USD885438S1 - Engine - Google Patents
Engine Download PDFInfo
- Publication number
- USD885438S1 USD885438S1 US29/708,406 US201929708406F USD885438S US D885438 S1 USD885438 S1 US D885438S1 US 201929708406 F US201929708406 F US 201929708406F US D885438 S USD885438 S US D885438S
- Authority
- US
- United States
- Prior art keywords
- engine
- new design
- view
- engine showing
- ornamental design
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Description
Claims (1)
- The ornamental design for an engine, as shown and described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/708,406 USD885438S1 (en) | 2019-10-05 | 2019-10-05 | Engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/708,406 USD885438S1 (en) | 2019-10-05 | 2019-10-05 | Engine |
Publications (1)
Publication Number | Publication Date |
---|---|
USD885438S1 true USD885438S1 (en) | 2020-05-26 |
Family
ID=70738011
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US29/708,406 Active USD885438S1 (en) | 2019-10-05 | 2019-10-05 | Engine |
Country Status (1)
Country | Link |
---|---|
US (1) | USD885438S1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022103511A1 (en) * | 2020-11-10 | 2022-05-19 | Mountain Aerospace Research Solutions, Inc. | Liquid-cooled air-breathing rocket engine |
Citations (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3200589A (en) * | 1961-11-03 | 1965-08-17 | North American Aviation Inc | Two stage baffled injector |
US4428191A (en) | 1964-10-01 | 1984-01-31 | Rolls Royce Limited | Fuel combustion in ducted flow |
USD273579S (en) * | 1982-03-03 | 1984-04-24 | The Boeing Company | Airplane engine nacelle |
US4471609A (en) * | 1982-08-23 | 1984-09-18 | The Boeing Company | Apparatus and method for minimizing engine backbone bending |
US5127602A (en) * | 1989-11-21 | 1992-07-07 | Federal Express Corporation | Noise reduction kit for jet turbine engines |
US5282359A (en) | 1991-10-17 | 1994-02-01 | Chester Robert G | Impulse jet engine |
US5727378A (en) | 1995-08-25 | 1998-03-17 | Great Lakes Helicopters Inc. | Gas turbine engine |
EP1515035A2 (en) * | 2003-09-10 | 2005-03-16 | Short Brothers Plc | A jet engine thrust reverser device |
US20050060982A1 (en) * | 2003-09-22 | 2005-03-24 | General Electric Company | Method and system for reduction of jet engine noise |
US20070245741A1 (en) * | 2006-04-24 | 2007-10-25 | General Electric Company | Methods and system for reducing pressure losses in gas turbine engines |
CA2677423A1 (en) * | 2007-02-14 | 2008-08-28 | Aircelle | Nacelle for the jet engine of an aircraft |
US20100205933A1 (en) * | 2008-12-08 | 2010-08-19 | Greg Mungas | Regeneratively cooled porous media jacket |
US20130014515A1 (en) * | 2010-02-10 | 2013-01-17 | Snecma | Link between the exhaust casing and a structural ring of the fan duct of a jet engine |
JP2013019330A (en) * | 2011-07-12 | 2013-01-31 | Ihi Corp | Variable exhaust nozzle of jet engine |
US20140161618A1 (en) * | 2011-02-16 | 2014-06-12 | Keystone Synergistic Enterprises, Inc. | Metal Joining And Strengthening Methods Utilizing Microstructural Enhancement |
US20140352797A1 (en) * | 2013-06-04 | 2014-12-04 | Rohr, Inc. | Aircraft jet engine |
WO2014196634A1 (en) * | 2013-06-06 | 2014-12-11 | 株式会社Ihi | Aircraft jet engine compressor blade and method for processing surface thereof |
US20150377033A1 (en) * | 2013-02-15 | 2015-12-31 | United Technologies Corporation | Cooling hole for a gas turbine engine component |
US20160040552A1 (en) * | 2013-03-15 | 2016-02-11 | General Electric Company | Modulated turbine cooling system |
US20160169516A1 (en) * | 2013-08-16 | 2016-06-16 | United Technologies Corporation | Gas turbine engine combustor bulkhead assembly |
US20160186689A1 (en) * | 2014-05-15 | 2016-06-30 | The Boeing Company | Thermoformed Cascades for Jet Engine Thrust Reversers |
US20170159490A1 (en) * | 2015-12-07 | 2017-06-08 | General Electric Company | Gas turbine engine fluid cooling systems and methods of assembling the same |
US20180038278A1 (en) | 2015-02-17 | 2018-02-08 | Safran Helicopter Engines | Constant-volume combustion system for a turbine engine of an aircraft engine |
US20180073391A1 (en) * | 2016-09-13 | 2018-03-15 | Rolls-Royce North American Technologies, Inc. | Turbine assembly with ceramic matrix composite blade track and actively cooled metallic carrier |
WO2018115731A1 (en) * | 2016-12-20 | 2018-06-28 | Safran Nacelles | Aircraft jet engine nacelle, propulsion assembly and aircraft comprising such a nacelle |
US20180280851A1 (en) * | 2017-03-28 | 2018-10-04 | Rolls-Royce Deutschland Ltd & Co Kg | Jet engine with a chamber |
US20200052570A1 (en) * | 2017-02-16 | 2020-02-13 | Holcomb Scientific Research Limited | Turbofan jet engine, powered by an electric motor with power from a high efficiency electric generator |
-
2019
- 2019-10-05 US US29/708,406 patent/USD885438S1/en active Active
Patent Citations (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3200589A (en) * | 1961-11-03 | 1965-08-17 | North American Aviation Inc | Two stage baffled injector |
US4428191A (en) | 1964-10-01 | 1984-01-31 | Rolls Royce Limited | Fuel combustion in ducted flow |
USD273579S (en) * | 1982-03-03 | 1984-04-24 | The Boeing Company | Airplane engine nacelle |
US4471609A (en) * | 1982-08-23 | 1984-09-18 | The Boeing Company | Apparatus and method for minimizing engine backbone bending |
US5127602B1 (en) * | 1989-11-21 | 1995-05-02 | Federal Express Corp | Noise reduction kit for jet turbine engines. |
US5127602A (en) * | 1989-11-21 | 1992-07-07 | Federal Express Corporation | Noise reduction kit for jet turbine engines |
US5282359A (en) | 1991-10-17 | 1994-02-01 | Chester Robert G | Impulse jet engine |
US5727378A (en) | 1995-08-25 | 1998-03-17 | Great Lakes Helicopters Inc. | Gas turbine engine |
EP1515035A2 (en) * | 2003-09-10 | 2005-03-16 | Short Brothers Plc | A jet engine thrust reverser device |
US20050060982A1 (en) * | 2003-09-22 | 2005-03-24 | General Electric Company | Method and system for reduction of jet engine noise |
US20070245741A1 (en) * | 2006-04-24 | 2007-10-25 | General Electric Company | Methods and system for reducing pressure losses in gas turbine engines |
CA2677423A1 (en) * | 2007-02-14 | 2008-08-28 | Aircelle | Nacelle for the jet engine of an aircraft |
US20100008772A1 (en) * | 2007-02-14 | 2010-01-14 | Aircelle | Nacelle for the jet engine of an aircraft |
US20100205933A1 (en) * | 2008-12-08 | 2010-08-19 | Greg Mungas | Regeneratively cooled porous media jacket |
US20130014515A1 (en) * | 2010-02-10 | 2013-01-17 | Snecma | Link between the exhaust casing and a structural ring of the fan duct of a jet engine |
US20140161618A1 (en) * | 2011-02-16 | 2014-06-12 | Keystone Synergistic Enterprises, Inc. | Metal Joining And Strengthening Methods Utilizing Microstructural Enhancement |
JP2013019330A (en) * | 2011-07-12 | 2013-01-31 | Ihi Corp | Variable exhaust nozzle of jet engine |
US20150377033A1 (en) * | 2013-02-15 | 2015-12-31 | United Technologies Corporation | Cooling hole for a gas turbine engine component |
US20160040552A1 (en) * | 2013-03-15 | 2016-02-11 | General Electric Company | Modulated turbine cooling system |
US20140352797A1 (en) * | 2013-06-04 | 2014-12-04 | Rohr, Inc. | Aircraft jet engine |
WO2014196634A1 (en) * | 2013-06-06 | 2014-12-11 | 株式会社Ihi | Aircraft jet engine compressor blade and method for processing surface thereof |
US20160169516A1 (en) * | 2013-08-16 | 2016-06-16 | United Technologies Corporation | Gas turbine engine combustor bulkhead assembly |
US20160186689A1 (en) * | 2014-05-15 | 2016-06-30 | The Boeing Company | Thermoformed Cascades for Jet Engine Thrust Reversers |
US20180038278A1 (en) | 2015-02-17 | 2018-02-08 | Safran Helicopter Engines | Constant-volume combustion system for a turbine engine of an aircraft engine |
US20170159490A1 (en) * | 2015-12-07 | 2017-06-08 | General Electric Company | Gas turbine engine fluid cooling systems and methods of assembling the same |
US20180073391A1 (en) * | 2016-09-13 | 2018-03-15 | Rolls-Royce North American Technologies, Inc. | Turbine assembly with ceramic matrix composite blade track and actively cooled metallic carrier |
WO2018115731A1 (en) * | 2016-12-20 | 2018-06-28 | Safran Nacelles | Aircraft jet engine nacelle, propulsion assembly and aircraft comprising such a nacelle |
US20200052570A1 (en) * | 2017-02-16 | 2020-02-13 | Holcomb Scientific Research Limited | Turbofan jet engine, powered by an electric motor with power from a high efficiency electric generator |
US20180280851A1 (en) * | 2017-03-28 | 2018-10-04 | Rolls-Royce Deutschland Ltd & Co Kg | Jet engine with a chamber |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2022103511A1 (en) * | 2020-11-10 | 2022-05-19 | Mountain Aerospace Research Solutions, Inc. | Liquid-cooled air-breathing rocket engine |
US11635044B2 (en) | 2020-11-10 | 2023-04-25 | Mountain Aerospace Research Solutions, Inc. | Liquid-cooled air-breathing rocket engine |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
USD903577S1 (en) | Aircraft | |
USD952609S1 (en) | Case with earphones | |
USD916291S1 (en) | Earpiece | |
USD928743S1 (en) | Earphone | |
USD939438S1 (en) | Charger | |
USD884165S1 (en) | Mounting cradle | |
USD884972S1 (en) | Shaver | |
USD896200S1 (en) | Earphones | |
USD864084S1 (en) | Aircraft | |
USD1028742S1 (en) | Watch | |
USD980625S1 (en) | Case | |
USD977251S1 (en) | Organizer | |
USD960024S1 (en) | Ring | |
USD904228S1 (en) | Automobile | |
USD907545S1 (en) | Engine hood | |
USD957893S1 (en) | Organizer | |
USD926436S1 (en) | Blouson | |
USD902847S1 (en) | Charger | |
USD939182S1 (en) | Snack | |
USD982066S1 (en) | Spectacles | |
USD894276S1 (en) | Whiteboard | |
USD936558S1 (en) | Boat | |
USD1017642S1 (en) | Manifold | |
USD904303S1 (en) | Stirling engine | |
USD922907S1 (en) | Automobile |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FEPP | Fee payment procedure |
Free format text: ENTITY STATUS SET TO UNDISCOUNTED (ORIGINAL EVENT CODE: BIG.); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |
|
FEPP | Fee payment procedure |
Free format text: ENTITY STATUS SET TO SMALL (ORIGINAL EVENT CODE: SMAL); ENTITY STATUS OF PATENT OWNER: SMALL ENTITY |