Cockpit display screen portion with transitional graphical user interface

Description

FIG. 1 is a perspective view of a cockpit display screen portion with a transitional graphical user interface illustrated in a cockpit display environment, showing the image that is isolated in FIG. 2;

FIG. 2 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 3 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 4 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 5 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 6 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 7 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 8 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 9 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 10 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 11 is a front view of the portion indicated by dot-dash broken line FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 12 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 13 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 14 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 15 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design;

FIG. 16 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design; and,

FIG. 17 is a front view of the portion indicated by dot-dash broken line in FIG. 1 showing an image in a transitional sequence of the claimed design.

The appearance of the transitional graphical user interface sequentially transitions between the images shown in FIGS. 2 and 3 in a first embodiment, between the images shown in FIGS. 2 and 4 in a second embodiment, between the images shown in FIGS. 2 and 5 in a third embodiment, between the images shown in FIGS. 6 and 7 in a fourth embodiment, between the images shown in FIGS. 6 and 8 in a fifth embodiment, between the images shown in FIGS. 6 and 9 in a sixth embodiment, between the images shown in FIGS. 10 and 11 in a seventh embodiment, between the images shown in FIGS. 10 and 12 in an eighth embodiment, between the images shown in FIGS. 10 and 13 in a ninth embodiment, between the images shown in FIGS. 14 and 15 in a tenth embodiment, between the images shown in FIGS. 14 and 16 in an eleventh embodiment, and between the images shown in FIGS. 14 and 17 in a twelfth embodiment. The process or period in which one image transitions to another image forms no part of the claimed design.

The horizontally-aligned solid-lined rectangle illustrates the cockpit display screen portion.

The dot-dash broken line in FIG. 1, indicating the portion shown enlarged in FIGS. 2-17, forms no part of the claimed design.

The broken-line subject matter within the horizontally-aligned solid-lined rectangle showing portions of a graphical user interface is included for the purpose of illustrating portions of the article of manufacture and form no part of the claimed design.

The broken-line subject matter outside of the horizontally-aligned solid-lined rectangle in FIG. 1 illustrates a cockpit environment that forms no part of the claimed design.

Claims

CLAIM The ornamental design for a cockpit display screen portion with a transitional graphical user interface, as shown and described.

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Inventors:	Shapiro; Geoffrey A. (Cedar Rapids, IA), Leedom; David L. (Center Point, IA), Lorch; Matthew M. (Cedar Rapids, IA)
Applicant:	Name City State Country Type Rockwell Collins, Inc. Cedar Rapids IA US
Assignee:	Rockwell Collins, Inc. (Cedar Rapids, IA)
Appl. No.:	D/642,114
Filed:	March 27, 2018

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Related U.S. Patent Documents

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	Application Number	Filing Date	Patent Number	Issue Date
	29539379	Sep 14, 2015

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Current U.S. Class:	D14/485
Current International Class:	1404
Field of Search:	;D14/485-495 ;D20/10,11,22-33,39,40

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References Cited [Referenced By]

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U.S. Patent Documents

6690299	February 2004	Suiter
7307549	December 2007	Firra
8159464	April 2012	Gribble et al.
8193948	June 2012	Shapiro
8364328	January 2013	Hedrick
8768541	July 2014	Detouillon
8779946	July 2014	Gribble et al.
D726758	April 2015	Bourret et al.
9019128	April 2015	Kim
D736239	August 2015	Maner
D736241	August 2015	Sic
9132913	September 2015	Shapiro
9280904	March 2016	Bourret
D773532	December 2016	Gauci
D791815	July 2017	Dzjind
9703476	July 2017	Pappas
9824689	November 2017	Shapiro
D866568	November 2019	Park
D896829	September 2020	Shi
2003/0025719	February 2003	Palmer et al.
2005/0156777	July 2005	King
2007/0008188	January 2007	Firra
2011/0029919	February 2011	Woltkamp
2013/0215023	August 2013	Bourret
2014/0277857	September 2014	Bourret et al.
2015/0211883	July 2015	He
2016/0179327	June 2016	Zammit-Mangion
2016/0180718	June 2016	Shapiro et al.
2016/0350049	December 2016	Barnidge
2017/0075558	March 2017	Shapiro
2018/0322792	November 2018	Pratap

Other References

EFIS--Primary Flight Display (PFD)--Airspeed Display (iFly 747-400), by Subsonic Flight Training, YouTube [online], published on Dec. 28, 2016, [retrieved on Sep. 23, 2020], retrieved from the Internet <URL: https://www.youtube.com/watch?v=hjrELZXYUNQ> (Year: 2016). cited by examiner . FSX How to Load Gauges in Position, by ArmchairAviator, YouTube [online], published on Mar. 9, 2010, [retrieved on Sep. 23, 2020], retrieved from the Internet <URL: https://www.youtube.com/watch?v=40Amlh4Vfdl> (Year: 2010). cited by examiner . File: Primary Flight Display of a Boeing 737-800.png, by WestNest, YouTube [online]. published on May 5, 2015, [retrieved on Sep. 23, 2020], retrieved from the Internet <URL: https://en.wikipedia.org/wiki/File:Primary_Flight_Display_of_a_Boeing_737- -800.png> (Year: 2015). cited by examiner . Aircraft Electronic Instrument Systems EIS EFIS System, by Xpert Group, YouTube [online], published on Nov. 30, 2017, [retrieved on Sep. 23, 2020], retrieved from the Internet <URL:https://www.youtube.com/watch?v=MtMNDOcfg5k> (Year: 2017). cited by examiner . Touch Screens Are Tested for Piloting Passenger Jets, by Clark, nytimes.com [online], published Jul. 5, 2013, [retrieved Mar. 24, 2017], retrieved from the Internet <URL:http://www.nytimes.com/2013/07/06/technology/passenger-jets-testi- ng-touchscreen-technology.html>. cited by applicant.

Primary Examiner: Whitmore; Ian F
Attorney, Agent or Firm: Suiter Swantz pc llo

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