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David Bulman

In the United States, there are 52 individuals named David Bulman spread across 30 states, with the largest populations residing in California, New York, Florida. These David Bulman range in age from 34 to 72 years old. Some potential relatives include Valeshia Wilson, Alicia Williams, Vaughn Wilson. You can reach David Bulman through various email addresses, including kelso8***@aol.com, david.bul***@rochester.rr.com, david.bul***@aol.com. The associated phone number is 319-377-0864, along with 6 other potential numbers in the area codes corresponding to 518, 563, 864. For a comprehensive view, you can access contact details, phone numbers, addresses, emails, social media profiles, arrest records, photos, videos, public records, business records, resumes, CVs, work history, and related names to ensure you have all the information you need.

Public information about David Bulman

Resumes

Resumes

David Bulman

David Bulman Photo 1
Location:
United States

Medic At Tjuh

David Bulman Photo 2
Location:
Greater Philadelphia Area
Industry:
Hospital & Health Care

National Sales Manager, Brasseler Usa Medical Llc

David Bulman Photo 3
Position:
National Sales Manager at Brasseler USA
Location:
Savannah, Georgia
Industry:
Medical Devices
Work:
Brasseler USA - Savannah, GA since Nov 2011
National Sales Manager Brasseler USA 2005 - 2007
National Sales Manager - Surgical Division
Education:
Villanova University 1981 - 1985
BS, Accounting
Skills:
Management, Operating Room, Medical Devices, Sales Operations, Surgeons, Capital Equipment, Sales Force Development

David Bulman - Orange, CA

David Bulman Photo 4
Work:
The Home Depot 2006 to 2013
Tool rental technician-Responsable panasonic disc. corp - Torrance, CA 2001 to 2006
Machine repair technician-responsable Cinram inc - Anaheim, CA 1996 to 2001
Machine repair technician-responsable for improvement, set US equipment rentals - Fullerton, CA 1993 to 1994
Mechanic

David Bulman - Raleigh, NC

David Bulman Photo 5
Work:
TAC Air, RDU International Airport 2011 to 2000
Line Service Technician Walgreen Company - Greenfield, MA 2009 to 2010
Pharmacy Technician Greenfield Middle School - Greenfield, MA 2009 to 2010
Title I Paraprofessional FedEx Office - Greenville, NC 2006 to 2008
Senior Project Coordinator
Education:
Westfield State College - Westfield, MA 2004
Bachelor of English Greenfield Community College - Greenfield, MA 2002
Liberal Arts

David Bulman

David Bulman Photo 6
Location:
Glens Falls, New York Area
Industry:
Hospital & Health Care

Manager, Advanced Mechanical Design At Ge Aviation

David Bulman Photo 7
Position:
Manager, Advanced Mechanical Design at GE Aviation
Location:
Cincinnati Area
Industry:
Airlines/Aviation
Work:
GE Aviation
Manager, Advanced Mechanical Design

Student At The Johns Hopkins University - Paul H. Nitze School Of Advanced International Studies (Sais)

David Bulman Photo 8
Location:
Washington D.C. Metro Area
Industry:
International Affairs
Education:
The Johns Hopkins University - Paul H. Nitze School of Advanced International Studies (SAIS) 2008 - 2013
MA (2010); PhD, China Studies and International Economics Columbia University in the City of New York 2001 - 2005
BA, Economics

Phones & Addresses

Name
Addresses
Phones
David Bulman
413-549-5637
David Bulman
508-872-1908
David Bulman
319-377-0864
David Bulman
413-253-9473, 413-256-3060
David Bulman
775-297-3379
David Bulman
518-459-3780
David N Bulman
518-793-5524, 518-538-0122, 518-793-5545
David N Bulman
518-793-5524, 518-793-5545

Publications

Us Patents

Turbine Engine Shroud Segment, Hanger And Assembly

US Patent:
7052235, May 30, 2006
Filed:
Jun 8, 2004
Appl. No.:
10/863434
Inventors:
Mary Ellen Alford - Cincinnati OH, US
David Edward Bulman - Cincinnati OH, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 25/28
US Classification:
4151731
Abstract:
A turbine engine shroud segment comprises a body including an outer surface from and along which a segment projection extends away from and in an axial direction. The segment projection includes circumferentially spaced apart segment support surfaces. A shroud hanger comprises a body including an inner surface from and along which a hanger projection extends in an axial direction. The hanger projection includes circumferentially spaced hanger bearing surfaces. In a circumferential turbine engine shroud assembly of shroud segments and hangers, a shroud hanger is assembled between a pair of adjacent shroud segments separated by an axial interface. The hanger projection is in juxtaposition with the interface, and respective segment support surfaces and hanger bearing surfaces are in registry.

Bolting Configuration For Joining Ceramic Combustor Liner To Metal Mounting Attachments

US Patent:
7546743, Jun 16, 2009
Filed:
Oct 12, 2005
Appl. No.:
11/247129
Inventors:
David Edward Bulman - Cincinnati OH, US
Mark Stewart Schroder - Hendersonville NC, US
John Joseph Lipinski - Simpsonville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F23R 3/60
US Classification:
60796, 60753
Abstract:
A gas turbine combustor includes a substantially cylindrical combustor liner located substantially concentrically within a flow sleeve, the combustor liner composed through a ceramic matrix composite material, a forward end of the combustor liner provided with a plurality of circumferentially arranged bolt holes. An inner metal ring is located about an outside surface of the forward end of the combustor liner, the inner metal ring provided with a second plurality of circumferentially spaced bolt holes, with a plurality of bolts extending through the first and second pluralities of bolt holes and secured by self-locking nuts. An outer metal ring is spaced radially outwardly of the inner metal ring, with a plurality of circumferentially spaced struts extending between the inner and outer rings.

Methods And Apparatus For Directing Airflow To A Compressor Bore

US Patent:
6361277, Mar 26, 2002
Filed:
Jan 24, 2000
Appl. No.:
09/490625
Inventors:
David E. Bulman - Cincinnati OH
Kenneth E. Seitzer - Mason OH
Craig P. Burns - Mason OH
Jeffrey D. Clements - Mason OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 508
US Classification:
416 96R, 416198 A
Abstract:
A gas turbine engine includes a compressor rotor assembly which directs air at a sufficent pressure and temperature to a compressor rotor bore. The compressor assembly includes a compressor including a plurality of rotors joined with a plurality of couplings. Each of the rotors includes a radially outer rim, a radially inner hub, and a web extending therebetween. The web includes a flange including a plurality of slots which define a plurality of radial vanes that are airfoil-shaped. The vanes effectively deswirl bleed air and re-direct the airflow to a compressor bore.

Methods And Apparatus For Radially Compliant Component Mounting

US Patent:
8141370, Mar 27, 2012
Filed:
Aug 8, 2006
Appl. No.:
11/463142
Inventors:
David Edward Bulman - Cincinnati OH, US
James Anthony Stumpf - Columbus IN, US
Mark S. Schroder - Greenville SC, US
John Joseph Lipinski - Simpsonville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F02C 7/20
US Classification:
60796, 60752
Abstract:
Methods and apparatus for a mounting assembly for a liner of a gas turbine engine combustor are provided. The combustor includes a combustor liner and a radially outer annular flow sleeve. The mounting assembly includes an inner ring surrounding a radially outer surface of the liner and including a plurality of axially extending fingers. The mounting assembly also includes a radially outer ring coupled to the inner ring through a plurality of spacers that extend radially from a radially outer surface of the inner ring to the outer ring.

Pitch Change Mechanism For Prop Fans

US Patent:
5152668, Oct 6, 1992
Filed:
Jul 23, 1990
Appl. No.:
7/556155
Inventors:
David E. Bulman - Cincinnati OH
Petr Hora - West Chester OH
Thomas C. Hermans - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
B64C 1132
B64C 1148
US Classification:
416129
Abstract:
The invention relates to pitch-change systems in aircraft propellers. The invention includes redundant planetary gear systems, each of which can independently change pitch if the other fails. The invention also includes a system for reducing displacement of the planets, which can occur during a failure.

Reduced-Stress Compressor Blisk Flowpath

US Patent:
6511294, Jan 28, 2003
Filed:
Sep 23, 1999
Appl. No.:
09/405308
Inventors:
Mark J. Mielke - Blanchester OH
James E. Rhoda - Mason OH
David E. Bulman - Cincinnati OH
Craig P. Burns - Mason OH
Paul M. Smith - Loveland OH
Daniel G. Suffoletta - Cincinnati OH
Steven M. Ballman - West Chester OH
Richard P. Zylka - Cincinnati OH
Lawrence J. Egan - Mason OH
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 522
US Classification:
416193A, 416201 R
Abstract:
A gas turbine engine rotor assembly including a rotor having a radially outer rim with an outer surface shaped to reduce circumferential rim stress concentration between each blade and the rim. Additionally, the shape of the outer surface directs air flow away from an interface between a blade and the rim to reduce aerodynamic performance losses between the rim and blades. In an exemplary embodiment, the outer surface of the rim has a concave shape between adjacent blades with apexes located at interfaces between the blades and the rim.

Bladed Disk Assembly

US Patent:
5259728, Nov 9, 1993
Filed:
May 8, 1992
Appl. No.:
7/880441
Inventors:
Stephen J. Szpunar - West Chester OH
David E. Bulman - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 530
US Classification:
416 2
Abstract:
A bladed disk assembly includes a rotor disk having an axial dovetail slot, and a rotor blade having a dovetail disposed in the slot. A blade retainer is fixedly joined to the disk for retaining the dovetail in the slot. A spacer is disposed in the slot between the blade retainer and the dovetail and is selectively compressible for allowing the dovetail to slide in the slot toward the blade retainer for generating friction forces to dissipate energy upon impact of a predeterminedly sized foreign object.

Torque Multiplier For Aircraft Propeller

US Patent:
5154372, Oct 13, 1992
Filed:
Jul 23, 1990
Appl. No.:
7/556676
Inventors:
Peter Hora - West Chester OH
David E. Bulman - Cincinnati OH
Thomas C. Hermans - Cincinnati OH
Thomas G. Wakeman - Lawrenceburg IN
Walter D. Howard - Cincinnati OH
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 124
F04D 2926
US Classification:
244 62
Abstract:
The invention concerns aircraft propellers of the variable pitch type. Each propeller blade is carried by a trunnion which is rotatably mounted to a common ring. Each trunnion contains a reduction gear set which is driven by a radial shaft. The reduction gear sets multiply the torque applied by the shafts, thus allowing shafts of reduced diameter to be used. The reduced diameter is important when the shafts must pass through a turbine flowpath, and thus be concealed within turbine blades. The reduced diameter shafts can be easily concealed within turbine blades without redesigning and compromising blade aerodynamics.

FAQ: Learn more about David Bulman

What are the previous addresses of David Bulman?

Previous addresses associated with David Bulman include: 438 Delynn Dr, Hazel Green, AL 35750; 952 E Sterling Ln, Flagstaff, AZ 86001; 1931 E Meats Ave, Orange, CA 92865; 26018 Cayuga, Lomita, CA 90717; 3236 Curtis St, San Diego, CA 92106. Remember that this information might not be complete or up-to-date.

Where does David Bulman live?

Waukon, IA is the place where David Bulman currently lives.

How old is David Bulman?

David Bulman is 61 years old.

What is David Bulman date of birth?

David Bulman was born on 1963.

What is David Bulman's email?

David Bulman has such email addresses: kelso8***@aol.com, david.bul***@rochester.rr.com, david.bul***@aol.com, nanatur***@hotmail.com, b***@wmconnect.com, dait***@earthlink.com. Note that the accuracy of these emails may vary and they are subject to privacy laws and restrictions.

What is David Bulman's telephone number?

David Bulman's known telephone numbers are: 319-377-0864, 518-459-3780, 518-793-5545, 563-568-2947, 864-598-9013, 904-823-1188. However, these numbers are subject to change and privacy restrictions.

How is David Bulman also known?

David Bulman is also known as: David Bulman, David L Bulman, Donna Bulman, Dave Bulman, Daid Bulman, Stacey M Bulman. These names can be aliases, nicknames, or other names they have used.

Who is David Bulman related to?

Known relatives of David Bulman are: Christopher Shelton, Rick Clark, David Bulman, Danielle Bulman, Donna Bulman, Jacqueline Bulman, Joshua Bulman, Kenneth Bulman, Lesa Bulman, Louise Bulman, Nathaniel Bulman, Stacey Bulman, Jennifer Crain, Misty Frye, Patrick Hickman, Jane Ryderson. This information is based on available public records.

What are David Bulman's alternative names?

Known alternative names for David Bulman are: Christopher Shelton, Rick Clark, David Bulman, Danielle Bulman, Donna Bulman, Jacqueline Bulman, Joshua Bulman, Kenneth Bulman, Lesa Bulman, Louise Bulman, Nathaniel Bulman, Stacey Bulman, Jennifer Crain, Misty Frye, Patrick Hickman, Jane Ryderson. These can be aliases, maiden names, or nicknames.

What is David Bulman's current residential address?

David Bulman's current known residential address is: 673 Bethlehem Dr, Waukon, IA 52172. Please note this is subject to privacy laws and may not be current.

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