BRIAN EDGAR NEAL, M.D.
Psychiatric in Seattle, WA

License number
Washington MD60641525
Category
Psychiatric
Type
Psychiatry
License number
Washington 252712
Category
Psychiatric
Type
Psychiatry
Address
Address
1100 9 Ave Ms:c8-Gim, Seattle, WA 98101
Phone
(206) 233-6762
(206) 625-7414 (Fax)

Personal information

See more information about BRIAN EDGAR NEAL at radaris.com
Name
Address
Phone
Brian Neal
4729 Shellridge Rd NW, Olympia, WA 98502
(360) 866-2579
Brian Neal
3705 Canterbury Ln, Bellingham, WA 98225
(360) 734-7530
Brian Neal
456 Centaurus Ave SW, Ocean Shores, WA 98569
Brian Neal, age 51
924 E 59Th St, Tacoma, WA 98404
(253) 476-1169
Brian Neal
8994 SE View Park Rd, Port Orchard, WA 98367
(360) 871-4933

Professional information

Brian Neal Photo 1

Project Manager At Ccs Printing

Position:
Project Manager/Major Acct Program Coordinator at CCS printing
Location:
Greater Seattle Area
Industry:
Printing
Work:
CCS printing since Jan 2000 - Project Manager/Major Acct Program Coordinator


Brian Neal Photo 2

Intregal Wing Fuel Cell Mechanic At Boeing Commercial Airplanes

Position:
intregal wing fuel cell mechanic at Boeing Commercial Airplanes
Location:
Greater Seattle Area
Industry:
Aviation & Aerospace
Work:
Boeing Commercial Airplanes - intregal wing fuel cell mechanic


Brian Neal Photo 3

Noise Suppressing Exhaust Mixer Assembly For Ducted-Fan, Turbojet Engine

US Patent:
4117671, Oct 3, 1978
Filed:
Dec 30, 1976
Appl. No.:
5/755837
Inventors:
Brian Neal - Seattle WA
Lars Q. Andersen - Bothell WA
Assignee:
The Boeing Company - Seattle WA
International Classification:
F02K 126, F02K 304
US Classification:
60262
Abstract:
To suppress jet noise emanating from a ducted-fan turbojet engine, an improved exhaust mixer assembly is disclosed that is mounted between the engine and the exhaust nozzle and that mixes the flow of high-velocity primary gases (turbine exhaust) with the lower-velocity air from the fan duct in a manner that achieves a significant reduction in the proportion of noise-causing high velocity gases while maintaining approximately the same thrust from the nozzle as other mixer-equipped engines. The mixer assembly includes an annular sleeve, a bulb-shaped plug disposed concentrically within the sleeve, and an annular corregugated mixer duct coaxially positioned between the plug and sleeve wherein these components are arranged so as to receive the primary and fan flows and separately redirect these flows within the assembly so that the flow of primary gases is rearwardly divergent while the flow of fan air is rearwardly convergent. As the primary and fan flows pass through a mixing plane at the aft terminus of the mixer duct, they intersect in a crossing pattern resulting from their divergent-convergent flow paths which yields faster and more complete mixing of the flows before they are discharged from the nozzle. The shaping and dimensioning of the sleeve, plug, and mixer duct are such that optimum mixing, and thus maximum suppression of noise, are achieved without introducing any excessive pressure losses in the mixer assembly and nozzle that otherwise would significantly diminish thrust.