The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 21, 2018

Filed:

Jul. 26, 2013
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Dan J. Baruzzini, Keller, TX (US);

Daniel N. Miller, Bainbridge Island, WA (US);

Neal D. Domel, Fort Worth, TX (US);

Jeff G. Hakes, Mansfield, TX (US);

Assignee:

Lockheed Martin Corporation, Bethesda, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 21/04 (2006.01); F02C 7/04 (2006.01); F15D 1/00 (2006.01); B64C 21/02 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/04 (2013.01); B64C 21/025 (2013.01); F15D 1/0095 (2013.01); B64D 2033/026 (2013.01); B64D 2033/0226 (2013.01); Y02T 50/166 (2013.01); Y10T 137/0318 (2015.04); Y10T 137/0536 (2015.04);
Abstract

An apparatus for suppressing shock-induced separation of high speed airflow from a relatively low-energy boundary layer. The apparatus may include an actuator or array of actuators configured to alternately inhale and exhale fluid and positioned to alternately inhale fluid from and exhale fluid into a boundary layer of a fluid mass flowing along the wall. The actuator may be positioned to inhale fluid from a boundary layer separation bubble induced by a supersonic shock wave propagated in the fluid mass.


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