USD892173S1 - Turbocharger transition section - Google Patents

Turbocharger transition section Download PDF

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Publication number
USD892173S1
USD892173S1 US29/697,886 US201929697886F USD892173S US D892173 S1 USD892173 S1 US D892173S1 US 201929697886 F US201929697886 F US 201929697886F US D892173 S USD892173 S US D892173S
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United States
Prior art keywords
turbocharger
transition section
view
transition
section
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
US29/697,886
Inventor
Harsha Vardhana Chikmangalore Manjunath
Andrew Theogift Jeyanth Selwyn Victor
Suresha Kumar Panambur
Paulraj Ramasamy
Ravikanth Bendarapu
Ramprasad Maruti Shetti
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
Transportation IP Holdings LLC
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 Transportation IP Holdings LLC filed Critical Transportation IP Holdings LLC
Priority to US29/697,886 priority Critical patent/USD892173S1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: PANAMBUR, SURESHA KUMAR, BENDARAPU, RAVIKANTH, CHIKMANGALORE MANJUNATH, HARSHA VARDHANA, RAMASAMY, PAULRAJ, SHETTI, RAMPRASAD MARUTI, JEYANTH SELWYN VICTOR, ANDREW THEOGIFT
Assigned to GE GLOBAL SOURCING LLC reassignment GE GLOBAL SOURCING LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GENERAL ELECTRIC COMPANY
Assigned to TRANSPORTATION IP HOLDINGS, LLC reassignment TRANSPORTATION IP HOLDINGS, LLC CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: GE GLOBAL SOURCING LLC
Application granted granted Critical
Publication of USD892173S1 publication Critical patent/USD892173S1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Description

FIG. 1 is a perspective view of a turbocharger transition section depicting our new design;
FIG. 2 is a front view thereof;
FIG. 3 is a rear view thereof;
FIG. 4 is a side view thereof;
FIG. 5 is an opposite side view thereof;
FIG. 6 is a top plan view thereof;
FIG. 7 is a bottom plan view thereof; and,
FIG. 8 is an additional perspective view thereof.
The broken line portion of the figures is included to show unclaimed subject matter only and forms no part of the claimed design.

Claims (1)

    CLAIM
  1. The ornamental design for a turbocharger transition section, as shown and described.
US29/697,886 2015-12-17 2019-07-11 Turbocharger transition section Active USD892173S1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/697,886 USD892173S1 (en) 2015-12-17 2019-07-11 Turbocharger transition section

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US29/548,899 USD818502S1 (en) 2015-12-17 2015-12-17 Turbocharger transition section
US29/644,877 USD859471S1 (en) 2015-12-17 2018-04-20 Turbocharger transition section
US29/697,886 USD892173S1 (en) 2015-12-17 2019-07-11 Turbocharger transition section

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US29/644,877 Division USD859471S1 (en) 2015-12-17 2018-04-20 Turbocharger transition section

Publications (1)

Publication Number Publication Date
USD892173S1 true USD892173S1 (en) 2020-08-04

Family

ID=62118338

Family Applications (3)

Application Number Title Priority Date Filing Date
US29/548,899 Active USD818502S1 (en) 2015-12-17 2015-12-17 Turbocharger transition section
US29/644,877 Active USD859471S1 (en) 2015-12-17 2018-04-20 Turbocharger transition section
US29/697,886 Active USD892173S1 (en) 2015-12-17 2019-07-11 Turbocharger transition section

Family Applications Before (2)

Application Number Title Priority Date Filing Date
US29/548,899 Active USD818502S1 (en) 2015-12-17 2015-12-17 Turbocharger transition section
US29/644,877 Active USD859471S1 (en) 2015-12-17 2018-04-20 Turbocharger transition section

Country Status (1)

Country Link
US (3) USD818502S1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD949921S1 (en) * 2020-07-17 2022-04-26 Powerhouse Engine Solutions Switzerland IP Holding GmbH Transition for engine exhaust

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD904579S1 (en) * 2019-08-06 2020-12-08 Transportation Ip Holdings, Llc Elbow pipe apparatus
USD907065S1 (en) * 2019-08-09 2021-01-05 Wehrli Custom Fabrication, Inc. Adapter for installation of a turbocharger

Citations (11)

* 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
US3371480A (en) * 1966-06-16 1968-03-05 United Aircraft Corp One and one-half stage split turbine construction
US6038861A (en) * 1998-06-10 2000-03-21 Siemens Westinghouse Power Corporation Main stage fuel mixer with premixing transition for dry low Nox (DLN) combustors
US6226978B1 (en) 1998-04-07 2001-05-08 Ghh Borsig Turbomaschinen Gmbh Hot gas-carrying gas collection pipe of gas turbine
US20020004003A1 (en) * 2000-07-04 2002-01-10 Emil Aschenbruck Device for cooling a component subject to temperature stress of nonuniform intensity
US6996992B2 (en) * 2002-08-23 2006-02-14 Man Turbo Ag Gas collection pipe carrying hot gas
US7261955B2 (en) * 2005-02-18 2007-08-28 Siemens Aktiengesellschaft MCrAlX alloy and turbine component having protective layer made from MCrAlX alloy
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
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
US20160076437A1 (en) 2010-12-21 2016-03-17 General Electric Company Apparatus and system for directing exhaust gas flow

Patent Citations (12)

* 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
US3371480A (en) * 1966-06-16 1968-03-05 United Aircraft Corp One and one-half stage split turbine construction
US6226978B1 (en) 1998-04-07 2001-05-08 Ghh Borsig Turbomaschinen Gmbh Hot gas-carrying gas collection pipe of gas turbine
US6038861A (en) * 1998-06-10 2000-03-21 Siemens Westinghouse Power Corporation Main stage fuel mixer with premixing transition for dry low Nox (DLN) combustors
US20020004003A1 (en) * 2000-07-04 2002-01-10 Emil Aschenbruck Device for cooling a component subject to temperature stress of nonuniform intensity
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
US6996992B2 (en) * 2002-08-23 2006-02-14 Man Turbo Ag Gas collection pipe carrying hot gas
US7261955B2 (en) * 2005-02-18 2007-08-28 Siemens Aktiengesellschaft MCrAlX alloy and turbine component having protective layer made from MCrAlX alloy
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
US20160076437A1 (en) 2010-12-21 2016-03-17 General Electric Company Apparatus and system for directing exhaust gas 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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD949921S1 (en) * 2020-07-17 2022-04-26 Powerhouse Engine Solutions Switzerland IP Holding GmbH Transition for engine exhaust

Also Published As

Publication number Publication date
USD859471S1 (en) 2019-09-10
USD818502S1 (en) 2018-05-22

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