Aircraft

Hu , et al. February 20, 2

Patent Grant D810653

U.S. patent number D810,653 [Application Number D/584,790] was granted by the patent office on 2018-02-20 for aircraft. This patent grant is currently assigned to EHANG INTELLIGENT EQUIPMENT (GUANGZHOU) CO., LTD.. The grantee listed for this patent is EHANG INTELLIGENT EQUIPMENT (GUANGZHOU) CO., LTD.. Invention is credited to Huazhi Hu, Hongsheng Jin, Xu Pan.


United States Patent D810,653
Hu ,   et al. February 20, 2018

Aircraft

Claims

CLAIM The ornamental design for an aircraft, as shown and described.
Inventors: Hu; Huazhi (Guangzhou, CN), Pan; Xu (Guangzhou, CN), Jin; Hongsheng (Guangzhou, CN)
Applicant:
Name City State Country Type

EHANG INTELLIGENT EQUIPMENT (GUANGZHOU) CO., LTD.

Guangzhou

N/A

CN
Assignee: EHANG INTELLIGENT EQUIPMENT (GUANGZHOU) CO., LTD. (Guangzhou, CN)
Appl. No.: D/584,790
Filed: November 17, 2016

Foreign Application Priority Data

May 17, 2016 [CN] 2016 3 0184752
Current U.S. Class: D12/327
Current International Class: 1201
Field of Search: ;D12/3,16.1,319-345 ;D21/436-455

References Cited [Referenced By]

U.S. Patent Documents
D197038 December 1963 Howard
D203781 February 1966 Peto
D220727 May 1971 Sawyer
D458892 June 2002 DeTore
D464604 October 2002 Jamgarov
D470079 February 2003 Lybarger
D475340 June 2003 Arata
D486775 February 2004 Reinhard
D488426 April 2004 Hall
D489315 May 2004 Dauvergne
D759764 June 2016 Lai
D763134 August 2016 Wang
D768789 October 2016 Fargeau
D772991 November 2016 Caubel
D782365 March 2017 Hung
D782366 March 2017 Xiao
D795967 August 2017 Haley
D797602 September 2017 Li
D798961 October 2017 Li
2017/0269609 September 2017 Bradlow
2017/0274983 September 2017 Beckman
2017/0295069 October 2017 Sweet, III
Primary Examiner: Spear; Robert M.
Assistant Examiner: Cash; Marissa J
Attorney, Agent or Firm: Dovas Law, P.C.

Description



FIG. 1 is a perspective view of an aircraft showing our new design;

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

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

FIG. 4 is a left side elevational view of the aircraft of FIG. 1;

FIG. 5 is a right side elevational view of the aircraft of FIG. 1;

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

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

* * * * *


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