Patents full text · MLC-0201
CPC subclass F05D
Indexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants
| No. | Publication | Title | Published | Assignee |
|---|---|---|---|---|
| 1 | US12416800B2 | Insertion tool | 2025-09-16 | GEN ELECTRIC |
| 2 | US12352180B2 | Compressor rotor destacking apparatus and method | 2025-07-08 | RTX CORP |
| 3 | US11815425B2 | Jig for vibration test of rotor blade | 2023-11-14 | IHI CORP |
| 4 | US11486271B1 | Adjustable mount for engine accessory | 2022-11-01 | PRATT & WHITNEY CANADA |
| 5 | US2022162991A1 | Compartment unit for turbine engine | 2022-05-26 | YANTAI JEREH PETROLEUM EQUIPMENT & TECHNOLOGIES CO LTD |
| 6 | US10962345B2 | Tool and method for inspecting an annular space of an engine | 2021-03-30 | GEN ELECTRIC |
| 7 | US10954855B1 | Air intake and exhaust system of turbine engine | 2021-03-23 | AMERICAN JEREH INT CORPORATION |
| 8 | US10697327B2 | Support interface and device for an engine casing | 2020-06-30 | SAFRAN AIRCRAFT ENGINES |
| 9 | US10512865B2 | Devices and methods for aligning filters in a holding frame | 2019-12-24 | EYERS WILLIAM KEITH ALBERT |
| 10 | US10371165B2 | Fan blade composite ribs | 2019-08-06 | UNITED TECHNOLOGIES CORP |
| 11 | US10137640B2 | Method for adhering parts and device for implementing said method | 2018-11-27 | SNECMA |
| 12 | US10072671B2 | Fan diffuser having a circular inlet and a rotationally asymmetrical outlet | 2018-09-11 | ENGERT MARKUS |
| 13 | US9932854B1 | Methods of cleaning a hot gas flowpath component of a turbine engine | 2018-04-03 | GEN ELECTRIC |
| 14 | US2017159570A1 | Pressure regulating device for a gas supply system of a gas turbine plant | 2017-06-08 | SIEMENS AG |
| 15 | US9567857B2 | Turbine split ring retention and anti-rotation method | 2017-02-14 | ROLLS ROYCE NAM TECH INC |
| 16 | US9541004B2 | Antagonist antibodies against EphB3 | 2017-01-10 | NOVARTIS AG |
| 17 | US2015165556A1 | Diode laser fiber array for powder bed fabrication or repair | 2015-06-18 | GEN ELECTRIC |
| 18 | US9027355B2 | Mechanical drive device for driving the high pressure sub assembly of an airplane engine | 2015-05-12 | COLOTTE BAPTISTE BENOÍT |
| 19 | US2014257666A1 | Online Enhancement for Improved Gas Turbine Performance | 2014-09-11 | GEN ELECTRIC |
| 20 | US2011168482A1 | Vane type silencers in elbow for gas turbine | 2011-07-14 | MERCHANT LAXMIKANT |
| 21 | US2010292906A1 | Method of controlling engine performance | 2010-11-18 | GIROUARD RAYMOND |
| 22 | US2010288052A1 | Method and device for implementing simulated test of centrifugal stress in turbine blade | 2010-11-18 | TANAKA TAKESHI |
| 23 | US6582187B1 | Methods and apparatus for isolating gas turbine engine bearings | 2003-06-24 | GEN ELECTRIC |
| 24 | US6481971B1 | Blade spacer | 2002-11-19 | GEN ELECTRIC |
| 25 | US6457937B1 | Fabricated torque shaft | 2002-10-01 | GEN ELECTRIC |
| 26 | US5655361A | Sound absorbing apparatus for a supersonic jet propelling engine | 1997-08-12 | MITSUBISHI HEAVY IND LTD |
| 27 | US5346365A | Gas turbine with exhaust gas casing and exhaust gas duct | 1994-09-13 | ASEA BROWN BOVERI |
| 28 | US5044883A | Water pump or the like | 1991-09-03 | NEUEDER LUDWIG |
| 29 | US3988897A | Apparatus for storing and re-utilizing electrical energy produced in an electric power-supply network | 1976-11-02 | SULZER AG |
29 records in this listing. Patents full text (MLC-0201). Request the full dataset.