Bizarre Patents
Microwave Oven With Removable Storage Cassette in Dashboard of Motor Vehicle
A microwave oven adapted for use within a motor vehicle dashboard area. The microwave oven has a removable storage cassette, and slidable platforms for securing and serving containers of beverages and foods.
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| Number | Title | Issue Date |
| 7304099 | Preparation of improved inks for inkjet printers The invention relates to an improved system for inkjet printing which results in images with increased permanence as measured by transfer of color from the image when the image is subjected to mechanical and/or chemical abrasion. The invention provides a fusible mat... | 12/04/2007 |
| 6502384 | Side thruster of flying object A side thruster of a flying object of the invention is provided with a solid gas generating agent, a nozzle arranged in a direction perpendicular to an axis of the flying object, a tube body for flowing the gas generated in accordance with a combustion of... | 01/07/2003 |
| 6412275 | Solid propellant gas generator impulse management scheme for high mass flow turn-down ratio A solid divert and attitude control system for use on a kill vehicle or missile that includes a solid propellant gas generator, a control valve for modulating the effective exit area of the solid propellant gas generator, and a controller for calculating ... | 07/02/2002 |
| 5671599 | Solid-propellant rocket engine with inner and outer burner surfaces Solid-propellant rocket engine with a combustion chamber, with a thrust nozzle, with one or more grains in the combustion chamber, at least one of which comprises two parts, namely, an inner burner part and an outer burner part, wherein the latter is conn... | 09/30/1997 |
| 5172547 | Electronic valve control for gas generator outflow A controlled fuel flow system from variable flow solid fuel gas generator to secondary combustor is provided, which system includes a hot gas valve which is operated by an electronic controller. The valve is mounted between the gas generator and the secon... | 12/22/1992 |
| 4777795 | Device for varying the thrust of a propulsion system using a solid propellant The device comprises, at the outlet of the combustion chamber 3, a movable assembly comprising a hollow closure member 26 constituting a needle 27, a thermal shield 22 and an annular piston 14. This closure member acts as a piston under the effect of the ... | 10/18/1988 |
| 4745740 | Velocity controller for ramjet missile and method therefor A velocity controller for a ramjet missile, having a supersonic inlet proximate the peripheral skin thereof for admitting air to a combustion zone of a ramjet engine, is comprised of a variable pitch cover disposed in pivotable engagement within the inlet... | 05/24/1988 |
| 4744300 | Utilization of metal hydride and acidic reagent for the accelerating of masses and propulsion devices for applying such materials The utilization of metal hydride and an acidic reagent for the accelerating of masses, and propulsion devices for applying such materials. The materials are of a saline complex metal hydride and acidic reagent which is sprayed onto the metal hydride which... | 05/17/1988 |
| 4630437 | Optical control method for solid fuel rocket burn rate A solid fuel rocket burn rate control method wherein grain preheating energy is supplied to the grain region just ahead of the regressing burn face by optical conductors such as fiber optic filaments that are buried in the grain and dispersed across the g... | 12/23/1986 |
| 4587805 | Electro-optical control of solid fuel rocket burn rate A solid fuel rocket burn rate control apparatus wherein grain preheating energy is supplied to the grain region just ahead of the regressing burn face by optical conductors such as fiber optic filaments that are buried in the grain and dispersed across th... | 05/13/1986 |
| 4387865 | Method for steering a solid propellant ballistic vehicle A method for steering solid propellant ballistic vehicles during powered flight which eliminates the requirement for cutoff control by allowing simultaneous fuel depletion and velocity-to-be-gained, VG, nulling. The vehicle booster is steered a... | 06/14/1983 |
| 4345427 | Rocket motor or gas generator having controlled thrust or mass flow output A solid propellant rocket motor of gas generator of the type having retractable filaments embedded in the propellant for the purpose of controlling the overall thrust or mass flow output is combined with a channeled separator located between the propellan... | 08/24/1982 |
| 3999379 | Reduction of depressurization thrust termination jolt Thrust termination of a solid propellant rocket motor is obtained by connecting the nozzle to the combustion chamber pressure vessel by means of explosive and extrusable bolts. When it is desired to obtain thrust termination, the explosive bolts are blown... | 12/28/1976 |
