula SAE 1990-1994 Society of Automotive Engineers - President 1991-92 Triangle Fraternity

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Licenses & Certifications

Volunteer Experience

  • FSAE Chief Design Judge - Aerodynamics

    Society of Automotive Engineers

    - Present 23 years 4 months

    Education

    Formula SAE is the largest STEM competition in the world for engineering students at the undergraduate and graduate level. Competitors design, build and compete on the track with small open-wheeled formula style race cars. In the Design competition, students are judged on their engineering knowledge, design decisions and execution. As a Chief Design Judge, I headed a small team of Design judges specializing in racecar aerodynamics for a number of years - starting in 2016 we expanded to…

    Formula SAE is the largest STEM competition in the world for engineering students at the undergraduate and graduate level. Competitors design, build and compete on the track with small open-wheeled formula style race cars. In the Design competition, students are judged on their engineering knowledge, design decisions and execution. As a Chief Design Judge, I headed a small team of Design judges specializing in racecar aerodynamics for a number of years - starting in 2016 we expanded to embedded design judges in each of the twenty judging queues due to the high number of teams implementing high performance aerodynamic aids on their race cars.

Publications

  • The Reactivity-Controlled Ignition Compounded Engine - A 72% Indicated Thermal Efficiency & 94bar IMEP Cycle for tomorrow's renewable fuels

    Self

    This work introduces a new engine cycle to simultaneously improve heavy duty transport economics through vastly improved thermal efficiency as well as low-cost exhaust aftertreatment while enabling zero carbon emissions-the Reactivity-Controlled Ignition Compounded Engine (RCICE). This engine uses a combination of high-performance topping cycle with compression ignition of high-octane renewable fuel whose ignition delay is shortened with recuperation of exhaust gas heat into charge air as well…

    This work introduces a new engine cycle to simultaneously improve heavy duty transport economics through vastly improved thermal efficiency as well as low-cost exhaust aftertreatment while enabling zero carbon emissions-the Reactivity-Controlled Ignition Compounded Engine (RCICE). This engine uses a combination of high-performance topping cycle with compression ignition of high-octane renewable fuel whose ignition delay is shortened with recuperation of exhaust gas heat into charge air as well as with waste heat recovery bottoming cycles. The cycle is designed to operate with a 1250 deg K turbine inlet temperature in all regimes, allowing maximum energy recovery with the dual Brayton and Rankine bottoming cycles. Operational efficiency on a European Stationary Cycle (ESC) of the RCICE is estimated to be 63% Brake Thermal Efficiency (BTE) versus the state of the art of 44% 1. Heavy duty emissions regulations such as CARB Phase 2 Green House Gas are met with low-cost aftertreatment enabled by 100% globally stoichiometric operation with zero carbon emissions through renewable fuels. Fuel and emission-control costs are projected to improve over 2022 state-of-the-art petroleum-based fuels by 50% even when accounting for the electrofuel premium of 30%.

    See publication
  • The Turbo Rocket - A high performance air-breathing rocket propulsion system with nuclear and chemical configurations

    AIAA

    A single gas path air-breathing rocket combined cycle architecture has been designed for maximal payload fraction for the terrestrial launch mission. The multi-mode cycle is able to operate as a rocket fan, supercharged ramjet, scramjet and pure rocket sequentially during the ascent to orbit. Primary enthalpy addition to the propellants can be sourced from either nuclear or chemical combustion sources with respective cycles named the Nuclear Thermal Turbo Rocket (NTTR) and Staged Combustion…

    A single gas path air-breathing rocket combined cycle architecture has been designed for maximal payload fraction for the terrestrial launch mission. The multi-mode cycle is able to operate as a rocket fan, supercharged ramjet, scramjet and pure rocket sequentially during the ascent to orbit. Primary enthalpy addition to the propellants can be sourced from either nuclear or chemical combustion sources with respective cycles named the Nuclear Thermal Turbo Rocket (NTTR) and Staged Combustion Turbo Rocket (SCTR), combined the Turbo Rocket family. These cycles are able to achieve mission average specific impulse (Isp) of 1,695 and 1,430 seconds respectively for an 11 meter core with 258 klb vacuum thrust. Moreover, the payload fractions achieved are 44.8% and 32% in a single stage with intended full reusability and propulsive landing, with additional improvements extending airbreathing operation from Mach 14.5 to Mach 18 described. Rocket thrust augmentation is sufficiently high that large core diameters with low net ballistic coefficient and full coverage thermal protection for aerobraking reentry with propulsive landing are applied to the base design. To demonstrate the cycle’s capabilities, an on-orbit refueled mission is described that achieves a single stage return to Earth’s surface from Low Earth Orbit (LEO) to Lunar surface and back that is able to deposit 75 and 25 tons on Luna, respectively, for the 11m NTTR and SCTR.

    See publication
  • Enhanced High Temperature Nuclear Plant Economics through Maximal Capacity Utilization - Cogeneration of Electrical Power and Synthetic Fuel with Fully Flexible Product Selection

    Thorium Energy Alliance Conference 8

    A new energy conversion cycle is proposed that enhances the economics of high temperature nuclear power plants. Maximal capacity utilization via coproduction of synthetic fuel and electricity with instantaneous diversion of heat energy to either product vastly improves nuclear power economics in the presence of daily and seasonal demand variations. Using synthetic fuel as an energy storage medium expands the market for nuclear energy to the 90% of primary energy consumption worldwide that is…

    A new energy conversion cycle is proposed that enhances the economics of high temperature nuclear power plants. Maximal capacity utilization via coproduction of synthetic fuel and electricity with instantaneous diversion of heat energy to either product vastly improves nuclear power economics in the presence of daily and seasonal demand variations. Using synthetic fuel as an energy storage medium expands the market for nuclear energy to the 90% of primary energy consumption worldwide that is currently fossil fuels.

    See publication
  • Single Stage to Orbital Habitat - A Mission Analysis

    Icarus Interstellar Starship Congress 2017

    A proposal using a prior developed nuclear thermal rocket to mine lunar ice and construct an orbital habitat, using the water for both propellant and structure

    See publication
  • The Nuclear Thermal Turbo Rocket – a conceptual high-performance Earth To Orbit propulsion system

    AIAA

    Highest performance launch system ever proposed - able to loft nearly an order of magnitude more payload into low earth orbit as a fraction of launch gross weight than current launch systems.

    The propulsion concept is able to transport more than 50% mass fraction in a Single Stage to Orbit (SSTO) via an air-breathing rocket trajectory with intended complete reusability. Payload fractions of up to 19% are predicted (dry mass includes reactor shielding) due to a mission average Isp of…

    Highest performance launch system ever proposed - able to loft nearly an order of magnitude more payload into low earth orbit as a fraction of launch gross weight than current launch systems.

    The propulsion concept is able to transport more than 50% mass fraction in a Single Stage to Orbit (SSTO) via an air-breathing rocket trajectory with intended complete reusability. Payload fractions of up to 19% are predicted (dry mass includes reactor shielding) due to a mission average Isp of more than 1,600 seconds. Comparisons to conventional chemical and other nuclear thermal launch propulsion systems are presented.

    See publication
  • Economics of transportation hydrocarbon fuels and environmental regulations with conceptual solutions – carbon-neutral and carbon-negative synfuels

    SAE

    Of all current proposals for sustainable transportation, the assumption is energy scarcity when there are economically favorable alternatives using existing technology. This paper explores the economics of a sustainable transportation energy pathway that provides carbon-neutral and carbon-negative synthetic fuel derived from seawater as the feedstock and power via Ocean Thermal Energy Cycle (OTEC). Seawater based synthetic fuel is naturally carbon-neutral - different synthesis processes can…

    Of all current proposals for sustainable transportation, the assumption is energy scarcity when there are economically favorable alternatives using existing technology. This paper explores the economics of a sustainable transportation energy pathway that provides carbon-neutral and carbon-negative synthetic fuel derived from seawater as the feedstock and power via Ocean Thermal Energy Cycle (OTEC). Seawater based synthetic fuel is naturally carbon-neutral - different synthesis processes can yield hydrogen, methane, methanol and ethanol as well as gasoline, diesel or jet fuel - and is carbon-negative when combined with aquaculture. Methanol is favored as a fuel as it requires relatively lower capital investment; can be easily transported and stored; can be used as a feedstock to many chemical processes that currently rely on petrochemicals; and can be coproduced with or converted to dimethyl ether. This paper proposes a new process that for the first time marries OTEC-power and seawater-based methanol synthetic fuel generation. The proposed process is optimized for highest product yield for a given capital investment, in that operating costs and therefore product costs are dominated by capital cost amortization. The methanol fuel produced by this process within the amortization period has a cost per unit of energy potentially comparable to petroleum-derived gasoline or diesel fuel and post-amortization to natural gas. The economics of this new process is compared to prior synthetic methanol processes proposed by Meyer Steinberg and William Avery.

    See publication
  • Development and economic analysis of a two stroke compounded engine concept – the BETE-Max

    SAE

    Forthcoming transportation carbon dioxide and environment emission regulations favor solutions with the lowest cost of ownership in the open market. Light duty vehicles and especially those used in urban areas benefit the most from increasing electrification, but medium and heavy duty vehicles - including truck, marine, rail and aircraft - have high continuous power requirements that benefit little from electrification until energy storage costs drop significantly.
    This paper explores energy…

    Forthcoming transportation carbon dioxide and environment emission regulations favor solutions with the lowest cost of ownership in the open market. Light duty vehicles and especially those used in urban areas benefit the most from increasing electrification, but medium and heavy duty vehicles - including truck, marine, rail and aircraft - have high continuous power requirements that benefit little from electrification until energy storage costs drop significantly.
    This paper explores energy storage costs whose alternatives will be weighed against increasing payload fraction costs. A conceptual solution is presented that provides low cost of ownership: an engine that operates as a spark-ignited two stroke engine with compounding and light electrification.
    This engine (named BETE-Max) has a high thermal efficiency across its operating range and is able to meet
    tailpipe emissions standards with low aftertreatment costs using known technology.

    See publication
  • Learn & Compete A primer for Formula SAE, Formula Student and Formula Hybrid teams

    Racecar Graphic Limited

    Other authors

Patents

  • Power-based turbocharger boost control techniques

    Issued US US20170350313A1

    A power-based control system and method for an engine comprising a turbocharger involve obtaining a set of parameters that each affect exhaust gas energy and using the set of parameters to (i) determine a target mass flow into the engine and a target boost for the turbocharger to achieve a torque request, (ii) determine a target power for a compressor of the turbocharger to achieve the target engine mass flow and the target turbocharger boost, (iii) determine a target pressure ratio and a…

    A power-based control system and method for an engine comprising a turbocharger involve obtaining a set of parameters that each affect exhaust gas energy and using the set of parameters to (i) determine a target mass flow into the engine and a target boost for the turbocharger to achieve a torque request, (ii) determine a target power for a compressor of the turbocharger to achieve the target engine mass flow and the target turbocharger boost, (iii) determine a target pressure ratio and a target mass exhaust flow for the turbine of the turbocharger to achieve a target turbine power equal to the target compressor power, and (iv) determine a target position of the wastegate valve to achieve the target turbine pressure ratio and mass exhaust flow, and commanding a wastegate valve to the target position.

    See patent
  • Methods and apparatus for additively manufactured identification features

    Issued US US 10,357,959 B2

    Techniques for integrating a machine-readable matrix with a component of a mechanical structure using three-dimensional (3-D) printing are disclosed. Such techniques include generating at least one data model representing the component, and projecting a matrix pattern identifying one or more features of the component onto a selected surface portion of the component to produce a modified data model for use as an input to a 3-D printer.

  • Engine condensation control system and method

    Issued US US9879626B1

    A system and method for controlling condensation formation in an engine having EGR and forced induction includes a controller for determining a water vapor mass fraction of an exhaust stream based on a water vapor mass fraction of an intake stream and water vapor from combustion. An estimated condensation temperature (CT) is determined for a current EGR level based on the water vapor mass fractions and is compared to an intake stream temperature upstream of the compressor inlet. The controller…

    A system and method for controlling condensation formation in an engine having EGR and forced induction includes a controller for determining a water vapor mass fraction of an exhaust stream based on a water vapor mass fraction of an intake stream and water vapor from combustion. An estimated condensation temperature (CT) is determined for a current EGR level based on the water vapor mass fractions and is compared to an intake stream temperature upstream of the compressor inlet. The controller commands the current EGR level as a maximum EGR level upon determining the intake stream temperature is less than the CT, and an increase in the current EGR level upon determining the intake stream temperature is greater than the CT. An air charge temperature (ACT) of the forced induction system may be controlled based on utilizing a target ACT as the CT to be controlled by a coolant pump.

    See patent
  • Continuous adaptation of an intake oxygen sensor for pressure, humidity and aging

    Issued US US9784195B2

    A technique is provided for compensating an untrimmed oxygen (O2) sensor utilized in operation of an exhaust gas recalculation (EGR) system associated with an engine. The technique includes, in one implementation, receiving a measurement from the O2 sensor at a known pressure, where the O2 sensor is positioned on an intake side of an engine system. Humidity compensation and pressure compensation are then determined for the O2 sensor measurement, where the pressure compensation is based in part…

    A technique is provided for compensating an untrimmed oxygen (O2) sensor utilized in operation of an exhaust gas recalculation (EGR) system associated with an engine. The technique includes, in one implementation, receiving a measurement from the O2 sensor at a known pressure, where the O2 sensor is positioned on an intake side of an engine system. Humidity compensation and pressure compensation are then determined for the O2 sensor measurement, where the pressure compensation is based in part on the humidity compensation. The EGR system is controlled using the untrimmed O2 sensor measurement that has been compensated for pressure and humidity.

    See patent
  • Integral purge ejector tee arrangement in a turbocompressor

    Issued US US9664154B2

    A boost purge ejector tee arrangement is integrated into a turbocompressor associated with an engine and includes first and second passages, an inlet port and a nozzle. The first passage is formed into a housing of the turbocompressor and includes an outlet in communication with a turbocompressor inlet. The second passage is formed into the housing and includes a boost air inlet in communication with an internal outlet area of the turbocompressor and intersecting the first passage. The inlet…

    A boost purge ejector tee arrangement is integrated into a turbocompressor associated with an engine and includes first and second passages, an inlet port and a nozzle. The first passage is formed into a housing of the turbocompressor and includes an outlet in communication with a turbocompressor inlet. The second passage is formed into the housing and includes a boost air inlet in communication with an internal outlet area of the turbocompressor and intersecting the first passage. The inlet port is associated with the housing and intersects the first passage. The nozzle is positioned in the first passage such that an outlet of the nozzle is proximate the intersection of the inlet port and first passage. During a boost mode of operation, the second passage is adapted to receive boost air flow, which flows through the nozzle thereby creating a vacuum and drawing purge through the inlet port.

  • Position control of flow control valves near endstops

    Issued US US20160305312A1

  • Two-step valvetrain preposition control strategy

    Issued US WO2017091455A1

  • Thermal Management Exhaust Treatment Device and Method of Manufacture

    Issued US US8715580 B2

    An exhaust gas treatment device is disposed in an exhaust gas treatment system and comprises a rolled metal cylinder of corrugated metal sheet having longitudinally extending passages extending axially from an inlet end to an outlet end and a conduit disposed between layers of the rolled metal cylinder and configured for circulation of a heat transfer medium there through, the conduit extending axially and radially the rolled metal cylinder.

  • Vehicle Waste Heat Recovery System and Method of Operation

    Issued US US8628025

    An engine assembly may include a first heat exchanger, a fluid supply system providing a fluid flow to the first heat exchanger, a fuel system, an engine block defining first and second cylinder bores, a first piston disposed within the first cylinder bore, and a second piston disposed within the second cylinder bore. The first cylinder bore may receive fuel from the fuel system for combustion therein to drive the first piston. The fluid flow may be pressurized within the first heat exchanger…

    An engine assembly may include a first heat exchanger, a fluid supply system providing a fluid flow to the first heat exchanger, a fuel system, an engine block defining first and second cylinder bores, a first piston disposed within the first cylinder bore, and a second piston disposed within the second cylinder bore. The first cylinder bore may receive fuel from the fuel system for combustion therein to drive the first piston. The fluid flow may be pressurized within the first heat exchanger and the pressurized fluid may be provided to the second cylinder bore to drive the second piston.

  • Forced Induction and Exhaust System

    Issued US US8528327

    In one exemplary embodiment of an exhaust system, the system includes an exhaust manifold in fluid communication with an internal combustion engine and a forced induction device in fluid communication with the exhaust manifold, the forced induction device including a housing. The system further includes a flow control device to control fluid communication between the forced induction device and a catalyst substrate and to control fluid communication between the exhaust manifold and the catalyst…

    In one exemplary embodiment of an exhaust system, the system includes an exhaust manifold in fluid communication with an internal combustion engine and a forced induction device in fluid communication with the exhaust manifold, the forced induction device including a housing. The system further includes a flow control device to control fluid communication between the forced induction device and a catalyst substrate and to control fluid communication between the exhaust manifold and the catalyst substrate.

    Other inventors
    • dominique lester
    • rodney baker
  • Cylinder Head for Improved Fluid Flow Performance

    Issued US US8251037

    A fluid flow valve in a cylinder head comprises a first valve end and an axially disposed second shaft end connected by a valve shaft. A first valve member is located at the first valve end and a second valve member is located axially from, and in fixed relationship to, the first valve member along the valve shaft. A valve support extends axially between and connects the first valve member and the second valve member; the valve support including an axially extending wall portion having…

    A fluid flow valve in a cylinder head comprises a first valve end and an axially disposed second shaft end connected by a valve shaft. A first valve member is located at the first valve end and a second valve member is located axially from, and in fixed relationship to, the first valve member along the valve shaft. A valve support extends axially between and connects the first valve member and the second valve member; the valve support including an axially extending wall portion having circumferentially spaced support struts extending radially between the valve shaft and the wall portion. Fluid flow passages extend axially through the wall portion, between the circumferentially spaced support struts, wherein fluid flows simultaneously about the exterior of the wall portion and through the fluid flow passages in the wall portion when the valve member is biased to an open position.

  • System and Method for Controlling a Supercharged Engine with Inlet and Port Throttle

    Issued US US8215293

    A method and system for controlling an engine with a supercharger includes a bypass valve control module controlling a bypass valve for the supercharger having a bypass flow area in response to a desired manifold absolute pressure, an inlet valve control module controlling an inlet throttle for a supercharger in response to a bypass flow area and a port throttle control module controlling a port throttle in response to the desired mass airflow.

  • Integrated Inlet and Bypass Throttle for Positive-Displacement Supercharged Engines

    Issued US US8069664

    A supercharged engine has a charge air intake and an engine exhaust outlet, a positive displacement supercharger connected to the air intake, a charge air and bypass control valve comprising a rotary body throttle valve including a rotary valve body, a primary air passage and a separate bypass air passage each extending through the rotary body. The primary air passage is fully open in a first rotary position of the rotary body wherein the bypass air passage is closed, and the bypass air passage…

    A supercharged engine has a charge air intake and an engine exhaust outlet, a positive displacement supercharger connected to the air intake, a charge air and bypass control valve comprising a rotary body throttle valve including a rotary valve body, a primary air passage and a separate bypass air passage each extending through the rotary body. The primary air passage is fully open in a first rotary position of the rotary body wherein the bypass air passage is closed, and the bypass air passage is fully open in a second rotary position wherein the primary air passage is closed. Airflow through the passages varies in an inverse manner as the rotary body is rotated between the first and second positions, whereby airflow through the control valve is controlled with a single actuator movable through the full range of positions and airflow through the primary and bypass passages is inversely varied.

  • Crankcase Vapor Management System

    Issued US US7992548

    An engine assembly includes a vapor canister in selective fluid communication with a crankcase to store alcohol vapor when the temperature inside the crankcase causes alcohol accumulated in the crankcase to boil. The vapor canister is in selective fluid communication with an air induction system to recirculate the alcohol vapor through the engine in a metered fashion.

    Other inventors
    • michael chapie
    • john s jackson
  • Integrated Bypass and Variable Geometry Configuration for an Exhaust Gas Turbocharger

    Issued US US6941755

    An exhaust gas turbocharger comprising: a twin scroll turbine housing; a turbine wheel positioned in the twin scroll housing; an exhaust gas inlet, operatively connected to port exhaust gas through each side of the twin scroll turbine housing and onto the turbine wheel; a bypass, operatively connected to the exhaust gas inlet to port exhaust gas around the twin scroll turbine housing to bypass the turbine wheel; and a valve, operatively positioned to control exhaust gas flow to each side of the…

    An exhaust gas turbocharger comprising: a twin scroll turbine housing; a turbine wheel positioned in the twin scroll housing; an exhaust gas inlet, operatively connected to port exhaust gas through each side of the twin scroll turbine housing and onto the turbine wheel; a bypass, operatively connected to the exhaust gas inlet to port exhaust gas around the twin scroll turbine housing to bypass the turbine wheel; and a valve, operatively positioned to control exhaust gas flow to each side of the twin scroll turbine housing and the bypass.

    Other inventors
  • Integrated Inlet Manifold Tuning Valve and Charge Motion Control Device for Internal Combustion Engines

    Issued US US6827054

    An integrated inlet manifold tuning valve for a variable configuration air inlet manifold and a charge motion control system. A tuning valve, which is preferably approximately a quarter-barrel valve, is arranged at an end of the low- and high-speed runners at or near an intake port for an internal combustion engine. The tuning valve operates to tune the variable manifold and provide a mixture motion for charge motion control.

    Other inventors
  • Charge Air Intercooler Having a Fluid Loop Integrated with the Vehicle Air Conditioning System

    Issued US US6796134

    An intercooler for a vehicle engine incorporating an exhaust gas turbocharger and an air conditioning system, the intercooler comprising: a charge air cooler loop operatively connected to cool heated, pressurized air from the turbocharger before it flows into the vehicle engine; and an air conditioning system bypass loop operatively connecting the air conditioning system to the charge air cooler loop.

    Other inventors
  • Material handling in additive manufacturing

    Filed US US20180339466A1

  • Robotic assembly of transport structures using on-site additive manufacturing

    Filed US US20180339456A1

  • Apparatus and methods for joining panels

    Filed US US20180334797A1

  • Multi-materials and print parameters for additive manufacturing

    Filed US US20180311769A1

  • Scatter reduction in additive manufacturing

    Filed US US20180311758A1

  • Additive manufacturing control systems

    Filed US US20180311757A1

  • Apparatus and methods for removable support structures in additive manufacturing

    Filed US US20180311733A1

  • Powder-bed fusion beam scanning

    Filed US US20180311760A1

  • Adaptive Heat Exchange Architecture for Optimum Energy Recovery ina Waste Heat Recovery Architecture

    Filed US US2013/0186088

    A waste heat recovery system that efficiently converts waste heat from an engine coolant and an engine exhaust in a vehicle. The system includes a coolant heat exchanger that receives heat from the engine coolant, an exhaust heat exchanger that receives heat from the engine exhaust and an economizer heat exchanger. A plurality of valves control the flow of the fluid in different modes as determined by a power ratio between the heat provided by the exhaust heat exchanger and the heat provided by…

    A waste heat recovery system that efficiently converts waste heat from an engine coolant and an engine exhaust in a vehicle. The system includes a coolant heat exchanger that receives heat from the engine coolant, an exhaust heat exchanger that receives heat from the engine exhaust and an economizer heat exchanger. A plurality of valves control the flow of the fluid in different modes as determined by a power ratio between the heat provided by the exhaust heat exchanger and the heat provided by the coolant heat exchanger, including an economizer heat exchanger after coolant heat exchanger mode at low power ratios, where the fluid from the pump flows to the economizer heat exchanger after the coolant heat exchanger and an economizer heat exchanger before coolant heat exchanger mode at high power ratios, where the fluid from the pump flows to the economizer heat exchanger before the coolant heat exchanger.

    Other inventors
  • System and Method for Controlling Exhaust Gas Recirculation

    Filed US US 2012/0323469

    A control system for an engine includes first and second modules. The first module estimates a total amount of exhaust gas recirculation (EGR) in the engine, wherein the total amount of EGR includes (i) EGR within cylinders of the engine and (ii) EGR flowing through an EGR system of the engine. The second module selectively controls an overlap of intake and exhaust valve timing in the engine based on (i) a position of an EGR valve in the EGR system and (ii) a comparison of the estimated total…

    A control system for an engine includes first and second modules. The first module estimates a total amount of exhaust gas recirculation (EGR) in the engine, wherein the total amount of EGR includes (i) EGR within cylinders of the engine and (ii) EGR flowing through an EGR system of the engine. The second module selectively controls an overlap of intake and exhaust valve timing in the engine based on (i) a position of an EGR valve in the EGR system and (ii) a comparison of the estimated total amount of EGR in the engine and an EGR threshold.

  • HVAC-APU Systems for Battery Electric Vehicles

    Filed US US 2012/0198875

    A HVAC-APU system is provided for a battery electric vehicle. The system includes, but is not limited to a refrigerant fluid. A power cycle loop section, a cabin heating cycle loop section, and a cabin refrigeration cycle loop section are in selective fluid communication with each other to advance the refrigerant fluid through the system. A compressor-expander train includes, but is not limited to a reversing compressor-expander and a high-pressure pump that are operably connected by a shaft…

    A HVAC-APU system is provided for a battery electric vehicle. The system includes, but is not limited to a refrigerant fluid. A power cycle loop section, a cabin heating cycle loop section, and a cabin refrigeration cycle loop section are in selective fluid communication with each other to advance the refrigerant fluid through the system. A compressor-expander train includes, but is not limited to a reversing compressor-expander and a high-pressure pump that are operably connected by a shaft. The high-pressure pump pressurizes the refrigerant fluid to form a high-pressure refrigerant fluid. An auxiliary fuel cell and combustion unit heats a heat transfer fluid. A heat exchanger transfers heat from the heated transfer fluid to the high-pressure refrigerant fluid to form a heated high-pressure refrigerant fluid. The reversing compressor-expander expands the heated high-pressure refrigerant fluid to rotate the shaft in a first direction to drive the high-pressure pump.

    Other inventors
  • Cold-spray nozzle

    US US20200009657A1

  • Systems and methods for joining node and tube structures

    US US20200056645A1

  • 3-d-printed components including fasteners and methods for producing same

    US WO2018236817A1

  • An interconnected deflectable panel and node and methods for producing same

    US WO2018226877A1

  • Apparatus and methods for additively manufacturing microtube heat exchangers

    US WO2019010378A1

  • Apparatus and methods for connecting nodes to panels in transport structures

    US WO2019040261A1

  • Apparatus and methods for optimization of powder removal features in additively manufactured components

    US WO2019055149A1

  • Apparatus and methods for removable support structures in additive manufacturing

    US US20190039138A1

  • Integrated wheel assemblies using motor and speed reducer

    US WO2019108355A1

  • Material handling in additive manufacturing

    US WO2018217896A1

  • Methods for additively manufactured identification features

    US US20190315116A1

  • Node with co-printed interconnect and methods for producing same

    US WO2018226867A1

  • Node with co-printed locating features and methods for producing same

    US EP3630454A1

  • Robotic assembly of transport structures using on-site additive manufacturing

    US WO2018217890A1

  • Scatter reduction in additive manufacturing

    US WO2018200303A1

  • Solar extended range electric vehicle

    US WO2019074847A1

  • Solar extended range electric vehicle with panel deployment and emitter tracking

    US WO2019074851A1

  • Suspension systems using hydraulic dampers

    US WO2019108354A1

  • Systems and methods for bridging components

    US WO2019040259A1

  • Systems and methods for implementing node to node connections in mechanized assemblies

    US WO2019010062A4

Honors & Awards

  • Ward's Ten Best Engines - 2013 GM LTG 2.0L Turbo

    Ward's Auto World

  • Ward's Ten Best Engines 2010 - GM LAF 2.4L

    Ward's Auto World

  • Ward's Ten Best Engines 2003 - BMW MINI Cooper S 1.6L HPD

    Ward's Auto World

Organizations

  • Institute of Electrical and Electronics Engineers

    -

    - Present
  • American Nuclear Society

    -

    - Present
  • American Institute of Aeronautics and Astronautics

    -

    - Present
  • Society of Automotive Engineers

    Technical Session Chairman

    - Present

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