Fixed wing aircraft with tilt rotors

Vander Lind , et al. June 8, 2

Patent Grant D921565

U.S. patent number D921,565 [Application Number D/708,019] was granted by the patent office on 2021-06-08 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 D921,565
Vander Lind ,   et al. June 8, 2021

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 (Alameda, CA), Sinha; Pranay (Sunnyvale, CA), McLaren; Campbell (Alameda, CA), Horn; Gregory Mainland (Mountain View, CA)
Applicant:
Name City State Country Type

Kitty Hawk Corporation

Palo Alto

CA

US
Assignee: Kitty Hawk Corporation (Palo Alto, CA)
Appl. No.: D/708,019
Filed: October 2, 2019

Current U.S. Class: D12/344
Current International Class: 1207
Field of Search: ;D12/1,2,3,4,16.1,174,319-345 ;D21/436-455 ;D13/109

References Cited [Referenced By]

U.S. Patent Documents
9975631 May 2018 McLaren
10046855 August 2018 Bevirt
10144503 December 2018 Vander Lind
D892710 August 2020 Vander Lind
2018/0105267 April 2018 Tighe
2018/0105279 April 2018 Tighe
2018/0334241 November 2018 Long
2020/0148347 May 2020 Bevirt
2020/0164972 May 2020 Kiesewetter
2020/0164995 May 2020 Lovering
2020/0269975 August 2020 Fink

Other References

Project Heaviside by Kitty Hawk YouTube Video (timelapse 0:59/1:13) [Oct. 3, 2019] found online [Dec. 10, 2020]--https://www.youtube.com/watch?v=q7mc3C19kE4. cited by examiner.

Primary Examiner: Voytek; John A
Attorney, Agent or Firm: Van Pelt, Yi & James LLP

Description



FIG. 1 is a perspective view taken from a top, front, and right side of a fixed wing aircraft with tilt rotors.

FIG. 2 is a front view of the aircraft of FIG. 1.

FIG. 3 is a rear view of the aircraft of FIG. 1.

FIG. 4 is a left view of the aircraft of FIG. 1.

FIG. 5 is a right view of the aircraft of FIG. 1.

FIG. 6 is a top view of the aircraft of FIG. 1; and,

FIG. 7 is a bottom view of the aircraft of FIG. 1.

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

* * * * *

References


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