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Henne, US
Brian A. Henne, Plymouth, WI US
| Patent application number | Description | Published |
|---|---|---|
| 20110000010 | SELF-SUSTAINING TOILET SEAT HINGE ASSEMBLY - A hinge assembly for a toilet having a bowl and a seat includes a hinge post configured to mount to the bowl. The hinge post includes a splined inner surface defining a bore. The hinge assembly also includes a pintle extending through the bore and configured to engage the seat to pivotally couple the seat to the hinge post. The pintle includes a splined portion that engages the splined inner surface of the hinge post to prevent rotation of the pintle relative to the hinge post. | 01-06-2011 |
Erik Henne, Seattle, WA US
| Patent application number | Description | Published |
|---|---|---|
| 20090138001 | Determining Patient-Specific Vapor Treatment and Delivery Parameters - Methods and systems for determining patient specific treatment parameters for delivering vapor to the lung to treat lung tissue. In some embodiments vapor is delivered to the lung to cause coagulative necrosis, inducing fibrosis and thereby reducing the volume of at least one segment of the lung. The delivery parameters can be adjusted depending on the desired degree of injury to be induced in the lung tissue. | 05-28-2009 |
| 20090301483 | Determining Patient-Specific Vapor Treatment and Delivery Parameters - Methods and systems for determining patient specific treatment parameters for delivering vapor to the lung to treat lung tissue. In some embodiments vapor is delivered to the lung to cause coagulative necrosis, inducing fibrosis and thereby reducing the volume of at least one segment of the lung. The delivery parameters can be adjusted depending on the desired degree of injury to be induced in the lung tissue. | 12-10-2009 |
Joseph Henne, Birmingham, MI US
| Patent application number | Description | Published |
|---|---|---|
| 20120038114 | BI-METAL SPIRAL WOUND GASKET - A spiral wound gasket ( | 02-16-2012 |
Kirk Henne, Belmont, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20110034487 | CXCR3 ANTAGONISTS - Compounds, compositions and methods that are useful in the treatment of inflammatory and immune conditions and diseases are provided herein. In particular, the invention provides compounds which modulate the expression and/or function of a chemokine receptor. The subject methods are useful for the treatment of inflammatory and immunoregulatory disorders and diseases, such as multiple sclerosis, rheumatoid arthritis, transplant rejection and type I diabetes. | 02-10-2011 |
Kirk Russell Henne, Belmot, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20100016353 | BENZOIMIDAZOLE DERIVATIVES USEFUL AS ANTIPROLIFERATIVE AGENTS - The invention relates to substantially pure compounds of the formula (1) and to pharmaceutically acceptable salts, prodrugs and solvates thereof, wherein R, R | 01-21-2010 |
Preston A. Henne, Hilton Head Island, SC US
| Patent application number | Description | Published |
|---|---|---|
| 20090183560 | Sub-scale sonic boom modeling - A method for modeling the acoustic signature produced by an aircraft of interest flying at a particular supersonic Mach number/altitude operating point of interest. The method includes operating a sub-scale aircraft that is a sub-scale version of the aircraft of interest at a supersonic Mach number and at an altitude that are respectively different from the Mach number and the altitude associated with the operating point of interest. The Mach number and altitude at which the sub-scale aircraft is operated is selected such that peak overpressure generated by the sub-scale aircraft and time to rise to peak overpressure are the same as peak overpressure and time to rise to peak overpressure caused by operating the aircraft of interest at the operating point of interest. | 07-23-2009 |
| 20100012777 | Supersonic Aircraft with Spike for Controlling and Reducing Sonic Boom - Method and arrangement for reducing the effects of a sonic boom created by an aerospace vehicle when said vehicle is flown at supersonic speed. The method includes providing the aerospace vehicle with a first spike extending from the nose thereof substantially in the direction of normal flight of the aerospace vehicle, the first spike having a second section aft of a first section that is aft of a leading end portion, the first and second sections having a second transition region therebetween and each of the sections having different cross-sectional areas, the leading end portion of the first spike tapering toward a predetermined cross-section with a first transition region between the predetermined cross-section and the first section. The first transition region is configured so as to reduce the coalescence of shock waves produced by the first spike during normal supersonic flight of the aerospace vehicle. A spike may also be included that extends from the tail of the aerospace vehicle to reduce the coalescence of shock waves produced by the spike during normal supersonic flight of the aerospace vehicle. | 01-21-2010 |
| 20110315819 | Supersonic Aircraft with Spike for Controlling and Reducing Sonic Boom - Method and arrangement for reducing the effects of a sonic boom created by an aerospace vehicle when said vehicle is flown at supersonic speed. The method includes providing the aerospace vehicle with a first spike extending from the nose thereof substantially in the direction of normal flight of the aerospace vehicle, the first spike having a second section aft of a first section that is aft of a leading end portion, the first and second sections having a second transition region there between and each of the sections having different cross-sectional areas, the leading end portion of the first spike tapering toward a predetermined cross-section with a first transition region between the predetermined cross-section and the first section. The first transition region is configured so as to reduce the coalescence of shock waves produced by the first spike during normal supersonic flight of the aerospace vehicle. A spike may also be included that extends from the tail of the aerospace vehicle to reduce the coalescence of shock waves produced by the spike during normal supersonic flight of the aerospace vehicle. | 12-29-2011 |
Preston A. Henne, Hilton Head, SC US
| Patent application number | Description | Published |
|---|---|---|
| 20080271787 | Isentropic compression inlet for supersonic aircraft - Embodiments of the invention relate to a supersonic inlet employing relaxed isentropic compression to improve net propulsive force by shaping the compression surface of the inlet. Relaxed isentropic compression shaping of the inlet compression surface functions to reduce cowl lip surface angles, thereby improving inlet drag characteristics and interference drag characteristics. Using supersonic inlets in accordance with the invention also demonstrated reductions in peak sonic boom overpressure while maintaining performance. | 11-06-2008 |
Randal M. Henne, Seattle, WA US
| Patent application number | Description | Published |
|---|---|---|
| 20100197895 | ANTIBODIES TO HUMAN TUMOR NECROSIS FACTOR RECEPTOR - Tumor necrosis factors and their receptors have proven usefulness in both basic research and as therapeutics. The present invention provides a new human tumor necrosis factor receptor designated as “Ztnfr12.” | 08-05-2010 |
Walter Henne, West Lafayette, IN US
| Patent application number | Description | Published |
|---|---|---|
| 20100330702 | ULTRASENSITIVE DETECTION OF BIOMOLECULES USING IMMUNOSEPARATION AND DIFFRACTOMETRY - Systems and methods for rapid and ultrasensitive detection of target hiomolecules in a sample are presented. The detection of biomolecules is achieved through a synergistic use of immunoseparation and diffractomctry, and the formation of antibody-biomolecule-ligand sandwich complexes that form diffraction gratings. Characteristic diffraction patterns are then produced upon illumination of the diffraction gratings with light. The diffraction patterns can he used to detect very low amounts of biomolecules present in the sample. | 12-30-2010 |
Walter Anthony Henne, Lafayette, IN US
| Patent application number | Description | Published |
|---|---|---|
| 20080254499 | Multiphoton in Vivo Flow Cytometry Method and Device - The invention relates to a method for diagnosing a disease state mediated by pathogenic cells, said method comprising the steps of administering to a patient a composition comprising a conjugate or complex of the general formula | 10-16-2008 |