Fixed wing aircraft with tilt rotors

- Kitty Hawk Corporation
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Description

FIG. 1 is a perspective view of a fixed wing aircraft with tilt rotors showing our new design.

FIG. 2 is a front view of a fixed wing aircraft with tilt rotors showing our new design.

FIG. 3 is a back view of a fixed wing aircraft with tilt rotors showing our new design.

FIG. 4 is a left view of a fixed wing aircraft with tilt rotors showing our new design.

FIG. 5 is a right view of a fixed wing aircraft with tilt rotors showing our new design.

FIG. 6 is a top view of a fixed wing aircraft with tilt rotors showing our new design; and,

FIG. 7 is a bottom view of a fixed wing aircraft with tilt rotors showing our new design.

In the drawings, the broken lines depict portions of fixed wing aircraft with tilt rotors that forms no part of the claimed design.

Claims

We claim the ornamental design for a fixed wing aircraft with tilt rotors, as shown and described.

Referenced Cited
U.S. Patent Documents
D199070 September 1964 Ruttner
D431610 October 3, 2000 Comacho
D492970 July 13, 2004 Tabor
D678169 March 19, 2013 Kennelly
9475579 October 25, 2016 Fredericks
D799402 October 10, 2017 Cummings
10071801 September 11, 2018 North
D832141 October 30, 2018 Ferner
D850357 June 4, 2019 Cummings
10414483 September 17, 2019 Ivans
10479482 November 19, 2019 Kuentzel
D873202 January 21, 2020 Tzarnotzky
10538321 January 21, 2020 North
Patent History
Patent number: D892710
Type: Grant
Filed: Jan 9, 2019
Date of Patent: Aug 11, 2020
Assignee: Kitty Hawk Corporation (Palo Alto, CA)
Inventors: Damon Vander Lind (East Palo Alto, CA), Pranay Sinha (Sunnyvale, CA), Campbell McLaren (Alameda, CA), Gregory Mainland Horn (Mountain View, CA)
Primary Examiner: Marissa J Cash
Application Number: 29/676,186
Classifications
Current U.S. Class: Propeller Driven (D12/344)