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Paul K Anschel

from Asheville, NC
Age ~52
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Also known as:
Paul Kenneth Anschel, Paul K Paul
Phone and address:
45 Windward Dr, Asheville, NC 28803
(828) 299-0656
Related to:
Jeremy W AnschelSara S Anschel, 89Kurt R AnschelJoseph M Marzluff, 77Elise M Anschel, 50
Connected to:
Harry Anscher, 34Mitchell S Anscher, 69Robert Anschlowar, 87Doris J Anschuetz, 107Israel A Anschuetz, 46Dean W Anschultz, 87Mike G Anschultz, 67Andy Anschutz, 74Cristy L Anschutz, 43Jody L Anschutz, 66

Paul Anschel Phones & Addresses

  • 45 Windward Dr, Asheville, NC 28803 (828) 299-0656
  • 27 Salola St, Asheville, NC 28806
  • 65 Overlook Rd, Asheville, NC 28803 (828) 274-1574
  • Gouldsboro, ME
  • 2571 Brush Creek Rd, Bryson City, NC 28713 (828) 488-8019
  • 5404 Middleton Ave, Durham, NC 27713 (919) 544-5118
  • 809 Parker St, Durham, NC 27701 (919) 688-9303
  • Fort Collins, CO
  • Swarthmore, PA

Work

Company: Borgwarner Oct 2008 Position: Director of global cd product development

Education

Degree: Masters School / High School: Colorado State University 1995 to 1997 Specialities: Mechanical Engineering

Skills

Engineering Management • Finite Element Analysis • Cfd • Heat Transfer • Data Acquisition • Project Management • Turbomachinery • Strategic Planning • Project Planning • Thermodynamics

Industries

Automotive

Resumes

Resumes

Paul Anschel Photo 1

Senior Technical Specialist, Advanced Engineering

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Location:
Asheville, NC
Industry:
Automotive
Work:
BorgWarner since Oct 2008
Director of Global CD Product Development
BorgWarner Turbo Systems Oct 2005 - Sep 2008
Simulations Manager, North America
BorgWarner Turbo Systems Mar 2003 - Oct 2005
Project Engineer
Magneti Marelli Powertrain USA LLC Nov 2000 - Mar 2003
FEA Analyst
Sturman Industries Jun 1997 - May 2000
Test Engineer
Education:
Colorado State University 1995 - 1997
Masters, Mechanical Engineering Swarthmore College 1991 - 1995
Bachelors, Engineering
Skills:
Engineering Management
Finite Element Analysis
Cfd
Heat Transfer
Data Acquisition
Project Management
Turbomachinery
Strategic Planning
Project Planning
Thermodynamics

Publications

Us Patents

Coupling Turbochargers For Passive Pre-Swirl Counter-Rotation

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US Patent:
8388302, Mar 5, 2013
Filed:
Aug 31, 2009
Appl. No.:
12/550551
Inventors:
William G. Anderson - White Lake MI, US
Paul Anschel - Asheville NC, US
Assignee:
BorgWarner Inc. - Auburn Hills MI
International Classification:
F04D 1/10
US Classification:
415 60, 4151991, 415206
Abstract:
A turbocharger with a high pressure (HP) and low pressure (LP) stage, designed such that swirl in a conduit providing fluid communication between the LP compressor outlet and the HP compressor inlet is received by the second stage compressor counter to the direction of rotation of the second stage compressor wheel. This is achieved without requiring vanes such as inlet guide vanes, and thus is highly efficient as well as free of blockage and excitation.

Duct For Changing Direction Of Flow, Particularly For Turbocharger Compressor Inlet

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US Patent:
8449250, May 28, 2013
Filed:
Oct 15, 2008
Appl. No.:
12/682793
Inventors:
Paul Anschel - Asheville NC, US
Stephen Roby - Asheville NC, US
Assignee:
BorgWarner Inc. - Auburn Hills MI
International Classification:
F01D 25/00
US Classification:
415206, 415184
Abstract:
A direction changing flow duct, for example, a compressor inlet duct () for a turbocharger compressor cover, wherein the direction of flow is made to change abruptly in a short distance. The direction changing segment is designed to provide a balanced output, optimize air flow, minimize pressure drop, and maintain compressor efficiency. This can be accomplished by providing a bulge () extending radially inwards into a first duct segment, outward bulges perpendicular to the inward bulge, for promoting flow attachment along the walls of the duct.

Simplified Variable Geometry Turbocharger With Variable Nozzle

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US Patent:
8590305, Nov 26, 2013
Filed:
Dec 4, 2009
Appl. No.:
13/132994
Inventors:
Paul Anschel - Asheville NC, US
Rajmohan Chandramohanan - Arden NC, US
Assignee:
BorgWarner Inc. - Auburn Hills MI
International Classification:
F02D 23/00
F04D 29/44
F04D 29/54
F01D 17/12
US Classification:
60602, 415158, 4151981, 415126
Abstract:
The flow path of exhaust gas to the turbine wheel () of a twin volute turbocharger is influenced by the shape and size of the nozzle formed by the shape () of the divider wall () and the shape of the flow passage determined by the walls () of the turbine housing. By moving the walls () toward, or away from the divider wall, the flow of exhaust gas through the nozzle, to the turbine wheel () can be modulated, which thus modulates the turbocharger boost pressure. The invention also applies to single volute turbines.

Diffuser Restraint System And Method

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US Patent:
20080193288, Aug 14, 2008
Filed:
Feb 6, 2008
Appl. No.:
12/027137
Inventors:
Paul Anschel - Asheville NC, US
Michael Bucking - Arden NC, US
Robert Lancaster - Indianapolis IN, US
Assignee:
BORG WARNER INC. - Auburn Hills MI
International Classification:
F04D 29/54
B23P 15/00
US Classification:
4152082, 29888025
Abstract:
A restraint system () for a vaned diffuser () of a turbocharger () or other fluid boosting device is provided that can reduce or eliminate losses. The system () uses a structure to provide both a pressure load on the vaned diffuser () and a seal for the vaned diffuser (). The structure can be a fluoroelastomer O-ring (). The O-ring () can be positioned at least partially in a channel () formed in at least one of the diffuser ring (′), the compressor housing () and the center housing ().

Variable Turbine Geometry Turbocharger

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US Patent:
20100104424, Apr 29, 2010
Filed:
Apr 29, 2008
Appl. No.:
12/597787
Inventors:
Paul Anschel - Asheville NC, US
David G. Grabowska - Asheville NC, US
Assignee:
BorgWarner Inc. - Auburn Hills MI
International Classification:
F01D 17/12
US Classification:
415159
Abstract:
A turbocharger is provided having a turbine wheel () with a plurality of extended tips (); and a variable turbine geometry assembly in fluid communication with the turbine wheel and having a nozzle ring () with a plurality of vanes () movably attached thereto. One or more of the extended tips are non-parallel with an edge of one or more of the plurality of vanes. The incidence angle can vary and can be from 1 to 60 degrees. The extended tips can extend into an inlet of the vane space housing the vanes.

Variable Geometry Turbocharger

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US Patent:
20100150701, Jun 17, 2010
Filed:
Jun 26, 2008
Appl. No.:
12/663891
Inventors:
Volker Simon - Landau, DE
Mathias Weber - Frankenthal, DE
Paul Anschel - Asheville NC, US
Assignee:
BORGWARNER INC. - Auburn Hills MI
International Classification:
F04D 29/56
US Classification:
415160
Abstract:
A variable geometry turbocharger is provided. The turbocharger improves efficiency by controlling flow to the rotor () via movable vanes (). The vanes () can be rotated using a pin () and groove () system. The vanes () can be multiple structures () that are movable with respect to each other to increase the length of each of the vanes (). The turbocharger also improves efficiency by creating a better seal in the area between the vanes () and the adjustment ring (). The seal can be provided by biasing the adjustment ring () towards each of the vanes (). The seal can be provided by expanding each of the vanes (). The seal can be provided by having a movable portion () of the adjustment ring () that is actuated by a pressure source or the like and axially moves towards the vanes (). The plurality of vanes () can be low solidity vanes.

Compressor Recirculation Into Annular Volume

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US Patent:
20130152582, Jun 20, 2013
Filed:
Aug 30, 2011
Appl. No.:
13/817906
Inventors:
Paul K. Anschel - Asheville NC, US
David G. Grabowska - Asheville NC, US
Brock Fraser - Asheville NC, US
Assignee:
BORGWARNER INC. - Auburn Hills MI
International Classification:
F02M 25/07
US Classification:
606052, 415145
Abstract:
To solve the problems of compressor wheel blade flow separation causing surge type noises when a compressor return or recirculation valve is opened or closed, bypass airflow from a compressor recirculation valve is fed into an annular volume, defined between inner and outer walls or shaped as a radially expanded, axially flattened cylindrical space in the compressor inlet, so that the generally unidirectional radial flow from the compressor recirculation valve is re-directed and organized as it is turned from generally radial to generally axial, merging with the general inlet flow and presenting the compressor wheel with airflow of “circumferentially uniform” flow velocity.

Compressor Recirculation Into Annular Volume

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US Patent:
20150285257, Oct 8, 2015
Filed:
Jun 19, 2015
Appl. No.:
14/744073
Inventors:
Paul K. Anschel - Asheville NC, US
David G. Grabowska - Asheville NC, US
Brock Fraser - Asheville NC, US
Assignee:
BorgWarner Inc - Auburn Hills MI
International Classification:
F04D 27/02
F02M 25/07
Abstract:
To solve the problems of compressor wheel blade flow separation causing surge type noises when a compressor return or recirculation valve is opened or closed, bypass airflow from a compressor recirculation valve is fed into an annular volume, defined between inner and outer walls or shaped as a radially expanded, axially flattened cylindrical space in the compressor inlet, so that the generally unidirectional radial flow from the compressor recirculation valve is re-directed and organized as it is turned from generally radial to generally axial, merging with the general inlet flow and presenting the compressor wheel with airflow of “circumferentially uniform” flow velocity.
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Paul K Anschel from Asheville, NC, age ~52 Get Report