Fixed wing aircraft with tilt rotors

Vander Lind , et al. A

Patent Grant D892710

U.S. patent number D892,710 [Application Number D/676,186] was granted by the patent office on 2020-08-11 for fixed wing aircraft with tilt rotors. This patent grant is currently assigned to Kitty Hawk Corporation. The grantee listed for this patent is Kitty Hawk Corporation. Invention is credited to Gregory Mainland Horn, Campbell McLaren, Pranay Sinha, Damon Vander Lind.


United States Patent D892,710
Vander Lind ,   et al. August 11, 2020

Fixed wing aircraft with tilt rotors

Claims

CLAIM We claim the ornamental design for a fixed wing aircraft with tilt rotors, as shown and described.
Inventors: Vander Lind; Damon (East Palo Alto, CA), Sinha; Pranay (Sunnyvale, CA), McLaren; Campbell (Alameda, CA), Horn; Gregory Mainland (Mountain View, CA)
Applicant:
Name City State Country Type

Kitty Hawk Corporation

Mountain View

CA

US
Assignee: Kitty Hawk Corporation (Palo Alto, CA)
Appl. No.: D/676,186
Filed: January 9, 2019

Current U.S. Class: D12/344
Current International Class: 1207
Field of Search: ;D12/1,2,3,4,16.1,319-345 ;D21/437-455

References Cited [Referenced By]

U.S. Patent Documents
D199070 September 1964 Ruttner
D431610 October 2000 Comacho
D492970 July 2004 Tabor
D678169 March 2013 Kennelly
9475579 October 2016 Fredericks
D799402 October 2017 Cummings
10071801 September 2018 North
D832141 October 2018 Ferner
D850357 June 2019 Cummings
10414483 September 2019 Ivans
10479482 November 2019 Kuentzel
D873202 January 2020 Tzarnotzky
10538321 January 2020 North
Primary Examiner: Cash; Marissa J
Attorney, Agent or Firm: Van Pelt, Yi & James LLP

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.

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Patent Diagrams and Documents

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