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
2016/0298498 Energy Storage and Retrieval Systems
Systems and methods for storing and retrieving thermo-mechanical energy are disclosed. The systems and methods include a thermodynamic cycle (e.g., a...
2016/0298497 HEAT ENERGY RECOVERY SYSTEM
Disclosed is a heat energy recovery system including: a heat energy recovery circuit that causes a working medium to circulate by means of a circulation pump...
2016/0298496 THERMIC MACHINE WITH THERMODYNAMIC CYCLE AND THE OPERATION THEREOF
Thermodynamic cycle thermic machine and the operation thereof. Consisting of a tank (1) of compressed subcooled liquid at room temperature, which is filled either...
2016/0298495 Adiabatic Salt Electric Energy Storage
Efficient energy storage is provided by using a working fluid flowing in a closed cycle including a ganged compressor and turbine, and capable of efficient...
2016/0298494 METHOD FOR MACHINING A CASING FOR A TURBO ENGINE, A CASING FOR TURBO ENGINE AND A TURBO ENGINE WITH A CASING
A method for machining a casing for a turbo engine is provided, wherein a) at least one blank part for the casing is positioned in a tooling fixture, b) the at...
2016/0298493 CUTOUTS IN GAS TURBINE STRUCTURES FOR DEFLECTION CONTROL
A mid-turbine frame is provided. The mid-turbine frame may comprise an inner case having an annular surface with an interface section disposed on the annular...
2016/0298492 TURBINE CASE COUPLING
Aspects of the disclosure are directed to a first case including a first plurality of threads, a second ease including a second plurality of threads, an...
2016/0298491 TURBOCHARGER BEARING ASSEMBLY
An assembly can include a turbocharger center housing that includes a through bore that extends between a compressor end and a turbine end of the turbocharger...
2016/0298490 TURBOCHARGER SPRING ASSEMBLY
A turbocharger bearing assembly can include a spacer that includes an axial through bore, a compressor side surface and a turbine side surface; a compressor...
2016/0298489 ANNULAR ELEMENT OF A TURBOMACHINE CASING
The invention relates to the field of turbomachines, and more specifically to an annular element (13) for a turbomachine casing, which has at least one inside...
2016/0298488 METHOD AND DEVICE FOR CLEANING A JET ENGINE
A method for cleaning a jet engine includes introducing into the engine, via a carrier gas by way of at least one nozzle, a cleaning medium which contains...
2016/0298487 PROTECTION SYSTEM AND TURBO ENGINE WITH A PROTECTION SYSTEM
A protection system for a turbo engine, in particular an aircraft engine is provided. The turbo engine comprises at least one fluid duct element with a casing...
2016/0298486 TURBINE ENGINE AND CONTROL METHOD
A turbine engine includes a compressor, a combustion chamber, first and second turbines downstream from the combustion chamber, a first rotary shaft...
2016/0298485 SPEED SENSOR FOR A GAS TURBINE ENGINE
A gas turbine engine includes a speed change mechanism. A fan drive shaft has a radially extending surface that is attached to the speed change mechanism. A...
2016/0298484 A METHOD FOR PROVIDING COOLANT TO A MOVABLE AIRFOIL
A gas turbine engine with an adjustable vane includes a platform with a hole and an aperture. A vane is supported for rotation relative to the platform by a...
2016/0298483 ACTIVE CLEARANCE CONTROL FOR AXIAL ROTOR SYSTEMS
A system includes a stator assembly including at least one stator airfoil. The system also includes a rotor assembly including at least one rotor airfoil...
2016/0298482 BRUSH SEAL
A seal includes a housing having a back plate and a front plate. A supporting bristle layer is disposed adjacent to the back plate, and bristles in the...
2016/0298481 ROTATING LABYRINTH M-SEAL
Aspects of the disclosure are directed to a seal associated with an engine of an aircraft. The seal includes a plurality of lands, and a barrel coupled to the...
2016/0298480 AIRFOIL DEVICE FOR A GAS TURBINE AND CORRESPONDING ARRANGEMENT
An airfoil device for a gas turbine has a root section mountable to an airfoil disc and an airfoil element. The root section has a platform at which the...
2016/0298479 FAN BLADE PLATFORM SEAL WITH LEADING EDGE WINGLET
A fan section for a gas turbine engine is provided. The fan section includes a fan hub including a slot and a fan blade including an airfoil extending from a...
2016/0298478 GAS TURBINE BUCKET SHANKS WITH SEAL PINS
The present application and the resultant patent provide improved gas turbine component sealing. In one example embodiment, a shank assembly may include a...
2016/0298477 SHROUD ARRANGEMENT OF A ROW OF BLADES OF STATOR VANES OR ROTOR BLADES
A cover band assembly of a blade row of stator or rotor blades is provided. The cover band assembly comprises a blade row that is arranged inside a main flow...
2016/0298476 WRAPPED DOG BONE SEAL
A seal for a gas turbine engine comprises a seal body extending from a first end to a second end. A wrap extends at least partially around the first and second...
2016/0298475 STATIC AXIAL BRUSH SEAL WITH DUAL BRISTLE PACKS
A brush seal is provided. The brush seal may comprise an annular backing plate and a first bristle pack coupled to the annular backing plate. The first bristle...
2016/0298474 SLIDING SEAL
The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section, a second seal section, and...
2016/0298473 SEAL CONFIGURATIONS FOR TURBINE ASSEMBLY AND BEARING COMPARTMENT INTERFACES
The present disclosure relates to gas turbine engine and seal configurations, and components for a gas turbine engine. In one embodiment, a seal for a gas...
2016/0298472 SHIM TO MAINTAIN GAP DURING ENGINE ASSEMBLY
Aspects of the disclosure are directed to a tube of an engine of an aircraft configured to transfer a fluid, a boss of the engine, and a shim coupled to at...
2016/0298471 ASYMMETRIC TWIN SCROLL VOLUTE
An asymmetric twin scroll turbine 10 combined with an integrated exhaust manifold cylinder head 20 may be designed to accommodate mixed, radial or axial flow...
2016/0298470 AIRFOILS
An airfoil cluster includes an inner diameter platform and an outer diameter platform. A plurality of airfoils extend radially from the inner diameter platform...
2016/0298469 AIRCRAFT BLADE LOCK RETAINER
The present disclosure provides devices related to aircraft engine fan assemblies and blade lock retainers. In various embodiments, a blade lock retainer is...
2016/0298468 BLADED ROTOR
A bladed rotor comprising a rotor disk (12) presenting two front faces (14, 15) and an outer peripheral face (16), sockets (18) being provided in the outer...
2016/0298467 ARTICLE HAVING VARIABLE COATING
A coated article includes a substrate and a continuous ceramic-based coating supported on the substrate. The ceramic-based coating varies in at least one of...
2016/0298466 GAS TURBINE ENGINE DAMPING DEVICE
An exemplary gas turbine engine assembly includes a damping device having a first side and a second side facing away from the first side. The first side is...
2016/0298465 GAS TURBINE ENGINE COMPONENT COOLING PASSAGE WITH ASYMMETRICAL PEDESTALS
A gas turbine engine component includes spaced apart walls that provide a cooling passage that extends in a first direction. A pedestal is arranged in the...
2016/0298464 COOLING HOLE PATTERNED AIRFOIL
An airfoil having a cooling hole pattern is disclosed. The cooling hole pattern may be an offset herringbone pattern. For instance, the airfoil may have rows...
2016/0298463 ENHANCED COOLING FOR BLADE TIP
In a featured embodiment, a gas turbine engine component comprises an airfoil having a leading edge, a trailing edge, and pressure and suction side walls...
2016/0298462 COOLING PASSAGES FOR A GAS TURBINE ENGINE COMPONENT
A gas turbine engine component includes a wall which includes a first surface and a second surface opposing the first surface. A plurality of cooling passages...
2016/0298461 ARTICLE OF MANUFACTURE FOR TURBOMACHINE
An article of manufacture includes a rotor blade configured for use with a turbomachine. The blade is configured for attachment to a rotor wheel. The blade is...
2016/0298460 ROTOR DAMPER
A rotor stage (100) of a gas turbine engine (10) comprises a platform (120) from which rotor blades extend. The platform is provided with a circumferentially...
2016/0298459 ROTOR DAMPER
A rotor stage of a gas turbine engine includes a platform from which rotor blades extend. The platform is provided with a circumferentially extending damper...
2016/0298458 ROTOR DAMPER
A rotor stage (100) of a gas turbine engine (10) comprises a platform (120) from which rotor blades extend. The platform is provided with a circumferentially...
2016/0298457 ROTOR DAMPER
A rotor stage (100) of a gas turbine engine (10) comprises a platform (120) from which rotor blades extend. The platform is provided with a circumferentially...
2016/0298456 METHOD FOR JOINING AT LEAST TWO ROTOR ELEMENTS OF A TURBOMACHINE
The invention relates to a method for joining at least two rotor elements of at least one rotor of a turbomachine. The detecting of a radial runout of at least...
2016/0298455 Adiabatic salt energy storage
Efficient energy storage is provided by using a working fluid flowing in a closed cycle including a ganged compressor and turbine, and capable of efficient...
2016/0298454 CUTTING BIT AND EXTRACTION TOOL FOR SAME
A cutting bit for a bit assembly secured to a cutter head includes a cutting end, a shank extending along a bit axis, and a shoulder positioned between the...
2016/0298453 BIT ASSEMBLY FOR CUTTER HEAD
A bit assembly for a cutting drum includes a sleeve and a bit. The sleeve includes shank portion, a flange positioned, and a bore extending through the flange...
2016/0298452 SYSTEM AND METHOD OF DETECTING DULL AND WORN CUTTER BITS
A mining machine including a chassis, an actuator, a cutter drum supported by the chassis, the cutter drum driven by the actuator, a cutter bit coupled to the...
2016/0298451 ANNULAR TOOL
The invention relates to an annular tool (1) having at least one working region (4) oriented radially outward and having high wear resistance, and a clamping...
2016/0298450 PASSIVE SAMPLING DEVICE AND METHOD OF SAMPLING AND ANALYSIS
The invention provides a device and method to quantitatively measure concentrations of volatile organic compound vapors below the ground surface using a...
2016/0298449 DOWNHOLE INSTRUMENT FOR DEEP FORMATION IMAGING DEPLOYED WITHIN A DRILL STRING
Methods and systems for acquiring data in a wellbore. The method includes deploying an instrument connected to an instrument line into a drill string, through...
← 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 | 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.