JACK ANDERSON
Medical Practice at Klish Way, Del Mar, CA
License number
Alaska MEDS3245
Issued Date
Apr 5, 1994
Effective Date
Dec 12, 2014
Expiration Date
Dec 31, 2016
Category
Medical
Address
Address
1122 Klish Way, Del Mar, CA 92014
Professional information
Jack Anderson - Del Mar, CA
Work:
American Income
Senior Supervising Agent San Diego Marketing Group - San Diego, CA
Sales Associate and Outsourcing for Quill.com Yogi's Restaurant Brown University Theta Delta Chi Fraternity
Treasurer Yogi's Restaurant - Providence, RI
Internship Brown University Theta Delta Chi Fraternity Brown University Theta Delta Chi Fraternity - Providence, RI
Volunteer Tutor Yogi's Restaurant - Providence, RI Yogi's Restaurant - Murrieta, CA Nancy Fuller Jacobs and Associates Brown University Basketball Team Torrey Pines High School - San Diego, CA
Assistant Basketball Coach Volunteer Assistant Basketball Coach - Special Olympics - San Diego, CA
Senior Supervising Agent San Diego Marketing Group - San Diego, CA
Sales Associate and Outsourcing for Quill.com Yogi's Restaurant Brown University Theta Delta Chi Fraternity
Treasurer Yogi's Restaurant - Providence, RI
Internship Brown University Theta Delta Chi Fraternity Brown University Theta Delta Chi Fraternity - Providence, RI
Volunteer Tutor Yogi's Restaurant - Providence, RI Yogi's Restaurant - Murrieta, CA Nancy Fuller Jacobs and Associates Brown University Basketball Team Torrey Pines High School - San Diego, CA
Assistant Basketball Coach Volunteer Assistant Basketball Coach - Special Olympics - San Diego, CA
Education:
Brown University
Bachelor of Arts in Economics Brown University
High School Diploma Torrey Pines High School - San Diego, CA
Bachelor of Arts in Economics Brown University
High School Diploma Torrey Pines High School - San Diego, CA
Jet Nozzle Mixer
US Patent:
7111448, Sep 26, 2006
Filed:
Jan 4, 2005
Appl. No.:
11/027981
Inventors:
Jack H. Anderson - Del Mar CA, US
International Classification:
F02K 1/48, F02K 1/60
US Classification:
60204, 602262, 60262, 23926517, 181220
Abstract:
An external jet nozzle mixer includes identically formed lobes. The external mixer works with the internal mixer further to mix the engine internal bypass flow with the internal jet engine core flow to level the disparate flow velocities, to reduce the peak velocities from the jet engine core and increase the lower bypass velocities of the engine internal bypass flow, and thereby reduce noise. The internal lobe contours act as lifting flutes, causing mixing of the primary hot and cold flows to mix before exiting the nozzle. The external lobe contours act as venturi chutes, accelerating the cooler ambient secondary air flow. The lobes thus act collectively as an injector to force the cooler ambient secondary flow into the previously mixed primary flow as it exits the nozzle. Also obtained is an increased thrust efficiency and a consequently decreased fuel consumption and engine emissions.
Jet Nozzle Mixer
US Patent:
7017331, Mar 28, 2006
Filed:
Feb 20, 2004
Appl. No.:
10/783839
Inventors:
Jack H. Anderson - Del Mar CA, US
International Classification:
F02K 1/54, F02K 1/46
US Classification:
60204, 60262, 60264, 23926519, 181220
Abstract:
A second stage external jet nozzle mixer () includes identically formed lobes which equal in number the lobes of the first stage internal mixer. The external mixer works with the internal mixer, and furthers the mixing of the jet engine internal bypass flow with the internal jet engine core flow. This mixing levels the disparate flow velocities attendant with the jet engine exhaust, reduces the peak velocities from the jet engine core and increases the lower bypass velocities of the jet engine internal bypass flow. The lobes include complex curvatures that greatly enhance mixing of the gases and ambient cooling air, and thereby reduce noise. At the lobe terminus, the lobe dimensional characteristics may be adjusted to thereby adjust the total terminus area to achieve a match to a jet engine to cause that jet engine to run at a determined RPM and noise level. Noise attenuation may also be adjusted by changing lobe dimensions. Prior existing second stage exhaust jet nozzle mixers may be retrofitted to allow alteration of their total terminus area by employing the disclosed device and method.
Jet Nozzle Mixer
US Patent:
7251927, Aug 7, 2007
Filed:
Feb 6, 2006
Appl. No.:
11/347320
Inventors:
Jack H Anderson - Del Mar CA, US
International Classification:
F02K 1/08, F02K 1/48
US Classification:
60204, 60262, 60264, 23926543, 181220
Abstract:
A second stage external jet nozzle mixer () includes identically formed lobes which equal in number the lobes of the first stage internal mixer. The external mixer works with the internal mixer, and furthers the mixing of the jet engine internal bypass flow with the internal jet engine core flow. This mixing levels the disparate flow velocities attendant with the jet engine exhaust, reduces the peak velocities from the jet engine core and increases the lower bypass velocities of the jet engine internal bypass flow. The lobes include complex curvatures that greatly enhance mixing of the gases and ambient cooling air, and thereby reduce noise. At the lobe terminus, the lobe dimensional characteristics may be adjusted to thereby adjust the total terminus area to achieve a match to a jet engine to cause that jet engine to run at a determined RPM and noise level. Noise attenuation may also be adjusted by changing lobe dimensions. Prior existing second stage exhaust jet nozzle mixers may be retrofitted to allow alteration of their total terminus area by employing the disclosed device and method.
Jet Nozzle Mixer
US Patent:
8069647, Dec 6, 2011
Filed:
Jul 25, 2006
Appl. No.:
11/491993
Inventors:
Jack H. Anderson - Del Mar CA, US
Assignee:
Comtran Limited - St. Peter Port
International Classification:
F02K 1/54, F02K 1/46
US Classification:
60204, 602261, 60262, 60770, 23926517, 181220
Abstract:
An external jet nozzle mixer includes identically formed lobes. The external mixer works with the internal mixer further to mix the engine internal bypass flow with the internal jet engine core flow to level the disparate flow velocities, to reduce the peak velocities from the jet engine core and increase the lower bypass velocities of the engine internal bypass flow, and thereby reduce noise. The internal lobe contours act as lifting flutes, causing mixing of the primary hot and cold flows to mix before exiting the nozzle. The external lobe contours act as venturi chutes, accelerating the cooler ambient secondary air flow. The lobes thus act collectively as an injector to force the cooler ambient secondary flow into the previously mixed primary flow as it exits the nozzle. Also obtained is an increased thrust efficiency and, consequently, decreased fuel consumption and engine emissions.