DAVID REX GILLIAM
Engineers in Bristol, VA

License number
Virginia 0402026623
Issued Date
Jan 30, 1996
Expiration Date
Jan 31, 2014
Category
Professional Engineer License
Type
Professional Engineer
Address
Address
Bristol, VA

Professional information

David Gilliam Photo 1

Compressor Unit Shell Construction

US Patent:
5538404, Jul 23, 1996
Filed:
Mar 17, 1995
Appl. No.:
8/405687
Inventors:
Michael A. DiFlora - Bristol TN
David R. Gilliam - Bristol VA
Prakash N. Pandeya - Bristol TN
Gordon T. Boyd - Abingdon VA
David T. Monk - Bristol TN
Assignee:
Bristol Compressors, Inc. - Bristol VA
International Classification:
F04B 3900
US Classification:
417312
Abstract:
A shell for a hermetic compressor unit, the shell having a top section or dome, and a bottom section, the dome having a unique shape which gives enhanced capacity for absorbing and attenuating structural and fluid transmitted wave energies emanating from the unit at wave frequencies of between 1,000 Hz and 2,000 Hz, while reducing total operating noise of the unit, the dome being formed of sheet metal and having a generally inverted cup-shaped configuration with generally cylindrical sidewalls and a top wall having a central portion surrounded by a peripheral portion, wherein the sidewall taken in a generally axial direction is substantially straight, wherein the central portion of the top constitutes from about 40 to about 90% of the total area of the top and has a generally hemispherical configuration on a mean radius of from about 6. 5 to about 10. 0 inches as measured from an origin point O. sub.


David Gilliam Photo 2

Compressor Suction Noise Attenuator And Assembly

US Patent:
5123816, Jun 23, 1992
Filed:
Apr 2, 1991
Appl. No.:
7/679413
Inventors:
David R. Gilliam - Bristol VA
Phillip S. Leonard - Bristol VA
Jackson R. Dale - Bristol TN
Assignee:
Bristol Compressors - Bristol VA
International Classification:
F04B 3900, F01N 718
US Classification:
417312
Abstract:
A suction noise attenuator adapted for mounting on a tubular, suction conduit of a gas compressor, the conduit having a gas port through the wall thereof, the attenuator having a shell formed with generally opposed, first and second end walls and generally opposed first and second side walls, all of the walls having proximal and distal portions relative to the suction conduit, the proximal portions being resiliently deformable and the combined edges thereof providing a substantially continuous perimeter mounting face, a distal wall interconnecting the distal portions of all the walls to define an attenuation cavity, the mounting face further defining an inlet to the cavity, the edges of the end walls being concave and adapted to conform substantially to the periphery of the conduit as the attenuator is pressed thereagainst, at least one locator device on the shell adapted for coupling with at least one locator device on the conduit for operatively positioning the attenuator on the conduit to connect the port and cavity in fluid communication, and shoulders on an exterior surface of the shell adapted for retaining a clip fastening device in operative position thereon for securing the attenuator to the conduit.


David Gilliam Photo 3

Discharge Muffler Placement In A Compressor

US Patent:
6935848, Aug 30, 2005
Filed:
May 19, 2003
Appl. No.:
10/441306
Inventors:
Steve Edwin Marshal - Abingdon VA, US
David Rex Gilliam - Bristol VA, US
David Turner Monk - Bristol VA, US
Benjamin Alan Majerus - Bristol VA, US
Assignee:
Bristol Compressors, Inc. - Bristol VA
International Classification:
F04B039/00, F04B017/00
US Classification:
417312, 417902, 181403
Abstract:
A muffler system for a compressor includes an expansion chamber muffler for attenuating sound pressure pulses and an acoustic muffler for filtering high-frequency pressure pulsations. The acoustic muffler is connected inline along the discharge side of the compressor between the discharge port of the cylinder head and a discharge tube in fluid communication with the outlet port of the compressor housing. A conduit is in fluid communication between the outlet port of the compressor housing and the condenser to supply the flow of refrigerant therebetween. Interposed adjacent the compressor housing, but exterior to the compressor housing is an expansion chamber muffler in fluid communication with the conduit for further attenuating pressure pulses generated by operation of the compressor.


David Gilliam Photo 4

Hermetic Electrical Feedthrough Assembly For A Compressor

US Patent:
2014006, Mar 6, 2014
Filed:
Oct 7, 2013
Appl. No.:
14/048027
Inventors:
Scott G. HIX - Bristol VA, US
David R. GILLIAM - Bristol VA, US
Joseph A. NEWLAND - Limestone TN, US
Doug BLANKENSHIP - Bristol TN, US
International Classification:
F04C 18/02
US Classification:
418 554
Abstract:
An electrical feedthrough assembly for providing connection to components of a compressor includes a housing having an inner surface defining a channel. A sealed wire assembly is provided in the channel. The sealed wire assembly includes a body having an outer surface and a plurality of wires sealingly passing through the body.


David Gilliam Photo 5

Compressor Unit Housing

US Patent:
6971860, Dec 6, 2005
Filed:
May 2, 2003
Appl. No.:
10/428524
Inventors:
David Rex Gilliam - Bristol VA, US
Steve Edwin Marshall - Abingdon VA, US
David Turner Monk - Bristol VA, US
Benjamin Alan Majerus - Bristol VA, US
Scott Garrison Hix - Bristol VA, US
Robert Bruce Peters - Bristol VA, US
Eugene Karl Chumley - Abingdon VA, US
William Thomas Wright - Bristol VA, US
Richard Lynn Smith - Kingsport TN, US
Assignee:
Bristol Compressors, Inc. - Bristol VA
International Classification:
F04B039/12
US Classification:
41742314, 417902
Abstract:
A hermetic compressor unit housing comprised of a shell having a top section and a bottom section which receives the top section, the shell being formed of sheet metal and having generally cylindrical sidewalls wherein the sidewall taken in a generally axial direction is substantially straight, each shell section having an opening, a substantially cylindrical portion, and a closed end portion, the opening having a substantially circular horizontal cross-sectional geometry defined by a major axis and a minor axis, the horizontal cross-sectional geometry including substantially liner opposing sidewall portions preferably disposed adjacent to the intersection of the horizontal sectional geometry with the minor axis, and methods of aligning the shell sections for installation of fixtures and mating of the shell sections.


David Gilliam Photo 6

System And Method For Detecting A Fault Condition In A Compressor

US Patent:
2009032, Dec 31, 2009
Filed:
Jun 29, 2009
Appl. No.:
12/494158
Inventors:
Bruce A. MOODY - Kingsport TN, US
Jerry D. EDWARDS - Bristol TN, US
David R. GILLIAM - Bristol VA, US
Eugene K. CHUMLEY - Abingdon VA, US
Richard C. DENZAU - Abingdon VA, US
Scott HIX - Bristol VA, US
Justin M. TONER - Kingsport TN, US
Mark R. TRENT - Bristol VA, US
Tim M. WAMPLER - Bluff City TN, US
John R. WILLIAMS - Bristol VA, US
International Classification:
F04B 49/06
US Classification:
417 441
Abstract:
A system and method for determining a fault condition in a compressor is provided. The current of a motor drive powering the compressor and the outdoor ambient temperature are measured and used to determine if a fault condition or a potential fault condition is present in the compressor. If a fault condition is determined to be present, the compressor can be shutdown to avoid damage to the compressor. If a potential fault condition is determined, remedial action can be taken to attempt to prevent the fault condition from occurring and shutting down the compressor.


David Gilliam Photo 7

Offset Mounting Foot

US Patent:
7281907, Oct 16, 2007
Filed:
Jan 23, 2004
Appl. No.:
10/764400
Inventors:
David Rex Gilliam - Bristol VA, US
David Turner Monk - Bristol VA, US
Robert Bruce Peters - Bristol VA, US
William Terry Addison - Bristol TN, US
Assignee:
Bristol Compressors, Inc. - Bristol VA
International Classification:
F04B 17/03, F04B 35/04, F16M 1/00
US Classification:
417363, 417415, 248638
Abstract:
A single piece offset mounting foot is positioned between the compressor and the floor of a cabinet for the compressor. The offset mounting foot has a main body having a geometric shape with a top and bottom surface connected by sidewalls that form a perimeter. A depression in the top surface receives a compressor and is offset in the direction of one of the sidewalls. A plurality of substantially equally spaced legs extend outward from the main body. The thickness of the offset mounting foot may be substantially uniform through the main body. The profile of the top surface in the main body is substantially concave forming a bowl-like surface that transitions smoothly from a minimum within the concave surface or concavity to a maximum in the direction toward the periphery and in the direction away from the center of the concavity. The bottom surface of the main body is configured or profiled to contact the floor or base of the cabinet into which the compressor is to be installed.


David Gilliam Photo 8

System And Method For Starting A Compressor

US Patent:
2009032, Dec 31, 2009
Filed:
Jun 29, 2009
Appl. No.:
12/494139
Inventors:
Bruce A. MOODY - Kingsport TN, US
Eugene K. CHUMLEY - Abingdon VA, US
Richard C. DENZAU - Abingdon VA, US
Jerry D. EDWARDS - Bristol TN, US
David R. GILLIAM - Bristol VA, US
Scott HIX - Bristol VA, US
Justin M. TONER - Kingsport TN, US
Mark R. TRENT - Bristol VA, US
Tim M. WAMPLER - Bluff City TN, US
John R. WILLIAMS - Bristol VA, US
International Classification:
F04B 49/06
US Classification:
417 13, 417 53
Abstract:
A system and method for starting a compressor is provided. An amount of liquid refrigerant that is located in an oil sump of the compressor is determined. Using the determined amount of liquid refrigerant, a starting algorithm for the compressor is selected. The selected starting algorithm is configured to remove the determined amount of liquid refrigerant from the oil sump before the compressor reaches a preselected operating speed. The selected starting algorithm is then executed to start the compressor.


David Gilliam Photo 9

Muffler System For A Compressor

US Patent:
2005027, Dec 15, 2005
Filed:
Jul 26, 2005
Appl. No.:
11/189527
Inventors:
Steven Marshall - Abingdon VA, US
David Gilliam - Bristol VA, US
David Monk - Bristol VA, US
Benjamin Majerus - Bristol VA, US
Assignee:
BRISTOL COMPRESSORS, INC. - Bristol VA
International Classification:
F04B039/00, F04B053/00
US Classification:
417540000, 417312000
Abstract:
A muffler system for a compressor includes an expansion chamber muffler for reducing pressure pulses at the compressor's fundamental pulsation frequency and a side-branch muffler for filtering high-frequency pressure pulses. The expansion muffler is positioned along the compressor discharge stream at a location that maximizes pulsation reduction at the compressor's fundamental pulsation frequency. The side-branch muffler is tuned to the frequency at which the pulsation reduction for the expansion muffler is at a minimum.


David Gilliam Photo 10

Compressor Unit Housing And Methods Of Alignment

US Patent:
2005023, Oct 27, 2005
Filed:
Jun 15, 2005
Appl. No.:
11/153184
Inventors:
David Gilliam - Bristol VA, US
Steve Marshall - Abingdon VA, US
David Monk - Bristol VA, US
Benjamin Majerus - Bristol VA, US
Scott Hix - Bristol VA, US
Robert Peters - Bristol VA, US
John Narney - Bristol VA, US
Eugene Chumley - Abingdon VA, US
William Wright - Bristol VA, US
Richard Smith - Kingsport TN, US
Assignee:
BRISTOL COMPRESSORS, INC. - Bristol VA
International Classification:
F04B001/00, F04B017/00
US Classification:
417902000, 417053000
Abstract:
A hermetic compressor unit housing comprised of a shell having a top section and a bottom section which receives the top section, the shell being formed of sheet metal and having generally cylindrical sidewalls wherein the sidewall taken in a generally axial direction is substantially straight, each shell section having an opening, a substantially cylindrical portion, and a closed end portion, the opening having a substantially circular horizontal cross-sectional geometry defined by a major axis and a minor axis, the horizontal cross-sectional geometry including substantially liner opposing sidewall portions preferably disposed adjacent to the intersection of the horizontal sectional geometry with the minor axis, and methods of aligning the shell sections for installation of fixtures and mating of the shell sections.