Klinge; John D.

Patent Applications and Registrations

Patent applications and USPTO patent grants for Klinge; John D..The latest application filed is for "aircraft, propulsion system, and inlet with supersonic compression".

Company Profile

0.6.7

Klinge; John D. - Palmdale CA US
Klinge; John D. - Fort Worth TX

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Aircraft, propulsion system, and inlet with supersonic compression Grant 8,915,061 - Anderson , et al. December 23, 2	2014-12-23
Aircraft, Propulsion System, And Inlet With Supersonic Compression App 20130199621 - Anderson; Jon T. ; et al.	2013-08-08
Apparatus and method for processing airflow with flowfield molded hypersonic inlet Grant 8,297,058 - Leland , et al. October 30, 2	2012-10-30
System, method, and apparatus for throat corner scoop offtake for mixed compression inlets on aircraft engines Grant 7,690,595 - Leland , et al. April 6, 2	2010-04-06
System, Method, And Apparatus For Throat Corner Scoop Offtake For Mixed Compression Inlets On Aircraft Engines App 20100051756 - Leland; Bradley C. ; et al.	2010-03-04
Method for designing flowfield molded hypersonic inlet for integrated turbojet and ram-scramjet applications Grant 7,568,347 - Leland , et al. August 4, 2	2009-08-04
Apparatus And Method For Processing Airflow With Flowfield Molded Hypersonic Inlet App 20090094987 - Leland; Bradley C. ; et al.	2009-04-16
Method for streamline traced external compression inlet App 20070181743 - Klinge; John D. ; et al.	2007-08-09
System, method, and apparatus for diverterless hypersonic inlet for integrated turbojet and ram-scramjet applications App 20070136032 - Leland; Bradley C. ; et al.	2007-06-14
System, method, and apparatus for designing streamline traced, mixed compression inlets for aircraft engines Grant 7,207,520 - Lundy , et al. April 24, 2	2007-04-24
System, method, and apparatus for designing streamline traced, mixed compression inlets for aircraft engines App 20060266412 - Lundy; Brian F. ; et al.	2006-11-30

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