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Dizdarevic
Faruk Dizdarevic, Anaheim, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20100163670 | DELTOID MAIN WING AERODYNAMIC CONFIGURATIONS - Deltoid Main Wing idea provides for several innovative aerodynamic configurations for large subsonic and supersonic civil and military aircraft including “T-tailed Deltoid Main Wing” configuration that allows for design of high-subsonic jumbo jet passenger aircraft with a capacity between 200 and 700 passengers whose outer dimensions fit within 80 m box on class VI airports while having more than twice lower fuel consumption per unit of payload when compared to the present classical-concept aircraft with the same passenger capacity, while further allowing for design of all-size and all-purpose, high-lift-capacity, and long-range unmanned aircraft. | 07-01-2010 |
| 20100224735 | CANARDED DELTOID MAIN WING AIRCRAFT - Canarded deltoid main wing aircraft idea allows for design of large supersonic civil and military aircraft with cruising speeds of up to Mach 3 at the altitude of over 25,000 meters. The fuel consumption per unit of payload of such aircraft would be at least twice lower with a longer range of over 50% when compared to existing supersonic aircraft of the same size. Simultaneously, the flight safety and ride quality during takeoff and landing at low speeds would be similar to the existing subsonic passenger aircraft. A low fuel consumption, long range, high ride quality, and high flight safety of these aircraft are widely opening a door for design of supersonic long range continental and intercontinental passenger aircraft that would be highly competitive with existing long range high subsonic passenger aircraft. | 09-09-2010 |
Ismar Dizdarevic, Nutley, NJ US
| Patent application number | Description | Published |
|---|---|---|
| 20100124535 | Aerosol Dispersions of Particles with Active Pharmaceutical Ingredients - Aerosols containing a plurality of aqueous droplets, each droplet containing on average at least one essentially-neutral particle sized to fit within the droplet are provided. Aerosols wherein an active pharmaceutical ingredient is attached to, or otherwise incorporated in the essentially neutral particles are also provided. Methods for administering an active pharmaceutical ingredient to a subject in need thereof via inhalation of these aerosols, preferably via nebulizer, are also provided. | 05-20-2010 |
Mithad Dizdarevic, Anaheim, CA US
| Patent application number | Description | Published |
|---|---|---|
| 20100163670 | DELTOID MAIN WING AERODYNAMIC CONFIGURATIONS - Deltoid Main Wing idea provides for several innovative aerodynamic configurations for large subsonic and supersonic civil and military aircraft including “T-tailed Deltoid Main Wing” configuration that allows for design of high-subsonic jumbo jet passenger aircraft with a capacity between 200 and 700 passengers whose outer dimensions fit within 80 m box on class VI airports while having more than twice lower fuel consumption per unit of payload when compared to the present classical-concept aircraft with the same passenger capacity, while further allowing for design of all-size and all-purpose, high-lift-capacity, and long-range unmanned aircraft. | 07-01-2010 |
| 20100224735 | CANARDED DELTOID MAIN WING AIRCRAFT - Canarded deltoid main wing aircraft idea allows for design of large supersonic civil and military aircraft with cruising speeds of up to Mach 3 at the altitude of over 25,000 meters. The fuel consumption per unit of payload of such aircraft would be at least twice lower with a longer range of over 50% when compared to existing supersonic aircraft of the same size. Simultaneously, the flight safety and ride quality during takeoff and landing at low speeds would be similar to the existing subsonic passenger aircraft. A low fuel consumption, long range, high ride quality, and high flight safety of these aircraft are widely opening a door for design of supersonic long range continental and intercontinental passenger aircraft that would be highly competitive with existing long range high subsonic passenger aircraft. | 09-09-2010 |
Zlatko Dizdarevic, Neuss DE
| Patent application number | Description | Published |
|---|---|---|
| 20100202823 | CLAMPING ARRANGEMENT AND EJECTOR AND CONICAL RING FOR THE SAME - A clamping arrangement for the force-fit connection of an outer component arrangement having a recess to an inner component arrangement, the clamping arrangement including an inner conical ring and an outer conical ring wherein one of the conical rings has bores for the leadthrough of clamping screws and the respective other conical ring has threaded bores for screwing in the clamping screws to brace the inner and outer conical rings against one another via the mutually facing first and second conical peripheral surfaces, and against the inner and outer component arrangement. At least one of the bores for the leadthrough of the clamping screw having an ejector thread for an ejector screw and the diameter of the ejector thread being greater than the diameter of the corresponding clamping screw. The clamping arrangement further including an ejector ring with an ejector bore for the leadthrough of the ejector screw which can be screwed into the ejector thread and the ejector ring having an ejector surface for engaging a clamping screw head of a clamping screw that is incompletely screwed into the corresponding threaded bore for the transmission of an ejector force onto the clamping screw head during the screwing in of the ejector screw. | 08-12-2010 |