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Klinge
Carolyn M. Klinge, Louisville, KY US
| Patent application number | Description | Published |
|---|---|---|
| 20110100817 | MICROFLUIDIC DEVICES AND METHODS OF USING SAME - The presently-disclosed subject matter provides microfluidic devices comprised of two or more carbon nanotube membranes disposed at predetermined intervals within a microchannel. Further provided are methods of using the same for the electrokinetic separation of one or more molecules of interest from a sample. | 05-05-2011 |
Dagmar Klinge, Schriesheim DE
| Patent application number | Description | Published |
|---|---|---|
| 20110178294 | NOVEL CARBOXYLIC ACID DERIVATIVES, THEIR PREPARATION AND USE - Carboxylic acid derivatives | 07-21-2011 |
Dagmar Klinge, Heidelberg DE
| Patent application number | Description | Published |
|---|---|---|
| 20100076188 | NOVEL CARBOXYLIC ACID DERIVATIVES, THEIR PREPARATION AND USE - Carboxylic acid derivatives | 03-25-2010 |
John D. Klinge, Palmdale, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20100051756 | SYSTEM, METHOD, AND APPARATUS FOR THROAT CORNER SCOOP OFFTAKE FOR MIXED COMPRESSION INLETS ON AIRCRAFT ENGINES - A system, method, and apparatus for throat corner scoop offtake for mixed compression inlets for high speed aircraft engine applications is disclosed. The throat corner scoops are small air intakes located inside the large mixed compression inlet. They are positioned in a region otherwise prone to generate low pressure airflow. The throat corner scoops capture and remove the low pressure airflow from the bulk stream that is passed on to the engine. This location also provides inlet stability enhancement, and the airflow is used on the auxiliary systems. | 03-04-2010 |
John D. Klinge, Fort Worth, TX US
| Patent application number | Description | Published |
|---|---|---|
| 20090094987 | APPARATUS AND METHOD FOR PROCESSING AIRFLOW WITH FLOWFIELD MOLDED HYPERSONIC INLET - A diverterless hypersonic inlet (DHI) for a high speed, air-breathing propulsion system reduces the ingested boundary layer flow, drag, and weight, and maintains a high capture area for hypersonic applications. The design enables high vehicle fineness ratios, low-observable features, and enhances ramjet operability limits. The DHI is optimized for a particular design flight Mach number. A forebody segment generates and focuses a system of multiple upstream shock waves at desired strengths and angles to facilitate required inlet and engine airflow conditions. The forebody contour diverts boundary layer flow to the inlet sides, effectively reducing the thickness of the boundary layer that is ingested by the inlet, while maintaining the capture area required by the hypersonic propulsion system. The cowl assembly is shaped to integrate with the forebody shock system and the thinned boundary layer region. | 04-16-2009 |
Kelly L. Klinge, Ames, IA US
| Patent application number | Description | Published |
|---|---|---|
| 20100129398 | Materials and Methods for Control of Porcine Reproductive and Respiratory Syndrome - Methods of reducing the severity of porcine reproductive and respiratory syndrome virus (PRRSV) infections, as well as, methods of preventing such infections are provided. The methods provide for the age-based innoculation of swine with PRRS antigen, preferably Ingelvac® ATP. | 05-27-2010 |
Timo Klinge, Munich DE
| Patent application number | Description | Published |
|---|---|---|
| 20110242943 | Hydrophone and Hydrophone Assembly for Performing Stereophonic Underwater Sound Recordings - A hydrophone for recording underwater sound includes a housing having an outer surface designed to serve as a boundary surface for an incident sound wave and at least one vibration sensor having a sensor surface for recording sound waves and for preparing a sensor signal. The sensor surface of the vibration sensor is in an opening of the housing. A hydrophone assembly includes a plurality of the hydrophones. | 10-06-2011 |