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Dwight D.

Dwight D. Koeberl, Durham, NC US

Patent application numberDescriptionPublished
20110070220Immunomodulating gene therapy - The present invention relates, in general, to Pompe disease and, in particular, to a methods of treating Pompe disease and to compounds/constructs suitable for use in such methods.03-24-2011

Dwight D. Locsin, Morgan Hill, CA US

Patent application numberDescriptionPublished
20100323852YOKE TRAINING SYSTEM - A yoke training system and method comprising a yoke bar suspended from an overhead mount via a suspension line connected to a swivel on the yoke bar. The yoke bar is able to freely rotate in 360 degrees and freely move front to back, back to front, and side to side. The free moving yoke bar assists the user in positioning himself in compromising positions where he is challenged to stabilize himself by entering into isometric contraction of the core and perform movements such as strength building exercise using the yoke bar in one of the sagitall, frontal and transverse planes, two or more of the planes simultaneously or sequentially, or any combination of the different or same planes simultaneously or sequentially. The user may reposition the bar and take on a new position when entering into isometric contraction again. Thus the user movement may be performed in different body positions of isometric contraction. Attachment devices may be connected to enhance effectiveness.12-23-2010

Dwight D. Schmiu, Rockford, IL US

Patent application numberDescriptionPublished
20100019862Lightweight Electromagnetic Interference Filter - A low pass filter includes a differential mode filter and a common mode filter. The common mode portion of the filter includes at least one inductor and one capacitor, as well as a damping circuit with at least one capacitor. The low pass filter has a reduced weight, which is useful in circumstances in which weight is a significant factor, such as in aircraft.01-28-2010

Dwight D. Vettel, Chandler, AZ US

Patent application numberDescriptionPublished
20080307769GAS TURBINE ENGINE ANTI-ICE FORMATION DEVICE AND SYSTEM - An anti-ice formation device for a gas turbine engine is configured to be mounted within an inlet duct of the engine, and adjacent the gas turbine engine compressor inlet. The device is configured to selectively receive a flow of compressed air that is discharged from the compressor. Because the compressed air is relatively hot, the anti-ice formation device temperature increases to a temperature sufficient to prevent ice accumulation and formation in the engine inlet duct. The anti-ice formation device is also configured such that heat is not transferred to the compressor inlet housing. As a result, the anti-ice formation device does not cause impeller clearance variations, which would adversely affect engine performance.12-18-2008