USD885438S1 - Engine - Google Patents

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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
Application number
US29/708,406
Inventor
Aaron Davis
Scott Stegman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mountain Aerospace Research Solutions Inc
Original Assignee
Mountain Aerospace Research Solutions Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mountain Aerospace Research Solutions Inc filed Critical Mountain Aerospace Research Solutions Inc
Priority to US29/708,406 priority Critical patent/USD885438S1/en
Assigned to Mountain Aerospace Research Solutions, Inc. reassignment Mountain Aerospace Research Solutions, Inc. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: STEGMAN, SCOTT, DAVIS, AARON
Application granted granted Critical
Publication of USD885438S1 publication Critical patent/USD885438S1/en
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Description

FIG. 1 is a front perspective view of an engine showing the new design.
FIG. 2 is a rear perspective view of an engine showing the new design.
FIG. 3 is a front view of an engine showing the new design.
FIG. 4 is a rear view of an engine showing the new design.
FIG. 5 is a first side view of an engine showing the new design.
FIG. 6 is a top view of an engine showing the new design.
FIG. 7 is a second side view of an engine showing the new design; and,
FIG. 8 is a bottom view of an engine showing the new design.

Claims (1)

    CLAIM
  1. The ornamental design for an engine, as shown and described.
US29/708,406 2019-10-05 2019-10-05 Engine Active USD885438S1 (en)

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

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ID=70738011

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Application Number Title Priority Date Filing Date
US29/708,406 Active USD885438S1 (en) 2019-10-05 2019-10-05 Engine

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US (1) USD885438S1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
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)

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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

Patent Citations (29)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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