Bizarre Patents
Wearable Device For Feeding and Observing Birds and Other Flying Animals
A device for feeding and observing flying animals comprising a hat, a support mounted on the hat and extending outward from the hat, and a feeder mounted on the support.
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| Number | Title | Issue Date |
| 8172178 | Device for generating aerodynamic disturbances so as to protect the outer surface of an aircraft against elevated temperatures An aircraft with an outer surface from which flows an aerodynamic stream of cold air and includes at least one hot gas outlet, characterized in that it includes at least one device (16) for generating aerodynamic disturbances so as to mix hot gas and cold air... | 05/08/2012 |
| 7686248 | System and method for internal passive cooling of composite structures According to one embodiment of the invention, an apparatus comprises a passive cooling system and a portion of an air vehicle which receives thermal energy. The passive cooling system is disposed adjacent the portion of the air vehicle and comprises a fluid transfer... | 03/30/2010 |
| 7401682 | Architecture for an acoustic liner An acoustic liner 20 includes a remote panel 26, a perforated proximate panel 22 transversely spaced from the remote panel and one or more partitions 32 spanning across the space between the panels. At least one baffle 44 cooperate... | 07/22/2008 |
| 7357351 | Linear shock wave absorber A linear cavity is provided on the leading edge of an object that is subject to the flow of liquids or gasses, where said cavity preferably has a wall that follows the curvature of a diminishing sine wave, although other configurations are possible that do not follo... | 04/15/2008 |
| 7334939 | Method and device for verifying a temperature value at a destination altitude of an aircraft The device comprises a means for measuring a dynamic temperature on the outside of the aircraft, a means for determining a static temperature around the aircraft, using said dynamic temperature, a means for determining, using said static temperature and a thermodyna... | 02/26/2008 |
| 7325772 | Aircraft heat sink and electronics enclosure An aircraft component including a first section adapted to be attached at an exterior surface of an aircraft to close an access opening through the exterior surface; and a second section extending outward from the first section and forming heat transfer surfaces to ... | 02/05/2008 |
| 7313963 | Isothermal de-iced sensor Temperature and pressure sensors are protected from ice buildup by a in heat exchange relationship with a probe surrounding the sensors. ... | 01/01/2008 |
| 7311287 | Methods for incorporating area ruled surfaces in a supersonic aircraft A vertical stabilizer is configured to minimize the rate of change of cross-sectional area distribution of the vehicle or device to which the vertical stabilizer is mounted. One or more “waisted” areas can be included at the tip and/or the root of the vertical s... | 12/25/2007 |
| 7311175 | Acoustic liner with bypass cooling An acoustic liner 20 includes a remote panel 26, a proximate panel 28 transversely spaced from the remote panel and a resonator chamber 34b residing between the panels. Perforations 38 penetrate the proximate panel in regist... | 12/25/2007 |
| 7283096 | Microstrip patch antenna for high temperature environments A patch antenna for operation within a high temperature environment. The patent antenna typically includes an antenna radiating element, a housing and a microwave transmission medium, such as a high temperature microwave cable. The antenna radiating element typicall... | 10/16/2007 |
| 7275720 | Actively cooled ceramic thermal protection system An apparatus and method for thermal protection is provided. A thermal protection apparatus includes a porous layer attached to an inner structural member requiring thermal protection. The porous layer serves as both a cooling air plenum and a transpiring medium. The... | 10/02/2007 |
| 7267303 | Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy A system for reducing plasma induced communication disruption is disclosed. The system utilizes an electrophilic gas injectant, bent reentry vehicle nose shaping and a number of flaps configured to provide 3-axis steering capability. Injecting electrophilic gas inje... | 09/11/2007 |
| 7247002 | Lamellate CMC structure with interlock to metallic support structure A component (10) for a gas turbine engine formed of a stacked plurality of ceramic matrix composite (CMC) lamellae (12) supported by a metal support structure (20). Individual lamellae are supported directly by the support structure via cooperat... | 07/24/2007 |
| 7237752 | System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping The present invention discloses a system and a method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping. Injecting electrophilic gas into plasma accomplishes reduction of plasma induced comm... | 07/03/2007 |
| 7232093 | Cooled insulation surface temperature control system An apparatus and method for surface temperature control is provided. Surface temperature control is achieved by flowing coolant in and then out of a low strength porous layer attached to a structural plenum. A semi-permeable layer may be attached to the outer surfac... | 06/19/2007 |
| 7222819 | Aircraft ram air inlet with multi-member closure flap A ram air inlet includes a channel with an intake in a wing leading edge, front and rear flaps arranged in the channel for selectively closing or opening the channel, and an actuator connected to the flaps. A front end of the front flap is pivotably connected by a f... | 05/29/2007 |
| 7219855 | Rising and moving apparatus and manufacturing method thereof A fluid-structure interactive analysis is performed while n types of wing structure models are caused to flap in accordance with a prescribed model of flapping manner. Based on an analysis, data 1, data 2, . . . data n of physical values related to flu... | 05/22/2007 |
| 7186951 | Sensor structure and sensor arrangement for measuring flow data on a flow body Sensor structure of a flow body protruding into a current for carrying out measurements of flow states, containing a structural part (1) with at least two measuring orifices (5), to which transfer lines (7) are coupled, which guide the flow medi... | 03/06/2007 |
| 7121512 | Drain particularly for engine support strut A drain, for example for an aircraft engine support strut, arranged on the trailing edge of the rear secondary structure of the strut. The drain includes a conduit with a substantially horizontal axis and a substantially rectangular cross-section, taken in a plane p... | 10/17/2006 |
| 7083147 | Modularized insulation, systems, apparatus, and methods Modularized insulation blanket for thermal and/or acoustical insulation. The modularized insulation blanket has a cover formed of a distal layer and proximal layer in sealed mated relationship. The distal and proximal layers are sealed along longitudinal and latitud... | 08/01/2006 |
| 7082878 | Missile with multiple nosecones A missile includes a payload assembly that has a pair of nosecones. The nosecones may be optimized for different environments and/or phases of flight, for example, having different shapes, different shell materials, different types of seals, and/or different separat... | 08/01/2006 |
| 7055781 | Cooled insulation surface temperature control system An apparatus and method for surface temperature control is provided. Surface temperature control is achieved by flowing coolant in and then out of a low strength porous layer attached to a structural plenum. A semi-permeable layer may be attached to the outer surfac... | 06/06/2006 |
| 7004428 | Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings An aircraft includes a fuselage, thin supersonic wings on the fuselage, there being trailing edge flaps carried by the wings, the flaps configured to provide flap deflection to simultaneously control wing twist and to reduce drag, when the aircraft is operated at su... | 02/28/2006 |
| 7000870 | Laminar flow wing for transonic cruise In combination, an aircraft wing and fuselage, comprising the wing having camber at or near the wing leading edge which has blunted sharpness and low sweep angle, and the fuselage having indentation along the wing side thereof, and lengthwise of the fuselage. ... | 02/21/2006 |
| 6948331 | Environmental control system for an aircraft An environmental control system for an aircraft includes a vapor cycle system for circulating a refrigerant through a fuel cooled condenser, a primary evaporator wherein the expanded refrigerant is used to provide cooling for a cooling medium and a secondary evapora... | 09/27/2005 |
| 6942183 | Air cycle air conditioning with adaptive ram heat exchanger An air conditioning pack for an aircraft provides primary and secondary heat exchangers arranged in a ram air duct. A third heat exchanger is arranged in the ram air duct and is fluidily connected to the primary and secondary heat exchangers. The overall or combined... | 09/13/2005 |
| 6939392 | System and method for thermal management A system for the management of thermal transfer in a gas turbine engine includes a heat generating sub-system in operable communication with the engine, a fuel source to supply a fuel, a fuel stabilization unit to receive the fuel from the fuel source and to provide... | 09/06/2005 |
| 6931834 | Cooling systems Apparatus for maintaining the temperature of a component of a gas turbine engine below a predetermined maximum working temperature comprises a reservoir for a cooling fluid having a boiling point below the working temperature and in which the component is immersed o... | 08/23/2005 |
| 6929866 | Composite foam structures A composite rigid foam structure that has a skin or coating on at least one of its surfaces. The skin is formed in situ by thermal spray techniques. The skin is bonded substantially throughout the surface of the porous substrate to the peripheries of the pores. The ... | 08/16/2005 |
| 6907920 | Heat exchanger panel The present invention relates to a heat exchanger panel which has broad utility in high temperature environments. The heat exchanger panel has a first panel, a second panel, and at least one fluid containment device positioned intermediate the first and second panel... | 06/21/2005 |
| 6857602 | Environmental control system and method of using the same The present invention is generally directed to an environmental control system (and method of using the same) that is capable of conveying conditioned gases toward at least one target component (e.g., an electrical or propulsion component) of a flight vehicle such a... | 02/22/2005 |
| 6612523 | Aircraft structures having improved through-thickness thermal conductivity An apparatus is provided for transferring heat through the thickness of aircraft structure formed from composite laminates. Z-pins having a high thermal conductivity are inserted through the composite laminate and placed in thermal communications with a h... | 09/02/2003 |
| 6578491 | Externally accessible thermal ground plane for tactical missiles A tactical missile includes a heat pipe connecting heat sources with heat sinks within the missile. The system includes a removable external heat dissipation device that connects to the heat pipe while the missile is being tested or reprogrammed. The exte... | 06/17/2003 |
| 6435454 | Heat pipe cooling of aircraft skins for infrared radiation matching A system and an apparatus for matching infrared radiation emitted from aircraft skins to background infrared radiation in order to minimize the contrast between the two radiations, and to thereby camouflage the aircraft from electro-optical detection syst... | 08/20/2002 |
| 6241184 | Vehicle having a ceramic radome joined thereto by an actively brazed compliant metallic transition element A missile has a body with a substantially circular nose opening therein, and a ceramic radome sized to cover the nose opening. A compliant metallic circular transition element is disposed structurally between the radome and the body. The transition elemen... | 06/05/2001 |
| 6178865 | Thermally massive radar decoy A light weight decoy for deceiving radar and forward looking infrared tracking systems. The decoy provides the same radar cross-section as that of an intercontinental ballistic missile (ICBM) and is thermally massive across the entire black body spectrum.... | 01/30/2001 |
| 6027072 | Payload chamber cooling system A cooling system (18) for supplying an even distribution of cooling air within a payload chamber (14) of a launch vehicle is disclosed. The cooling system (18) includes an elongate duct (20), a diverter (22), and a plurality of partitions (24a, 24b, 24c .... | 02/22/2000 |
| 5979831 | System and method for attaching a structural component to an aerospace vehicle A system and method for attaching an annular structural component to an aerospace vehicle is provided. The system includes a plurality of fittings circumferentially affixed to an engagement portion of the vehicle, and a plurality of supports. Each support... | 11/09/1999 |
| 5897076 | High-efficiency, supersonic aircraft A supersonic flight aircraft having a longitudinally forwardly extending fuselage having an axis in the direction of flight, and a wing, and which comprises the wing extending generally laterally relative to the axis, and having a leading edge angled forw... | 04/27/1999 |
| 5882765 | Element made of a reinforced low density heat protective material and method to obtain said element An element made of a reinforced low density heat protective material including an elastomer and/or a silicon resin matrix loaded with organic and/or inorganic components, wherein the reinforcement is formed of glass or ceramic thread sections or the like ... | 03/16/1999 |
