USD814522S1 - Transition section for a turbocharged engine - Google Patents

Transition section for a turbocharged engine Download PDF

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Publication number
USD814522S1
USD814522S1 US29/568,787 US201629568787F USD814522S US D814522 S1 USD814522 S1 US D814522S1 US 201629568787 F US201629568787 F US 201629568787F US D814522 S USD814522 S US D814522S
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United States
Prior art keywords
transition section
turbocharged engine
engine
turbocharged
view
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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.)
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US29/568,787
Inventor
Praveen Turuvekere Gurudatt
Jayesh Jain
Andrew Theogift Jeyanth Selwyn Victor
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.)
Transportation IP Holdings LLC
Original Assignee
General Electric Co
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.)
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Priority to US29/568,787 priority Critical patent/USD814522S1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: JAIN, JAYESH, SELWYN VICTOR, ANDREW THEOGIFT JEYANTH, TURUVEKERE GURUDATT, PRAVEEN
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Publication of USD814522S1 publication Critical patent/USD814522S1/en
Assigned to GE GLOBAL SOURCING LLC reassignment GE GLOBAL SOURCING LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GENERAL ELECTRIC COMPANY
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Description

FIG. 1 is a bottom back perspective view of a design for a transition section for a turbocharged engine according to the present disclosure.
FIG. 2 is top back perspective view of the transition section for a turbocharged engine of FIG. 1.
FIG. 3 is a front view of the transition section for a turbocharged engine of FIG. 1.
FIG. 4 is a back view of the transition section for a turbocharged engine of FIG. 1.
FIG. 5 is a left side view of the transition section for a turbocharged engine of FIG. 1.
FIG. 6 is a right side view of the transition section for a turbocharged engine of FIG. 1.
FIG. 7 is a top view of the transition section for a turbocharged engine of FIG. 1; and,
FIG. 8 is bottom view of the transition section for a turbocharged engine of FIG. 1.
The transition section may be in an engine exhaust system. The dash-dot-dash lines shown by FIGS. 1, 2, 7, and 8 define the bounds of the claimed design and form no part thereof.

Claims (1)

    CLAIM
  1. The ornamental design for a transition section for a turbocharged engine, as shown and described.
US29/568,787 2016-06-21 2016-06-21 Transition section for a turbocharged engine Active USD814522S1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/568,787 USD814522S1 (en) 2016-06-21 2016-06-21 Transition section for a turbocharged engine

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Application Number Priority Date Filing Date Title
US29/568,787 USD814522S1 (en) 2016-06-21 2016-06-21 Transition section for a turbocharged engine

Publications (1)

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USD814522S1 true USD814522S1 (en) 2018-04-03

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US29/568,787 Active USD814522S1 (en) 2016-06-21 2016-06-21 Transition section for a turbocharged engine

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD931424S1 (en) * 2020-02-21 2021-09-21 Wehrli Custom Fabrication, Inc. Intake manifold bridge
USD949921S1 (en) * 2020-07-17 2022-04-26 Powerhouse Engine Solutions Switzerland IP Holding GmbH Transition for engine exhaust

Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526281A (en) * 1947-04-10 1950-10-17 Wright Aeronautical Corp Turbine and turbine nozzle construction
US4196593A (en) 1976-12-01 1980-04-08 Societe D'etudes De Machines Thermiques S.E.M.T. Internal combustion engine supercharger set
US4678397A (en) 1983-06-15 1987-07-07 Nissan Motor Co., Ltd. Variable-capacitance radial turbine having swingable tongue member
US4907952A (en) 1986-12-05 1990-03-13 Honda Giken Kogyo Kabushiki Kaisha Turbocharger
US5119633A (en) 1990-09-25 1992-06-09 Cummins Engine Company, Inc. Power turbine bypass for improved compression braking
US5619854A (en) 1994-05-25 1997-04-15 Gec Alsthom Diesels, Ltd. Turbocharged internal combustion engine
US6226978B1 (en) * 1998-04-07 2001-05-08 Ghh Borsig Turbomaschinen Gmbh Hot gas-carrying gas collection pipe of gas turbine
US6568902B2 (en) * 2000-07-04 2003-05-27 Man Turbomaschinen Ag Ghh Borsig Device for cooling a component subject to temperature stress of nonuniform intensity
US6802184B2 (en) 2000-04-20 2004-10-12 Daimlerchrysler Ag Turbocharger device for an internal combustion engine
US6996992B2 (en) * 2002-08-23 2006-02-14 Man Turbo Ag Gas collection pipe carrying hot gas
US7000634B2 (en) 2000-10-26 2006-02-21 Lindinvent Ab Adjustable valve for variable flows and a method for reducing flow through a valve
US7305827B2 (en) 2005-11-22 2007-12-11 Honeywell International, Inc. Inlet duct for rearward-facing compressor wheel, and turbocharger incorporating same
US20080127492A1 (en) * 2006-12-04 2008-06-05 Alistair Jeffrey Smith Method, System, and Computer Software Code for Repairing a Transition Section of an Engine
US7779633B2 (en) 2006-09-13 2010-08-24 Ford Global Technologies, Llc Method for determining the exhaust back pressure upstream of a turbine of an exhaust-driven turbocharger
US7877981B2 (en) 2006-06-23 2011-02-01 Ford Global Technologies, Llc Control strategy for turbocharged diesel engine
US20110123315A1 (en) 2009-11-21 2011-05-26 Robinson Lee J Multi-stage turbocharger system
US20140182290A1 (en) * 2012-12-31 2014-07-03 General Electric Company Multi-stage turbocharged engine
US20140271155A1 (en) * 2013-03-13 2014-09-18 General Electric Company Modular turbomachine inlet assembly and related inlet transition section
US8959913B2 (en) 2011-09-15 2015-02-24 General Electric Company Systems and apparatus for transferring fluid flow
EP2846027A1 (en) 2013-09-10 2015-03-11 Delphi International Operations Luxembourg S.à r.l. Method to determine exhaust manifold pressure
US20160076437A1 (en) * 2010-12-21 2016-03-17 General Electric Company Apparatus and system for directing exhaust gas flow

Patent Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2526281A (en) * 1947-04-10 1950-10-17 Wright Aeronautical Corp Turbine and turbine nozzle construction
US4196593A (en) 1976-12-01 1980-04-08 Societe D'etudes De Machines Thermiques S.E.M.T. Internal combustion engine supercharger set
US4678397A (en) 1983-06-15 1987-07-07 Nissan Motor Co., Ltd. Variable-capacitance radial turbine having swingable tongue member
US4907952A (en) 1986-12-05 1990-03-13 Honda Giken Kogyo Kabushiki Kaisha Turbocharger
US5119633A (en) 1990-09-25 1992-06-09 Cummins Engine Company, Inc. Power turbine bypass for improved compression braking
US5619854A (en) 1994-05-25 1997-04-15 Gec Alsthom Diesels, Ltd. Turbocharged internal combustion engine
US6226978B1 (en) * 1998-04-07 2001-05-08 Ghh Borsig Turbomaschinen Gmbh Hot gas-carrying gas collection pipe of gas turbine
US6802184B2 (en) 2000-04-20 2004-10-12 Daimlerchrysler Ag Turbocharger device for an internal combustion engine
US6568902B2 (en) * 2000-07-04 2003-05-27 Man Turbomaschinen Ag Ghh Borsig Device for cooling a component subject to temperature stress of nonuniform intensity
US7000634B2 (en) 2000-10-26 2006-02-21 Lindinvent Ab Adjustable valve for variable flows and a method for reducing flow through a valve
US6996992B2 (en) * 2002-08-23 2006-02-14 Man Turbo Ag Gas collection pipe carrying hot gas
US7305827B2 (en) 2005-11-22 2007-12-11 Honeywell International, Inc. Inlet duct for rearward-facing compressor wheel, and turbocharger incorporating same
US7877981B2 (en) 2006-06-23 2011-02-01 Ford Global Technologies, Llc Control strategy for turbocharged diesel engine
US7779633B2 (en) 2006-09-13 2010-08-24 Ford Global Technologies, Llc Method for determining the exhaust back pressure upstream of a turbine of an exhaust-driven turbocharger
US20080127492A1 (en) * 2006-12-04 2008-06-05 Alistair Jeffrey Smith Method, System, and Computer Software Code for Repairing a Transition Section of an Engine
US20110123315A1 (en) 2009-11-21 2011-05-26 Robinson Lee J Multi-stage turbocharger system
US20160076437A1 (en) * 2010-12-21 2016-03-17 General Electric Company Apparatus and system for directing exhaust gas flow
US8959913B2 (en) 2011-09-15 2015-02-24 General Electric Company Systems and apparatus for transferring fluid flow
US20140182290A1 (en) * 2012-12-31 2014-07-03 General Electric Company Multi-stage turbocharged engine
US20140271155A1 (en) * 2013-03-13 2014-09-18 General Electric Company Modular turbomachine inlet assembly and related inlet transition section
EP2846027A1 (en) 2013-09-10 2015-03-11 Delphi International Operations Luxembourg S.à r.l. Method to determine exhaust manifold pressure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD931424S1 (en) * 2020-02-21 2021-09-21 Wehrli Custom Fabrication, Inc. Intake manifold bridge
USD949921S1 (en) * 2020-07-17 2022-04-26 Powerhouse Engine Solutions Switzerland IP Holding GmbH Transition for engine exhaust

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