Autothrottle for an aircraft

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Description

FIG. 1 is a front, top, left side perspective view of an autothrottle for an aircraft showing our new design, shown in a condition of use;

FIG. 2 is a front, top, right side perspective view thereof;

FIG. 3 is a front elevation view thereof;

FIG. 4 is a left side elevation view thereof;

FIG. 5 is a right side elevation view thereof;

FIG. 6 is a top plan view thereof; and,

FIG. 7 is a front, top, left side perspective view thereof.

The dashed broken lines depict portions of the autothrottle for an aircraft that form no part of the claimed design. The dashed broken lines in FIGS. 1 to 7 showing a cockpit depict environmental structure that forms no part of the claimed design.

Claims

The ornamental design for an autothrottle for an aircraft as shown and described.

Referenced Cited
U.S. Patent Documents
D553554 October 23, 2007 Figueiredo
D575212 August 19, 2008 Tsay
D592126 May 12, 2009 da Silveira
D759569 June 21, 2016 Kasparian
D759574 June 21, 2016 Kasparian
D871290 December 31, 2019 Kasparian
D879704 March 31, 2020 Kasparian
Patent History
Patent number: D1092319
Type: Grant
Filed: Dec 29, 2023
Date of Patent: Sep 9, 2025
Assignee: AEROJONES AVIATION TECHNOLOGY CO., LTD. (Taichung)
Inventors: Dmitriy Kvarta (Strausberg), Po-Chen Chen (Strausberg)
Primary Examiner: Jerry Shiuan-Hua Hsu
Application Number: 29/923,532
Classifications