USD631420S1 - Airplane turbine engine shield - Google Patents

Airplane turbine engine shield Download PDF

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Publication number
USD631420S1
USD631420S1 US29/341,742 US34174209F USD631420S US D631420 S1 USD631420 S1 US D631420S1 US 34174209 F US34174209 F US 34174209F US D631420 S USD631420 S US D631420S
Authority
US
United States
Prior art keywords
turbine engine
engine shield
airplane turbine
airplane
shield
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
US29/341,742
Inventor
Joseph Locklear
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.)
Individual
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Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US29/341,742 priority Critical patent/USD631420S1/en
Application granted granted Critical
Publication of USD631420S1 publication Critical patent/USD631420S1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Description

FIG. 1 is a front elevation view of an airplane turbine engine shield showing my new design;
FIG. 2 is a rear elevation view thereof;
FIG. 3 is a right elevation view thereof, the opposite side being a mirror image of the shown; and,
FIG. 4 is an in-use isometric view thereof.
The broken lines in the drawings depict environmental subject matter only and form no part of the claimed design.

Claims (1)

  1. The ornamental design for an airplane turbine engine shield, as shown and described.
US29/341,742 2009-08-12 2009-08-12 Airplane turbine engine shield Active USD631420S1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/341,742 USD631420S1 (en) 2009-08-12 2009-08-12 Airplane turbine engine shield

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/341,742 USD631420S1 (en) 2009-08-12 2009-08-12 Airplane turbine engine shield

Publications (1)

Publication Number Publication Date
USD631420S1 true USD631420S1 (en) 2011-01-25

Family

ID=43480158

Family Applications (1)

Application Number Title Priority Date Filing Date
US29/341,742 Active USD631420S1 (en) 2009-08-12 2009-08-12 Airplane turbine engine shield

Country Status (1)

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US (1) USD631420S1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130213003A1 (en) * 2009-01-16 2013-08-22 Jeffrey A. Matos Retractable bird and debris deflector for an aircraft jet engine
US8657895B2 (en) 2012-05-02 2014-02-25 Michael J. Kline Jet engine deflector
US20140360362A1 (en) * 2013-06-06 2014-12-11 General Electric Company Method and systems for particle separation in an exhaust gas recirculation system
US8968437B2 (en) 2012-05-02 2015-03-03 Michael J Kline Jet engine with deflector

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130213003A1 (en) * 2009-01-16 2013-08-22 Jeffrey A. Matos Retractable bird and debris deflector for an aircraft jet engine
US9249727B2 (en) * 2009-01-16 2016-02-02 Jeffrey A. Matos Retractable bird and debris deflector for an aircraft jet engine
US8657895B2 (en) 2012-05-02 2014-02-25 Michael J. Kline Jet engine deflector
US8945255B2 (en) 2012-05-02 2015-02-03 Michael J Kline Jet engine with deflector
US8968437B2 (en) 2012-05-02 2015-03-03 Michael J Kline Jet engine with deflector
US10024237B2 (en) 2012-05-02 2018-07-17 Michael J Kline Jet engine with deflector
US10774744B2 (en) 2012-05-02 2020-09-15 Michael J. Kline Jet engine with deflector
US11181044B2 (en) 2012-05-02 2021-11-23 Michael J. Kline Fiber-reinforced aircraft component and aircraft comprising same
US11668238B2 (en) 2012-05-02 2023-06-06 Michael J. Kline Fiber-reinforced aircraft component and aircraft comprising same
US20140360362A1 (en) * 2013-06-06 2014-12-11 General Electric Company Method and systems for particle separation in an exhaust gas recirculation system

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