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USD885438S1 - Engine - Google Patents

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Publication number
USD885438S1
USD885438S1US29/708,406US201929708406FUSD885438SUS D885438 S1USD885438 S1US D885438S1US 201929708406 FUS201929708406 FUS 201929708406FUS D885438 SUSD885438 SUS 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 IncfiledCriticalMountain Aerospace Research Solutions Inc
Priority to US29/708,406priorityCriticalpatent/USD885438S1/en
Assigned to Mountain Aerospace Research Solutions, Inc.reassignmentMountain Aerospace Research Solutions, Inc.ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS).Assignors: STEGMAN, SCOTT, DAVIS, AARON
Application grantedgrantedCritical
Publication of USD885438S1publicationCriticalpatent/USD885438S1/en
Activelegal-statusCriticalCurrent
Anticipated expirationlegal-statusCritical

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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.
US29/708,4062019-10-052019-10-05EngineActiveUSD885438S1 (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
US29/708,406USD885438S1 (en)2019-10-052019-10-05Engine

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
US29/708,406USD885438S1 (en)2019-10-052019-10-05Engine

Publications (1)

Publication NumberPublication Date
USD885438S1true USD885438S1 (en)2020-05-26

Family

ID=70738011

Family Applications (1)

Application NumberTitlePriority DateFiling Date
US29/708,406ActiveUSD885438S1 (en)2019-10-052019-10-05Engine

Country Status (1)

CountryLink
US (1)USD885438S1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
WO2022103511A1 (en)*2020-11-102022-05-19Mountain Aerospace Research Solutions, Inc.Liquid-cooled air-breathing rocket engine

Citations (27)

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US4428191A (en)1964-10-011984-01-31Rolls Royce LimitedFuel combustion in ducted flow
USD273579S (en)*1982-03-031984-04-24The Boeing CompanyAirplane engine nacelle
US4471609A (en)*1982-08-231984-09-18The Boeing CompanyApparatus and method for minimizing engine backbone bending
US5127602A (en)*1989-11-211992-07-07Federal Express CorporationNoise reduction kit for jet turbine engines
US5282359A (en)1991-10-171994-02-01Chester Robert GImpulse jet engine
US5727378A (en)1995-08-251998-03-17Great Lakes Helicopters Inc.Gas turbine engine
EP1515035A2 (en)*2003-09-102005-03-16Short Brothers PlcA jet engine thrust reverser device
US20050060982A1 (en)*2003-09-222005-03-24General Electric CompanyMethod and system for reduction of jet engine noise
US20070245741A1 (en)*2006-04-242007-10-25General Electric CompanyMethods and system for reducing pressure losses in gas turbine engines
CA2677423A1 (en)*2007-02-142008-08-28AircelleNacelle for the jet engine of an aircraft
US20100205933A1 (en)*2008-12-082010-08-19Greg MungasRegeneratively cooled porous media jacket
US20130014515A1 (en)*2010-02-102013-01-17SnecmaLink between the exhaust casing and a structural ring of the fan duct of a jet engine
JP2013019330A (en)*2011-07-122013-01-31Ihi CorpVariable exhaust nozzle of jet engine
US20140161618A1 (en)*2011-02-162014-06-12Keystone Synergistic Enterprises, Inc.Metal Joining And Strengthening Methods Utilizing Microstructural Enhancement
US20140352797A1 (en)*2013-06-042014-12-04Rohr, Inc.Aircraft jet engine
WO2014196634A1 (en)*2013-06-062014-12-11株式会社IhiAircraft jet engine compressor blade and method for processing surface thereof
US20150377033A1 (en)*2013-02-152015-12-31United Technologies CorporationCooling hole for a gas turbine engine component
US20160040552A1 (en)*2013-03-152016-02-11General Electric CompanyModulated turbine cooling system
US20160169516A1 (en)*2013-08-162016-06-16United Technologies CorporationGas turbine engine combustor bulkhead assembly
US20160186689A1 (en)*2014-05-152016-06-30The Boeing CompanyThermoformed Cascades for Jet Engine Thrust Reversers
US20170159490A1 (en)*2015-12-072017-06-08General Electric CompanyGas turbine engine fluid cooling systems and methods of assembling the same
US20180038278A1 (en)2015-02-172018-02-08Safran Helicopter EnginesConstant-volume combustion system for a turbine engine of an aircraft engine
US20180073391A1 (en)*2016-09-132018-03-15Rolls-Royce North American Technologies, Inc.Turbine assembly with ceramic matrix composite blade track and actively cooled metallic carrier
WO2018115731A1 (en)*2016-12-202018-06-28Safran NacellesAircraft jet engine nacelle, propulsion assembly and aircraft comprising such a nacelle
US20180280851A1 (en)*2017-03-282018-10-04Rolls-Royce Deutschland Ltd & Co KgJet engine with a chamber
US20200052570A1 (en)*2017-02-162020-02-13Holcomb Scientific Research LimitedTurbofan 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 numberPriority datePublication dateAssigneeTitle
US3200589A (en)*1961-11-031965-08-17North American Aviation IncTwo stage baffled injector
US4428191A (en)1964-10-011984-01-31Rolls Royce LimitedFuel combustion in ducted flow
USD273579S (en)*1982-03-031984-04-24The Boeing CompanyAirplane engine nacelle
US4471609A (en)*1982-08-231984-09-18The Boeing CompanyApparatus and method for minimizing engine backbone bending
US5127602B1 (en)*1989-11-211995-05-02Federal Express CorpNoise reduction kit for jet turbine engines.
US5127602A (en)*1989-11-211992-07-07Federal Express CorporationNoise reduction kit for jet turbine engines
US5282359A (en)1991-10-171994-02-01Chester Robert GImpulse jet engine
US5727378A (en)1995-08-251998-03-17Great Lakes Helicopters Inc.Gas turbine engine
EP1515035A2 (en)*2003-09-102005-03-16Short Brothers PlcA jet engine thrust reverser device
US20050060982A1 (en)*2003-09-222005-03-24General Electric CompanyMethod and system for reduction of jet engine noise
US20070245741A1 (en)*2006-04-242007-10-25General Electric CompanyMethods and system for reducing pressure losses in gas turbine engines
CA2677423A1 (en)*2007-02-142008-08-28AircelleNacelle for the jet engine of an aircraft
US20100008772A1 (en)*2007-02-142010-01-14AircelleNacelle for the jet engine of an aircraft
US20100205933A1 (en)*2008-12-082010-08-19Greg MungasRegeneratively cooled porous media jacket
US20130014515A1 (en)*2010-02-102013-01-17SnecmaLink between the exhaust casing and a structural ring of the fan duct of a jet engine
US20140161618A1 (en)*2011-02-162014-06-12Keystone Synergistic Enterprises, Inc.Metal Joining And Strengthening Methods Utilizing Microstructural Enhancement
JP2013019330A (en)*2011-07-122013-01-31Ihi CorpVariable exhaust nozzle of jet engine
US20150377033A1 (en)*2013-02-152015-12-31United Technologies CorporationCooling hole for a gas turbine engine component
US20160040552A1 (en)*2013-03-152016-02-11General Electric CompanyModulated turbine cooling system
US20140352797A1 (en)*2013-06-042014-12-04Rohr, Inc.Aircraft jet engine
WO2014196634A1 (en)*2013-06-062014-12-11株式会社IhiAircraft jet engine compressor blade and method for processing surface thereof
US20160169516A1 (en)*2013-08-162016-06-16United Technologies CorporationGas turbine engine combustor bulkhead assembly
US20160186689A1 (en)*2014-05-152016-06-30The Boeing CompanyThermoformed Cascades for Jet Engine Thrust Reversers
US20180038278A1 (en)2015-02-172018-02-08Safran Helicopter EnginesConstant-volume combustion system for a turbine engine of an aircraft engine
US20170159490A1 (en)*2015-12-072017-06-08General Electric CompanyGas turbine engine fluid cooling systems and methods of assembling the same
US20180073391A1 (en)*2016-09-132018-03-15Rolls-Royce North American Technologies, Inc.Turbine assembly with ceramic matrix composite blade track and actively cooled metallic carrier
WO2018115731A1 (en)*2016-12-202018-06-28Safran NacellesAircraft jet engine nacelle, propulsion assembly and aircraft comprising such a nacelle
US20200052570A1 (en)*2017-02-162020-02-13Holcomb Scientific Research LimitedTurbofan jet engine, powered by an electric motor with power from a high efficiency electric generator
US20180280851A1 (en)*2017-03-282018-10-04Rolls-Royce Deutschland Ltd & Co KgJet engine with a chamber

Cited By (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
WO2022103511A1 (en)*2020-11-102022-05-19Mountain Aerospace Research Solutions, Inc.Liquid-cooled air-breathing rocket engine
US11635044B2 (en)2020-11-102023-04-25Mountain Aerospace Research Solutions, Inc.Liquid-cooled air-breathing rocket engine

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