Aircraft engine pylon having a mobile cowl

Patent metadata

Field	Value
Publication number	US-11780599-B2
Application number	US-202217694747-A
Country	US
Kind code	B2
Filing date	Mar 15, 2022
Priority date	Mar 17, 2021
Publication date	Oct 10, 2023
Grant date	Oct 10, 2023

Abstract

An engine pylon has a primary structure fastened between an engine and an aircraft wing and a cowling system having a front set of fixed cowls, a rear cowl, a displacement system having a first structure as one with the rear cowl and having a first slide mechanism, and a second structure fastened to a fixed structure of the wing and having second slide mechanism. The slide mechanisms cooperate so as to realize a sliding connection and to move the rear cowl in translation from an advanced position to a retracted position. An immobilizing system locks the rear cowl in the advanced position.

First claim

The invention claimed is:

1. An engine pylon of an aircraft having a wing with a fixed structure, the engine pylon having a primary structure configured to fasten an engine and the wing to each other, and a cowling system having:
a front set of cowls wherein cowls of the front set are fastened around the primary structure,
a rear cowl disposed in a continuation of and at a rear of the front set of cowls,
a displacement system having a first structure as one with the rear cowl and having first slide means, and a second structure configured to be fastened to the fixed structure of the wing and having second slide means, wherein the first slide means and the second slide means cooperate with one another so as to realize a sliding connection, so as to move the rear cowl in translation from an advanced position, in which the rear cowl is in the continuation of and at the rear of the front set of cowls, to a retracted position, in which the rear cowl is moved away, towards the rear, from the front set of cowls, and
an immobilizing system alternately adopting a locked position in which the immobilizing system immobilizes the rear cowl in the advanced position, and an unlocked position in which the immobilizing system does not immobilize the rear cowl.

2. The engine pylon according to claim 1 ,
wherein the first slide means comprises two parallel rails,
wherein each rail is fastened to the first structure,
wherein the second slide means comprises two grooves made in the second structure, and
wherein each rail slides inside one of the grooves.

3. The engine pylon according to claim 2 ,
wherein the cowling system has a plurality of positioning pegs distributed at a front of the first structure, and
wherein, for each positioning peg, the primary structure of the engine pylon has a recess in which the positioning peg is housed in the advanced position.

4. The engine pylon according to claim 3 , wherein two of the positioning pegs are constituted by front ends of the rails.

5. The engine pylon according to claim 4 , wherein one of the two positioning pegs is fastened to the first structure in a bottom part of the first structure.

6. The engine pylon according to claim 1 , wherein each cowl is constituted of just a single component.

7. The engine pylon according to claim 1 , wherein the first structure has an upper spar that extends in a generally horizontal plane and that supports the first slide means, a lower spar that is positioned obliquely and extends upwards as the lower spar progresses from the front towards the rear, and a plurality of ribs that extend in generally vertical planes and that are fastened to the lower spar and to the upper spar.

8. An aircraft comprising:
a wing,
an engine, and
an engine pylon having a primary structure configured to fasten an engine and the wing to each other, and a cowling system having:
a front set of cowls wherein cowls of the front set are fastened around the primary structure,
a rear cowl disposed in a continuation of and at a rear of the front set of cowls,
a displacement system having a first structure as one with the rear cowl and having first slide means, and a second structure configured to be fastened to the fixed structure of the wing and having second slide means, wherein the first slide means and the second slide means cooperate with one another so as to realize a sliding connection, so as to move the rear cowl in translation from an advanced position, in which the rear cowl is in the continuation of and at the rear of the front set of cowls, to a retracted position, in which the rear cowl is moved away, towards the rear, from the front set of cowls, and
an immobilizing system alternately adopting a locked position in which the immobilizing system immobilizes the rear cowl in the advanced position, and an unlocked position in which the immobilizing system does not immobilize the rear cowl,

the engine pylon being fastened between the wing and the engine.

Assignees

• Airbus Operations Sas

Inventors

• Pautis Olivier
• Blanc Jonathan

Classifications

• B64D27/402

  comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant · CPC title

• B64D29/02 Primary

  associated with wings · CPC title

• B64D27/18 Primary

  within, or attached to, wings · CPC title

• B64D27/26

  Operations & Transport · mapped topic

• B64D29/08

  Inspection panels for power plants · CPC title