Easy To Use Patents Search & Patent Lawyer Directory

At Patents you can conduct a Patent Search, File a Patent Application, find a Patent Attorney, or search available technology through our Patent Exchange. Patents are available using simple keyword or date criteria. If you are looking to hire a patent attorney, you've come to the right place. Protect your idea and hire a patent lawyer.

Searching:





Search by keyword, patent number, inventor, assignee, city or state:




Patent # Description
2016/0290189 INTERNAL COMBUSTION ENGINE AND COGENERATION SYSTEM
An internal combustion engine, which can improve an annual energy consumption efficiency, is provided. A gas engine 1 includes: an oil cooler 11 having a...
2016/0290188 OIL JET DEVICE
Oil jet device including a main body and having a fluid communication passage held in fluid communication with an oil passageway, a nozzle pipe having an oil...
2016/0290187 Sequential injection lubrication system for internal combustion engine operating on natural gas or alternative...
A sequential injection lubrication system for an internal combustion engine operating on natural gas or alternative fuels, the lubrication system having a...
2016/0290186 START OF AN INTERNAL COMBUSTION ENGINE WITH AT LEAST ONE ENGINE VALVE IN AN OPEN STATE DURING CRANKING
Start-up of an internal combustion engine comprises maintaining one or more engine valves in an engine cylinder in a continuously open state for more than one...
2016/0290185 ADJUSTABLE CAMSHAFT
An adjustable camshaft for an internal combustion engine may have a support shaft that extends along a rotational axis; a cam pack having a cam element that is...
2016/0290184 VARIABLE VALVE ACTUATOR
A valve actuation system is provided. A fluid actuator is configured to selectively prevent a valve from moving to a particular position. A source of fluid is...
2016/0290183 VARIABLE-STROKE VALVE TRAIN OF AN INTERNAL COMBUSTION ENGINE
The invention relates to a DOHC sliding cam valve train of an internal combustion engine with a four-cylinder in-line arrangement and cylinder shutoff. One of...
2016/0290182 CAM CAP
A cam cap is placed on a journal of a camshaft attached to a sprocket to constitute a bearing supporting the journal. The cam cap includes an accommodating...
2016/0290181 VALVE TIMING CONTROLLER
A valve timing controller includes a driving rotor, a driven rotor, a planetary rotor, a planetary carrier, and an elastic component to produce a restoring...
2016/0290180 VALVE OPENING/CLOSING TIMING CONTROL DEVICE
The valve opening/closing timing control device includes: the driving rotating body; the driven rotating body; an advancing chamber and a retarding chamber...
2016/0290179 LASH ADJUSTER
A lash adjuster includes a body which is cylindrical in shape and a plunger. The plunger is reciprocably inserted into the body and has an interior in which a...
2016/0290178 BALL PLUNGER FOR USE IN A HYDRAULIC LASH ADJUSTER AND METHOD OF MAKING SAME
A method of cold-forming a ball plunger blank includes providing a slug having a generally cylindrical surface extending between a first end and a second end,...
2016/0290177 LIFTER STRUCTURE
A lifter structure includes a cylindrical member configured to be reciprocally slid in a guide hole of a lifter guide according to rotation of a cam and having...
2016/0290176 Power Compounder
An apparatus and method is disclosed wherein mechanical power is returned to a prime mover producing waste heat. The apparatus includes a working fluid...
2016/0290175 COMPOSITIONS COMPRISING TETRAFLUOROPROPENE AND TETRAFLUOROETHANE; THEIR USE IN POWER CYCLES; AND POWER CYCLE...
A method for converting heat from a heat source to mechanical energy is provided. The method comprises heating a working fluid E-1,3,3,3-tetrafluoropropene and...
2016/0290174 HEAT PIPE AFTERCOOLING SYSTEM FOR A TURBOMACHINE
A turbomachine includes a compressor having an intake portion and an outlet portion. The compressor compresses air received at the intake portion to form a...
2016/0290173 ADJUSTING VALVE DRIVE MECHANISM AND STEAM TURBINE
An adjusting valve drive mechanism of a steam turbine drives an adjusting valve which opens and closes a steam channel, through which steam flows, by a valve...
2016/0290172 High-Pressure Side Separation of Liquid Lubricant for Lubricating Volumetrically Working Expansion Machines
The invention relates to a method for lubricating an expansion machine (30) in a thermodynamic cycle device, wherein the thermodynamic cycle device comprises...
2016/0290171 STEAM TURBINE PLANT
A steam turbine plant is provided with: a plurality of steam turbines; a multistage pressure condenser composed of a plurality of condensers which are...
2016/0290170 STEAM ACCUMULATOR COMPRISING A LATENT HEAT ACCUMULATOR AND A STEAM THERMOCOMPRESSOR
The present invention relates to a method for decoupling the provision of electricity and high-pressure steam of a combined heat and power plant which has the...
2016/0290169 TURBINE FRAME AND AIRFOIL FOR TURBINE FRAME
A turbine frame for a turbine engine having an axial centerline, the turbine frame comprising an inner hub, an outer hub encircling the inner hub, a plurality...
2016/0290168 TURBINE EXHAUST FRAME AND METHOD OF VANE ASSEMBLY
A turbine frame for a turbine engine having an axial centerline, includes an inner hub, an outer hub encircling the inner hub, a plurality of struts extending...
2016/0290167 TRI-TAB LOCK WASHER
A washer includes a hub and a first lobe connected to the hub. The first lobe includes a first hole. A second lobe is also connected to the hub and includes a...
2016/0290166 QUAD-TAB U-WASHER
A washer includes a first lobe comprising a first hole, a second lobe comprising a second hole, a third lobe comprising a third hole, and a fourth lobe...
2016/0290165 TRANSITION DUCT ASSEMBLY
A transition duct assembly has a plurality of transition ducts (2). Each transition duct has a tubular main body and has a flange portion provided at a...
2016/0290164 METHOD FOR ADDITIVE MANUFACTURING OF A GAS TURBINE CASING PART
A method for manufacturing a turbine casing part having a bearing chamber system including a shell (1) and at least one bearing receptacle (2) and further...
2016/0290163 TURBINE HOUSING
An object is to reduce loss of exhaust gas by improving a surface roughness to enhance efficiency of a turbocharger and to reduce generation of a crack due to...
2016/0290162 LUBRICATION DEVICE FOR A TURBINE ENGINE
The invention relates to a lubrication device for a turbine engine, comprising an oil intake pipe (23) provided with a pump (24) for supplying oil and control...
2016/0290161 DEVICE FOR CENTRING AND GUIDING THE ROTATION OF A TURBINE ENGINE SHAFT INCLUDING IMPROVED MEANS FOR RETAINING...
A device for centring and guiding the rotation of a turbine engine shaft, in which the outer race of a bearing is retained axially upstream and downstream by a...
2016/0290160 TURBOMACHINE WITH A COATING, USE OF A PLASTIC FOR COATING AND METHOD FOR COATING THE TURBOMACHINE
A turbomachine includes an inner housing which radially defines the flow channel of the turbomachine. A thermal barrier coating is arranged about the inner...
2016/0290159 LIQUID-COOLED TURBINE HOUSING WITH INTERMEDIATE CHAMBER
A turbocharger (10) with a liquid-cooled turbine housing (12) including an intermediate chamber (30) adjacent to the liquid chamber (20) of the turbine housing...
2016/0290158 AIRFOIL CONTOUR FOR LOW-LOSS ON-BOARDING OF COOLING AIR THROUGH AN ARTICULATING SPINDLE
A turbine stator vane assembly for a gas turbine engine is disclosed and includes an airfoil rotatable about an axis transverse to an engine longitudinal axis....
2016/0290157 SYSTEM FOR COOLING A TURBINE ENGINE
In one aspect the present subject matter is directed to a system for cooling a turbine engine. The system includes a cooling medium source, a stator vane...
2016/0290156 BALANCED TURBINE ENGINE PORTION AND TURBINE ENGINE
A balanced turbomachine part including one angular sector arranged to form a balancing ring centered about a ring axis. The angular sector includes a plurality...
2016/0290155 TEST BENCH FOR AN AIRCRAFT TURBOJET ENGINE, WITH SHUTTERS
A test bench for an aircraft turbojet engine is provided. The test bench comprises a U-shaped configuration with a passage in the form of an elongated...
2016/0290154 PROVIDING POWER TO A DATA CENTER
Techniques for providing power to a data center includes transferring heat from a computer data center to warm a fluid stored within an energy regeneration...
2016/0290153 TURBINE-TYPE FLOW RATE CONTROLLING DEVICE
A power generating portion formed of a rotor and a stator is provided. The rotor is formed of a ring incorporating a permanent magnet and an impeller. The...
2016/0290152 TURBINE-TYPE FLOW RATE CONTROLLING DEVICE
A power generating portion formed of a rotor and a stator is provided. The rotor is formed of a ring incorporating a permanent magnet and an impeller. The...
2016/0290151 Fusible Bond for Gas Turbine Engine Coating System
A seal comprises a housing. A coating has at least two layers with a bond layer to be positioned between a housing and a second hard layer. The second hard...
2016/0290150 SEALS FOR GAS TURBINE ENGINE
The present disclosure relates to a first seal for an aircraft blade outer air seal ("BOAS") comprising a first portion comprising a first channel and a second...
2016/0290149 SEGMENTED SEAL FOR GAS TURBINE ENGINE
One exemplary embodiment of this disclosure relates to a gas turbine engine. The engine includes a first rotor disk, a second rotor disk, and a...
2016/0290148 TURBINE NOZZLE BOX
A turbine nozzle box includes an annular outer ring plate, an annular nozzle unit, and an annular inner ring plate. The annular outer ring plate is operable to...
2016/0290147 HYBRID NOZZLE SEGMENT ASSEMBLIES FOR A GAS TURBINE ENGINE
A nozzle segment assembly for a gas turbine engine may generally include inner and outer ring support segments and a nozzle fairing positioned between the...
2016/0290146 MULTI-AIRFOIL GUIDE VANE UNIT
A multi-airfoil guide vane unit includes a first platform member, a second platform member, and at least two airfoil members, the airfoil members having a...
2016/0290145 TURBINE RING ASSEMBLY WITH SEALING
A turbine ring assembly includes a ring support structure and a plurality of ring sectors made of CMC material and forming a turbine ring, each ring sector...
2016/0290144 TURBINE RING ASSEMBLY WITH INTER-SECTOR CONNECTIONS
A turbine ring assembly includes a ring support structure and a plurality of CMC ring sectors forming a turbine ring. Each ring sector is K-shaped in radial...
2016/0290143 AXIAL FLUID MACHINE AND METHOD FOR POWER EXTRACTION
A method and a device for power extraction by means of an axial fluid machine, in an annulus tube comprising at least a rotatable inner wall (308, 408, 501)...
2016/0290142 BLADE FEATURE TO SUPPORT SEGMENTED COVERPLATE
A gas turbine engine component comprises a blade having a leading edge and a trailing edge. The blade is mounted to a disc and configured for rotation about an...
2016/0290141 RETAINING RINGS FOR TURBOMACHINE DISK AND COVERPLATE ASSEMBLIES
A retaining ring for a turbomachine disk and coverplate assembly includes a ring body defining a coverplate interface side and an opposed disk lip interface...
2016/0290140 COMPLIANT RAIL HANGER
A gas turbine engine assembly includes a supporting component and a supported component. The supporting component includes features engaged by the supported...
← Previous | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 | Next →

File A Patent Application

  • Protect your idea -- Don't let someone else file first. Learn more.

  • 3 Easy Steps -- Complete Form, application Review, and File. See our process.

  • Attorney Review -- Have your application reviewed by a Patent Attorney. See what's included.