Device for protecting the airfoils of an aircraft against bad weather and positioning method

Patent metadata

Field	Value
Publication number	US-10549867-B2
Application number	US-201715842584-A
Country	US
Kind code	B2
Filing date	Dec 14, 2017
Priority date	Dec 15, 2016
Publication date	Feb 4, 2020
Grant date	Feb 4, 2020

Abstract

Devices for protecting aircraft against bad weather. A device for protecting a wing of an aircraft including a load-bearing structure for a protective wall for the wing, the load-bearing structure having a supporting frame having at least two uprights linked by at least one cross member, at least one upright, at the end of the frame having a linking attachment arrangement permitting at least rotation about an axis perpendicular to the surface, the other uprights, each having one foot with an arrangement configured to facilitate the movement of the frame over the surface on which the frame rests. The protection device enables immediate, rapid and easy positioning requiring very few operators.

First claim

The invention claimed is:

1. A protection device for a wing of an aircraft while the aircraft is on the ground, comprising:
a protective wall for the aircraft wing sized and shaped to cover an entirety of the aircraft wing;
a load-bearing structure for the protective wall, the load-bearing structure comprising:
a supporting frame having at least two uprights linked by at least one cross member extending in a longitudinal direction between the at least two uprights, the supporting frame comprising a lattice structure having guys extending laterally away from the uprights in a cantilevered manner,
at least one of the uprights, comprising a static upright, at a first end of the frame being attached to the ground by a link permitting at least rotation about one axis,
the remaining one or more uprights, each comprising a moveable upright and having one foot with means configured to facilitate the movement of the frame over a surface on which the frame stands.

2. The protection device according to claim 1 , wherein the protective wall has edges and one of the edges opposite the static upright has a cushioned roll.

3. The protection device according to claim 1 , wherein the foot of each of the remaining one or more uprights is provided with a caster, and at least one caster is motorized to enable the frame to be moved.

4. The protection device according to claim 1 , wherein the foot of each of the remaining one or more uprights has a stabilizer.

5. The protection device according to claim 1 , wherein the cover wall has a width at the first end of the frame and a width at a second, opposite end of the frame, wherein the width at the second end is greater than the width at the first end.

6. The protection device according to claim 1 , wherein the cover wall includes a portion extending transversely greater than a transverse dimension of a remainder of the cover wall.

7. A system for protecting wings of an aircraft while the aircraft is on the ground, including two protection devices, each comprising:
a protective wall for the aircraft wing sized and shaped to cover an entirety of the aircraft wing,
a load-bearing structure for the protective wall, the load-bearing structure comprising:
a supporting frame having at least two uprights linked by at least one cross member extending in a longitudinal direction between the at least two uprights, the supporting frame comprising a lattice structure having guys extending laterally away from the uprights in a cantilevered manner,
at least one of the uprights, comprising a static upright, at a first end of the frame being attached to the ground by a link permitting at least rotation about one axis,
the remaining one or more uprights, each comprising a moveable upright and having one foot with means configured to facilitate the movement of the frame over a surface on which the frame stands,
a cushioned roll being arranged at a second end of the frame, opposite the first end
wherein the surface, on which the aircraft stands, includes attachment means complementing those provided on the linking static upright, enabling at least rotation about an axis perpendicular to said surface.

8. The protection system according to claim 7 , wherein a marking visually identifying the path of each protection device is provided on said surface.

9. A method for using the protection device according to claim 1 for a wing of an aircraft, comprising:
moving the protection device, including a protective wall for the aircraft wing sized and shaped to cover an entirety of the aircraft wing, to the wing of the aircraft,
arranging the frame alongside a leading edge or trailing edge of the wing such that the wall extends over and covers an entire surface of said wing.

10. The method according to claim 9 , further comprising:
positioning the aircraft between two protection devices,
moving the protection devices to an operational position in which the wings of the aircraft are protected,
stopping and locking the protection devices in an operational position,
moving the protection devices to an idle position in which the aircraft is released,
stopping and locking the protection devices in the idle position.

11. A protection device system for use with an aircraft on the ground, comprising:
an aircraft having a wing of a predetermined size and shape;
a protective wall for the aircraft wing sized and shaped to cover an entirety of the aircraft wing;
a load-bearing structure for the protective wall, the load-bearing structure comprising:
a supporting frame having at least two uprights linked by at least one cross member extending in a longitudinal direction between the at least two uprights, the supporting frame comprising a lattice structure having guys extending laterally away from the uprights in a cantilevered manner,
at least one of the uprights, comprising a static upright, at a first end of the frame being attached to the ground by a link permitting at least rotation about one axis,
the remaining one or more uprights, each comprising a moveable upright and having one foot with means configured to facilitate the movement of the frame over a surface on which the frame stands.

12. The protection device according to claim 11 , wherein the protective wall has edges and one of the edges opposite the static upright has a cushioned roll.

13. The protection device according to claim 11 , wherein the foot of each of the remaining one or more uprights is provided with a caster, and at least one caster is motorized to enable the frame to be moved.

14. The protection device according to claim 11 , wherein the foot of each of the remaining one or more uprights has a stabilizer.

Assignees

• Airbus Operations Sas

Inventors

• Mateo Stéphane
• Hector Romain
• Couet Christophe

Classifications

• B64F1/005 Primary

  Protective coverings for aircraft not in use · CPC title

• B64F1/36

  Other airport installations (ground installations for de-icing aircraft B64F5/20) · CPC title