Aircraft propulsion unit comprising a nacelle provided with a fan cowl locking and closing mechanism

Patent metadata

Field	Value
Publication number	US-9643714-B2
Application number	US-201414514639-A
Country	US
Kind code	B2
Filing date	Oct 15, 2014
Priority date	Oct 18, 2013
Publication date	May 9, 2017
Grant date	May 9, 2017

Abstract

An aircraft propulsion unit comprising a nacelle with a fan cowl locking and closing mechanism. The fan cowls of the nacelle can be closed by a single operator in accordance with the ergonomic standards defined for a single individual. A nacelle is provided with a lateral locking mechanism configured to keep one of the two fan cowls in the closed position, so as to reduce the spacing between the two lower sides of the fan cowls, whereas the presence of a stop between a first elastic member provided on one fan cowl and a second elastic member provided on the other fan cowl allows the operator to provide only that effort required to overcome the force exerted by a single spring at a time.

First claim

The invention claimed is:

1. An aircraft propulsion unit comprising:
a nacelle surrounding a propulsion member,
the nacelle being substantially cylindrical and centered about a longitudinal axis and having a first and a second fan cowl arranged on both sides of a first plane of symmetry of the nacelle comprising the longitudinal axis,
said fan cowls being movable between a closed position in which a lower side of the first fan cowl and a lower side of the second fan cowl are contiguous and an open position in which said lower sides are spaced apart,
the nacelle moreover comprising a spacing mechanism having a first and a second elastic member,
the first elastic member being fixed to the first fan cowl and the second elastic member being fixed to the second fan cowl,
the nacelle further comprising at least one lateral locking mechanism having an anchoring point fixed to the nacelle and a movable member fixed to one of the first or the second fan cowl, and
the movable member being capable of being displaced towards a deployed position in which the movable member is fixed to the anchoring point when the fan cowl is in the closed position,
wherein each of said elastic members comprises a body confining an elastic element and a first end of a rod, the elastic element exerting a force on said first end, such that one free end of the rod extends beyond the body in a plane perpendicular to the longitudinal axis, the spacing mechanism moreover comprising a stop that is fixed in relation to the nacelle, the stop comprising a planar wall in the first plane of symmetry, the free end of the rod of each of said elastic members being supported against said planar wall when the fan cowl on which said elastic member is fixed is displaced towards the closed position.

2. The aircraft propulsion unit according to claim 1 , wherein the lateral locking mechanism is arranged in a second plane of symmetry of the nacelle, the second plane of symmetry comprising the longitudinal axis and being substantially perpendicular to the first plane of symmetry.

3. The aircraft propulsion unit according to claim 1 , wherein the stop is fixed to the nacelle.

4. The aircraft propulsion unit according to claim 1 , wherein the stop is fixed to the propulsion unit.

5. An aircraft comprising a propulsion unit comprising:
a nacelle surrounding a propulsion member,
the nacelle being substantially cylindrical and centered about a longitudinal axis and having a first and a second fan cowl arranged on both sides of a first plane of symmetry of the nacelle comprising the longitudinal axis,
said fan cowls being movable between a closed position in which a lower side of the first fan cowl and a lower side of the second fan cowl are contiguous and an open position in which said lower sides are spaced apart,
the nacelle moreover comprising a spacing mechanism having a first and a second elastic member,
the first elastic member being fixed to the first fan cowl and the second elastic member being fixed to the second fan cowl,
the nacelle further comprising at least one lateral locking mechanism having an anchoring point fixed to the nacelle and a movable member fixed to one of the first or the second fan cowl, and the movable member being capable of being displaced towards a deployed position in which the movable member is fixed to the anchoring point when the fan cowl is in the closed position,
wherein each of said elastic members comprises a body confining an elastic element and a first end of a rod, the elastic element exerting a force on said first end, such that one free end of the rod extends beyond the body in a plane perpendicular to the longitudinal axis, the spacing mechanism moreover comprising a stop that is fixed in relation to the nacelle, the stop comprising a planar wall in the first plane of symmetry, the free end of the rod of each of said elastic members being supported against said planar wall when the fan cowl on which said elastic member is fixed is displaced towards the closed position.

Assignees

• Airbus Operations Sas
• Airbus Operations Sas

Inventors

• Bulin Guillaume
• Oberle Patrick
• Devienne Nicolas
• Ritter Matthieu

Classifications

• B64D29/06 Primary

  Attaching of nacelles, fairings or cowlings · CPC title

• B64C7/02 Primary

  Nacelles · CPC title