FIG. 1 is a front left side isometric view of a wing root leading edge extension for a left wing of an aircraft showing my new design;
FIG. 2 is a top plan view of the wing root leading edge extension of FIG. 1;
FIG. 3 is a bottom plan view thereof;
FIG. 4 is a front elevational view thereof;
FIG. 5 is a rear elevational view thereof;
FIG. 6 is a left side elevational view thereof;
FIG. 7 is a right side elevational view thereof; and
FIG. 8 is a front right side isometric view of a wing root leading edge extension for a right wing of an aircraft showing my new design;
FIG. 9 is a top plan view of the wing root leading edge extension of FIG. 8;
FIG. 10 is a bottom plan view of FIG. 8;
FIG. 11 is a front elevational view of FIG. 8;
FIG. 12 is a rear elevational view of FIG. 8;
FIG. 13 is a right side elevational view of FIG. 8; and,
FIG. 14 is a left side elevational view of FIG. 8.
The broken lines on the peripheral edge of the interior surface of the wing root leading edge extension represent a boundary, the area within which forms no part of the claimed design.
Patent |
Priority |
Assignee |
Title |
2927749, |
|
|
|
3693913, |
|
|
|
3968946, |
Mar 31 1975 |
The Boeing Company |
Extendable aerodynamic fairing |
4569494, |
Dec 23 1982 |
The Boeing Company |
Pitch control of swept wing aircraft |
5314142, |
Mar 19 1991 |
Airbus Operations Limited |
Wing root aerofoil for forward swept wings |
6073889, |
Oct 16 1997 |
Boeing Company, the |
Wing flap seal bump |
6152404, |
May 13 1997 |
DaimlerChrysler Aerospace Airbus GmbH |
Apparatus for influencing a wing root airflow in an aircraft |
7510144, |
Mar 16 2006 |
EADS CONSTRUCCIONES AERONAUTICAS, S A |
Elastic pre-deformed fairings for aircrafts |
8128035, |
Apr 15 2008 |
The Boeing Company |
Winglets with recessed surfaces, and associated systems and methods |
8177170, |
Nov 08 2005 |
Airbus Operations SAS |
Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations |
20100019080, |
|
|
|
20120187252, |
|
|
|
182014, |
|
|
|
D287962, |
May 17 1984 |
BEECH AIRCRAFT CORPORATION, A CORP OF DE |
Brace for stabilizer of V-tail aircraft |