...that the Eveready Battery began as an invention called the "electric flowerpot," which was a tube with a battery and light bulb inside? The idea was to fasten this gizmo to the side of a flowerpot so it would illuminate the flowers from the bottom. The idea died on the vine and the businessman who licensed the flower pot, Conrad Huber, was left with a pile of useless tubes -- until he found a way to market them as batteries to light the world!
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| Number | Title | Issue Date |
| 8113005 | Jet engine with detachably arranged generator unit The present technology generally relates to jet engines, in particular for an aircraft, having at least one turbine shaft on which at least one compressor and a turbine are arranged, and a housing extends over the lateral surfaces of the jet engine, wherein furtherm... | 02/14/2012 |
| 8006501 | Device for driving the rotor of turbine engine auxiliary A device for driving the rotor of an auxiliary is mounted on a turbine engine auxiliaries support which includes a pinion for driving the rotor shaft. The device includes a tubular shaft driven by the pinion and supported by a first bearing (18) and a second ... | 08/30/2011 |
| 7966833 | Turbine engine with a power turbine equipped with an electric power generator centered on the axis of the turbine engine A turbine engine for an aircraft is disclosed. The engine includes a gas generator and a receiver driven by a power turbine. The receiver includes a propeller driven by a free power turbine provided with an outer case. The propeller includes a propeller case located... | 06/28/2011 |
| 7721555 | Gas turbine with free-running generator driven by by-pass gas flow A gas turbine, especially an aircraft engine is provided. The gas turbine comprises at least one compressor (15, 16), at least one combustion chamber (17), at least one turbine (18, 19), and at least one generator (20) for generating elec... | 05/25/2010 |
| 7603864 | Blade tip electric machine An electromagnetic machine that generates electric power from an engine by having rotor poles on the tips of the fan blade airfoils and stator elements circumferentially placed around the blade airfoils. As the pole tips on the blade airfoils are excited, they rotat... | 10/20/2009 |
| 7500365 | Accessory gearbox Provided is an accessory gearbox for a gas turbine engine that contributes minimally to engine weight and complexity. An accessory gearbox comprises a stationary frame that is circumferentially disposed about a central longitudinal axis of the engine. The frame incl... | 03/10/2009 |
| 7434406 | Drive for using a direct driven generator to start a counter-rotating multi-spool gas turbine engine A drivetrain for a multi-spool counter rotating gas turbine engine may include a lay shaft for connecting a power turbine shaft of the engine with a gas generator shaft of the engine when the drivetrain is in engine start mode. In normal operation mode, an actuator ... | 10/14/2008 |
| 7386983 | Apparatus for driving an accessory gearbox in a gas turbine engine A mechanical drive system for an accessory gearbox of a gas turbine engine is provided. The engine has a high-pressure drive shaft and a low-pressure drive shaft. The mechanical drive system includes a first tower shaft, a second tower shaft, a first lay shaft, and ... | 06/17/2008 |
| 7373771 | Cooling arrangement for an accessory gearbox and method of cooling The accessory gearbox (AGB) has at least one coolant passage between the AGB and the accessory for externally cooling the accessory without coolant flow inside the accessory. ... | 05/20/2008 |
| 7368827 | Electrical assembly for monitoring conditions in a combustion turbine operating environment An electrical assembly for use in various operating environments such as a casing of a combustion turbine 10 is provided. The assembly may include an electrical energy-harvesting device 51 disposed in a component within the casing of the turbine to con... | 05/06/2008 |
| 7246482 | Gas turbine engine bleed air power assist system and method A bleed air power assist system is coupled to a gas turbine engine that includes a high pressure turbine, a low pressure turbine, and an electrical generator driven by the high pressure turbine. The bleed air power assist system selectively bleeds air discharged fro... | 07/24/2007 |
| 7131275 | Gas turbine engine system having an electric starter motor with integral clutch A gas turbine engine system includes an electric starter motor which utilizes a partially hollow or cupped shaped rotor. Space is provided inside the rotor to fit the required clutch, bearings, and drive shaft. A rotor shaft drives the input shaft through the clutch... | 11/07/2006 |
| 7114322 | Gas-turbine power generating installation and method of operating the same A gas-turbine power generating installation capable of effectively utilizing gases produced in overage gas fields, etc. and a method of operating the installation are provided. The gas-turbine power generating installation is installed in the vicinity of an outrage ... | 10/03/2006 |
| 7109595 | Small multi-functional butane gas-powered portable electric generator The object of the present invention is a multi-functional electric generator comprising, an engine, a generator, a voltage-stabilizer control circuit, a gas storage gauge and a lighter. A manual electrical rod can be assembled to a side of the engine allowing the ge... | 09/19/2006 |
| 7093447 | Auxiliary power unit with an oil-free compressor An auxiliary power unit for aircraft with a load compressor that delivers cabin air free of oil contamination by supporting a drive shaft for the load compressor with oil-free bearings and coupling the load compressor to a gearbox and power head for the auxiliary po... | 08/22/2006 |
| 7086219 | Cowl structure for a gas turbine engine A cowl structure (18) for a gas turbine engine (10) comprises an outer skin (26) defining a first path for a load applied to the engine (10). The cowl structure (18) includes an inner skin (24) defining a second path for the... | 08/08/2006 |
| 7055330 | Apparatus for driving an accessory gearbox in a gas turbine engine A mechanical drive system for an accessory gearbox of a gas turbine engine is provided. The gas turbine engine includes a high-pressure drive shaft and a low-pressure drive shaft. The mechanical drive system includes a tower shaft and a lay shaft. The tower shaft is... | 06/06/2006 |
| 7055303 | Gas turbine engine architecture A gas turbine engine having an oil cavity architecture and bearing placement which reduce heat rejection and oil system complexity by enclosing the reduction gearbox bearings and at least the shaft bearings supporting the high pressure shaft in the same oil cavity. | 06/06/2006 |
| 7040082 | Assistance and emergency drive for electrically-driven accessories The invention relates to a system for driving an accessory, such as a fuel pump or an oil pump in a turboengine, said system comprising an electric motor and further comprising an air turbine associated with said electric motor. Said air turbine is suitable for bein... | 05/09/2006 |
| 7028461 | Uniaxial gas turbine system A uniaxial gas turbine system, comprising a uniaxial gas turbine, a rotary machine driven by the uniaxial gas turbine, a continuously variable transmission for transmitting a driving force from the uniaxial gas turbine to the rotary machine, and a control device for... | 04/18/2006 |
| 7013651 | Compact quick attach starter-generator installation A mounting system for mounting an air-cooled device to a mount, the device having a mounting flange and a cooling air outlet radially inward of an outer periphery of the device, the mounting flange adapted to cooperate with the mount, where the mounting system has a... | 03/21/2006 |
| 6966188 | Plate-like body connecting method, connected body, tail pipe for gas turbine combustor, and gas turbine combustor The present invention provides a plate-like body connecting method in which functions such that cooling capability is not reduced. There is provided a plate-like body connecting method for connecting at least two plate-like bodies each having passages that extend al... | 11/22/2005 |
| 6962057 | Gas turbine power generation system In a gas turbine power generation system having a gas turbine engine and a generator connected to the engine, maintenance ease is enhanced by forming the housing to have openable maintenance faces at two of its faces. Installation space is reduced and a compact conf... | 11/08/2005 |
| 6903466 | Wind-power generator pod constituted by the body of an electricity generator The pod of wind-powered generator is constituted by a rigid fairing in which at least one electricity generator for coupling to at least one wind-driven propeller is disposed. The rigid fairing of the pod is formed by the body of the generator in which there are mou... | 06/07/2005 |
| 6851267 | Compact quick attach starter-generator installation A mounting system, for installing a starter-generator to an accessory housing, where the starter-generator has a mounting end with a connecting flange and a cooling air outlet radially inward of a peripheral starter-generator housing edge, and where the accessory ho... | 02/08/2005 |
| 6832486 | Electrical machine An electrical machine, such as a generator or motor, is incorporated in a gas turbine engine. The engine has compressor blades which are shrouded at. Beyond the shroud, an electrical machine is provided by rotor projections which run in a channel in flux cores, with... | 12/21/2004 |
| 6729140 | Electrical machine An electrical machine, such as a generator or motor, is incorporated in a gas turbine engine. The engine has compressor blades which are shrouded at. Beyond the shroud, an electrical machine is provided by rotor projections which run in a channel in flux cores, with... | 05/04/2004 |
| 5687561 | Ducted fan gas turbine engine accessory drive A ducted fan gas turbine engine includes a fan which is driven by a low pressure turbine via a load transmitting shaft. The load transmitting shaft additionally drives the accessories of the engine and the aircraft upon which it is mounted. In the event o... | 11/18/1997 |
| 5586429 | Brayton cycle industrial air compressor A Brayton cycle air compressor system having two turbinecompressors and a recuperated combustion chamber interconnected. A portion of the hot compressed high pressure air is used as combustion air for the combustion chamber. In addition, a portion of the ... | 12/24/1996 |
| 5435124 | Mounting bracket for an aircraft engine accessory A bracket for mounting an accessory on an aircraft engine is disclosed. The bracket includes a mounting wedge (70) adapted to be secured to the engine, a carrier (120) which is supported by the mounting wedge and in turn supports an end of the accessory, ... | 07/25/1995 |
| 5428952 | Geodesic engine mount structure The lack of torsional rigidity in the mounting of a turbine engine (10) to a transmission (12) in a power unit (14), (16) is avoided utilizing a mounting structure including a relatively small ring-like base (58), (60) connected to the transmission (12) a... | 07/04/1995 |
| 5410870 | Aircraft engine layout Aircraft engine, whose ancillary equipment forms a unitary assembly wherein the equipment is located to the rear of the air intake duct in a substantially closed central compartment just upstream of the gas generator. The equipment positioned along the en... | 05/02/1995 |
| 5284012 | Nacelle cooling and ventilation system A nacelle cooling and ventilation system for an aircraft gas turbine engine which includes a chin scoop and duct assembly for directing air through the engine bay where it is exhausted into the engine exhaust through an exhaust shroud eductor. The nacelle... | 02/08/1994 |
| 5193976 | Injection device for the ON-LINE wet cleaning of compressors In an injection device for the ON-LINE wet cleaning of compressor, the liquid cleaning agent is injected via a nozzle into the flow passage upstream of the compressor. The nozzle is a molecular atomizer which is mounted in the casing wall of the compresso... | 03/16/1993 |
| 5129223 | Radiant energy power source structure A radiant energy power source structure for providing electrical power to a jet aircraft is disclosed. The device comprises a plurality of inward facing longitudinal ribs arranged in an annular configuration positioned radially outward of the plurality of... | 07/14/1992 |
| 5039281 | Method and apparatus for supplying compressed air to auxiliary systems of a vehicle An apparatus for supplying compressed air to the auxiliary system of a vehicle such as an aircraft, or other device powered by a gas turbine engine, comprises an auxiliary compressor which is connected by a differential to the main drive shaft of the comp... | 08/13/1991 |
| 4864812 | Combined auxiliary and emergency power unit Weight and spatial concerns in aircraft are alleviated or minimized through a combined auxiliary and emergency power unit including a gear box 10 adapted to drive a generator 16 and a hydraulic pump 18 as auxiliary to emergency power supplies for the airc... | 09/12/1989 |
| 4729218 | Gas turbine engine with generator arrangement A gas turbine engine with an electrically driven fuel pump unit wherein the rotor of the gas turbine engine operates an electric generator. The generator supplies two separate circuits. One circuit serves in the customary way to supply electricity for the... | 03/08/1988 |
| 4706908 | Lightweight auxiliary power and forced air supply unit A lightweight auxiliary power and forced air supply unit that may be used to provide electricity and forced air for use by an air conditioning system on a vehicle such as an aircraft. The unit includes a turbine (12), a generator (13), a forced air unit (... | 11/17/1987 |
| 4380897 | Gas turbine containing an additional combustion gas compressor A gas turbine containing an additional combustion gas compressor and a gearing drive which, on the one hand, is rotatably connected by means of a rigid coupling and an axial bearing with the gas turbine and, on the other hand, is rotatably connected by me... | 04/26/1983 |