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Eugenio Divalentin Phones & Addresses

  • Cedar Falls, IA
  • Waterloo, IA
  • 1049 Hillcrest Ave, Brighton, MI 48116 (810) 229-3167
  • Enfield, CT
  • Westland, MI
  • Riverdale, MD

Publications

Us Patents

Airflow Control For Multiple-Displacement Engine During Engine Displacement Transitions

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US Patent:
7013866, Mar 21, 2006
Filed:
Mar 23, 2005
Appl. No.:
11/087443
Inventors:
Michael J Prucka - Grass Lake MI, US
Gregory L Ohl - Ann Arbor MI, US
Zhong Li - Westland MI, US
Mark J Duty - Goodrich MI, US
Eugenio DiValentin - Brighton MI, US
Michael A Bonne - Leonard MI, US
Assignee:
DaimlerChrysler Corporation - Auburn Hills MI
International Classification:
F02D 13/04
US Classification:
123319
Abstract:
A method for controlling airflow in an intake manifold of a multiple-displacement engine during an engine displacement mode transition includes determining, before a displacement mode transition, a post-transition mass air flow rate necessary to maintain a pre-transition engine torque output, as well as an airflow transient multiplier based on engine speed and an estimated post-transition manifold air pressure. After multiplying the requested mass air flow rate with the transient multiplier, the resulting compensated requested mass air flow rate is divided by a maximum mass air flow rate to obtain a requested percent airflow. The percent airflow is thereafter used with engine speed to determine a requested post-transition manifold air pressure-to-barometric pressure ratio, for example, using a lookup table; and the requested post-transition pressure ratio is used to determine a transient post-transition throttle position, to which an engine throttle will be moved upon initiating the displacement mode transition.

Method For Controlling An Operating Condition Of A Vehicle Engine

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US Patent:
7181332, Feb 20, 2007
Filed:
Oct 25, 2005
Appl. No.:
11/257673
Inventors:
Roger K Vick - Troy MI, US
Michael J Prucka - Grass Lake MI, US
Timothy A Coatesworth - Lake Orion MI, US
Denise M Kramer - Macomb MI, US
Eugenio DiValentin - Brighton MI, US
Gregory L Ohl - Ann Arbor MI, US
Assignee:
DaimlerChrysler Corporation - Auburn Hills MI
International Classification:
B60T 7/12
F02B 75/02
US Classification:
701103, 731173, 731181, 123316, 12340645, 12356814, 701108
Abstract:
A residual ratio factor characterizing the amount of residual exhaust gas left in a selected cylinder at the end of a piston intake stroke is determined from tabular and surface models based on previously gathered dynamometer data from a test vehicle at various engine speeds. The residual ratio factor is then used to calculate the mole fractions of air and residual exhaust gas in the selected cylinder, which, in turn, are used to determine mass airflow at an engine intake port at the end of the intake stroke. The mass airflow can then be used to derive further models for determining an engine operating parameter, such as fuel/air ratio, required for achieving at preselected vehicle operating condition.

Method For Controlling An Operating Condition Of A Vehicle Engine

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US Patent:
7292928, Nov 6, 2007
Filed:
Jan 18, 2007
Appl. No.:
11/624263
Inventors:
Roger K Vick - Troy MI, US
Michael J Prucka - Grass Lake MI, US
Timothy A Coatesworth - Lake Orion MI, US
Denise M Kramer - Macomb MI, US
Eugenio DiValentin - Brighton MI, US
Gregory L Ohl - Ann Arbor MI, US
Assignee:
Chrysler LLC - Auburn Hills MI
International Classification:
B60T 7/12
F02P 5/00
US Classification:
701103, 12340645
Abstract:
A residual ratio factor characterizing the amount of residual exhaust gas left in a selected cylinder at the end of a piston intake stroke is determined from tabular and surface models based on previously gathered dynamometer data from a test vehicle at various engine speeds. The residual ratio factor is then used to calculate the mole fractions of air and residual exhaust gas in the selected cylinder, which, in turn, are used to determine mass airflow at an engine intake port at the end of the intake stroke. The mass airflow can then be used to derive further models for determining an engine operating parameter, such as fuel/air ratio, required for achieving at preselected vehicle operating condition.

Ground Mode Control Of Aircraft Propeller Speed And Pitch

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US Patent:
50290916, Jul 2, 1991
Filed:
Apr 11, 1989
Appl. No.:
7/336269
Inventors:
Roy W. Schneider - Ellington CT
Eugenio DiValentin - Enfield CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
G06F 1548
B63H 310
B64C 1134
F01D 700
US Classification:
36443101
Abstract:
A ground mode pitch position logic and control is shown and described in this invention. A method for scheduling and limiting the pitch actuator reference signal in accordance with the actuator commanded schedule, propeller overspeed and propeller underspeed.

Propeller Speed Control Having Control Parameters Based On System Dynamic Characteristics

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US Patent:
54166993, May 16, 1995
Filed:
Nov 18, 1992
Appl. No.:
7/977938
Inventors:
Eugenio DiValentin - Enfield CT
Roy W. Schneider - Ellington CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
B64C 1150
US Classification:
36442401
Abstract:
An aircraft propeller speed control defines values for propeller speed governing control law parameters, such as gains and dynamic compensations, based on known values of propeller and engine dynamic characteristics over the complete propeller operating envelope. Adjusting control law gains and dynamic compensations as functions of propeller and engine dynamic characteristics over the entire flight envelope provides for control of propeller speed to obtain optimum stability and consistent propulsion performance over the entire flight envelope.

Propeller Speed Governor Having A Derivative Inhibit At High Flight Speeds

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US Patent:
50170899, May 21, 1991
Filed:
Apr 11, 1989
Appl. No.:
7/336273
Inventors:
Roy W. Schneider - Ellington CT
Eugenio DiValentin - Enfield CT
Assignee:
United Technologies Corporation - Hartford CT
International Classification:
B63H 300
B64C 318
US Classification:
416 35
Abstract:
A propeller speed governor having a derivative feedback of propeller speed and having a means such as a switch to open the derivative feed back loop when airspeed exceeds a predetermined amount is shown and described. This derivative inhibit is used to provide improved dynamic compensation at high and low speeds.
Eugenio N Divalentin from Cedar Falls, IA, age ~68 Get Report