Research/Patents/US 5351889
US 5351889

FLOW TRIPPED INJECTOR

Assignee

UNITED STATES OF AMERIA, THE, AS REPRESENTED BY THE SECRETARY OF THE NAVY

Filed

Oct 16, 1991

Granted

Oct 4, 1994

Location

San Diego CA (SAIC/General Dynamics)

Abstract

A turbulent flow injector includes a ceramic injector body having an outerylindrical wall with an inner surface, an inner cylindrical wall having an inner surface, an end wall at an outlet end of the body terminating the outer and inner walls so as to define an annular cavity between the inner and outer walls. The annular cavity is open at an inlet end of the body. A duct, defined by the inner surface of the inner wall, has an inlet at the inlet end of the body. A heat conductive insert is positioned within the annular cavity and has an outer surface in thermal contact with the inner surface of the outer wall. The insert has an external section extending beyond the inlet end of the body and cooling fins extending from the external section. An annular air chamber is defined between the insert and the inner wall of the body. An important feature of the invention is a protuberance mounted at the inlet end of the body and radially extending over the inlet of the duct for inducing turbulent flow in a fluid flowing through the duct.

Source: Google Patents

35 USC §181 Secrecy Order

Imposed

Dec 23, 1991

Rescinded

Feb 18, 1994

Duration

2 years, 1 month

Inventor

  • 1STEVEN K. WHITESIDE

Sensitive facility: San Diego CA (SAIC/General Dynamics)

Record Details

Patent number
US 5351889
Application
07777031
Aerospace match
No
Dataset source
35 USC §181 SO records
Back to patent indexSource: USPTO 35 USC §181 secrecy order records