Device for articulating a door of a nacelle of an aircraft and nacelle provided with said articulation device

An articulation device connects a door (46) of an aircraft nacelle (30), the nacelle (30) including an external wall called a fairing including at least one opening (44) adapted to be closed by at least the door (46). The articulation device includes at least one arm (56) connected by a first pivotal axle (58) to the nacelle (30) and by a second pivotal axle (60) to the door (46), the two pivotal axles (58, 60) being substantially parallel.

FIELD OF THE INVENTION

The present invention relates to a device for the articulation of a good of an aircraft nacelle as well as an aircraft nacelle provided with said articulation device.

BACKGROUND OF THE INVENTION

The motors of aircraft are generally integrated within a structure, called in what follows a nacelle, connected by connection means to the aircraft, particularly by a mast to the wing.

This nacelle has several functions, particularly those of regulating and controlling the movements of the air about and in the motor so as to optimize the aerodynamic flows, to protect the motor from external elements, to attenuate sonic nuisance, to ventilate the internal zones, to take part in the distribution of mechanical forces of the motor and if desired to support systems for pressure reversal.

Finally, the nacelle should permit the routine maintenance and upkeep of the motor and its components.

To this end, the nacelle comprises, at the level of its external surface, an opening permitting access to the interior of the nacelle and a movable part adapted to occupy at least two positions, a first so-called closed position in which said movable part is disposed in prolongation of the external surface of the nacelle so as to close said opening, and a second position in which it frees at least partially the opening.

In what follows of the description, the movable portion is called a door.

InFIGS. 1 and 2, there is shown at10a nacelle connected by a mast12to a wing14, said nacelle comprising a front air inlet16and a lateral fuselage18with a longitudinal axis20. The nacelle10comprises at least one opening22, preferably two disposed on each side, on opposite sides of the mast12, adapted each to be closed respectively by a door24.

According to the prior art, each door24is articulated relative to the upper edge of the opening22and pivots about an axis26substantially parallel to the axis20of the nacelle, disposed near the mast12.

As a supplement, locking means are provided to hold the doors24closed. According to one embodiment, the lower ends of the doors are connected when these latter are in closed position, by bolts (not shown).

Preferably, as shown inFIG. 2, two props28are provided to hold each door in open position.

Even if this type of door is relatively simple and permits easy access to the elements mounted in the lower portion of the motor, it does not give complete satisfaction for the following reasons:

The positioning of the door in the open position facing the opening at the level of the medial portion of the upper portion, does not favor access to these parts. Thus, the operators must slide between the door and the motor first of all lowering themselves to pass below the panel of the door, taking the risk of injuring themselves against the edges of the door.

However, this manner of opening does not permit ensuring optimum safety to the operators. Thus, even if they are held by props, the doors can close abruptly, especially due to gusts of wind, and injure the operator disposed between the door and the motor.

As shown inFIG. 1, the upper portions of the existing articulated doors have a large wind profile even though the doors are dimensioned to resist wind gusts of the order of 100 Km/h. However, these stresses in the open position are much greater than those to which the doors are subjected in closed position. Thus, the doors are dimensioned for unusual use.

Finally, for a door of large size, its manipulation can be difficult, the operator having to raise said doors to effect the opening. In excess of certain dimensions, it is necessary to provide an onboard system for assisting opening and closing, complicating the design and increasing the installed weight of the aircraft.

Moreover, certain installation of propulsive systems, particularly of large size, can be relatively near the other portions of the aircraft, with configurations that can give rise to interference between the door in open position and the air foil or the nose of the attack edge in deployed position, or any other fixed or movable surface. It is necessary in these cases to provide protection which add a further increase of weight and complexity to the aircraft.

Also, the present invention seeks to overcome the drawbacks of the prior art by providing an articulation device for a door of an aircraft nacelle, permitting freeing in an optimum manner the opening and rendering the intervention of the operators more certain, and possibly lightening the nacelle.

SUMMARY OF THE INVENTION

To this end, the invention has for its object an articulation device connecting a door of an aircraft nacelle, said nacelle comprising an external wall called fairing comprising at least one opening adapted to be closed by at least one said door, characterized in that the articulation device comprises at least one arm connected by means of a first pivotal axis to a nacelle and by means of a second pivotal axis to the door, the two pivotal axes being substantially parallel.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

InFIG. 3there is shown at30an aircraft nacelle connected by means of a mast32to a wing34. This nacelle comprises in the direction of the airflow an air inlet36, a nozzle38connected by an external wall or frame40with substantially circular sections perpendicular to the longitudinal axis42of the nacelle, said nacelle comprising a motor.

However, the invention is not limited to this embodiment and covers all the different variations of material of the connecting elements between the nacelle and the rest of the aircraft, the anchoring region of the nacelle, the shapes, dimensions and materials of the nacelle, the type of motor and the emplacement of the motor.

So as to be able to act within the nacelle, below the fairing, and have access to the motor, to it components and/or its accessories, the nacelle comprises at the level of its fairing40, at least one opening44adapted to be closed by at least one movable part called in what follows door46. Thus, the door46is adapted to occupy a first position, called closed, in which it closes the opening and comes substantially into prolongation of the fairing so as to reduce disturbances in the air flow about the nacelle, and another position, called open, in which it frees at least in part the opening40, as shown inFIGS. 3 and 5.

Preferably, the nacelle comprises two openings44and two corresponding doors46disposed on opposite sides of the mast, the doors extending from the mast to the lower part of the nacelle.

According to one configuration, the opening44has lateral edges in planes substantially perpendicular to the longitudinal axis42of the nacelle, a lateral front edge48and a lateral rear edge50(in the direction of air flow in the nacelle) and respectively lower52and upper54edges substantially parallel to the longitudinal axis42of the nacelle, the corresponding door46having shapes adapted to the opening.

Preferably, the doors do not comprise pressure reversers and are disposed at the level of the zones of fairing of the nacelle but do not comprise pressure reversers to the extent to which the reversers give rise to relatively great forces on the nacelle. On the contrary, if the pressure reversers give rise only to small forces compatible with the door, they can be disposed at the level of this latter.

So as to promote the relative movement of the door46relative to the nacelle30, articulation means are provided.

These articulation means will now be described for a door, the other door or doors having the same articulation mechanism or another one.

According to the invention, the articulation means comprise at least one arm56connected by means of a first pivotal axle58to the nacelle and by means of a second pivotal axle60to the door46, the two pivotal axles being substantially parallel. This arrangement permits spacing the door46from the nacelle so as to facilitate access to the opening.

Preferably, the first pivotal axle58is offset inwardly of the nacelle relative to the fairing and the arm56has a suitable shape, particularly an elbow, such that the door will be adapted to be disposed substantially parallel and adjacent the fairing of the nacelle in the open position, as shown inFIGS. 3 and 5.

Preferably, the length of the arm56and the position of the connection of said arm to the door are adjusted to the dimensions of the door46such that this latter will be offset relative to the opening44in the open position and entirely frees said opening. This configuration gives rise to better access to the opening. Moreover, according to this arrangement, the operator is not positioned between the nacelle and the door as in the prior art, which permits increasing his safety. Finally, the door46being substantially pressed against the fairing of the nacelle, it offers a lower wind resistance, which contributes to reducing the risk of abrupt closure and decreasing the weight of the door, this latter in open position being subjected to lower stresses connected with the wind.

According to one embodiment, the pivotal axles58and60are substantially parallel to the front lateral edge48of the opening, the first pivotal axle58being disposed at the level of the edge of the lateral front edge48. The second pivotal axle60is provided substantially in the middle of the door.

The movement of the center of gravity of the door being located in a substantially horizontal plane, the risk of accidents caused by self closure of the door is extremely reduced compared to the kinematics of the prior art according to which the weight of the door has a tendency to cause self closure.

Preferably, the pivotal axles58and60are slightly inclined relative to the vertical so as to obtain a stable open condition of the door and/or to facilitate the opening of the door thanks to the weight of said door.

According to another characteristic of the invention, the door comprises locking means to hold it in closed position.

To this end, the lateral front edge48of the opening comprises a first throat62whose opening is oriented rearwardly, adapted to receive the front lateral edge64of the door46and the rear lateral edge50of the opening comprises a second throat66whose opening is oriented radially outwardly of the nacelle, adapted to receive the rear lateral incurved edge68of the door46.

As a supplement, the arm is in at least two portions having at least one degree of freedom relative to each other.

According to a first modification shown inFIGS. 4A,4B,4C and5, the arm56comprises a first portion70articulated relative to the nacelle, a second portion72articulated relative to the door and a third pivotal axle74, connecting the two portions70and72, substantially parallel to the pivotal axles58and60.

According to another modification shown inFIGS. 8A to 8D, the arm56is telescopic and comprises a first portion76articulated relative to the nacelle, a second portion78articulated relative to the door, the portions76and78being sliding relative to each other.

The third arrangement according to the invention requires a door having at least three degrees of freedom, as shown inFIGS. 4A to 4Cor8A to8D. Thus, the first modification comprises three degrees of freedom provided by articulations58,60and74. The second modification comprises three degrees of freedom provided by the two articulations58and60and translation between the portions76and78.

This arrangement permits obtaining the immobilization of the door46in closed position, the forces exerted particularly by the air flow about the nacelle tending to hold the door in closed position.

Thus, in this case, the air flows tend to hold the lateral rear incurved edge68in the second throat66which prevents the door to move rearwardly and the retraction of the front lateral edge64of the first throat62.

So as to ensure more certain locking, bolts can be provided to prevent the rear lateral edge68of the door to disengage from the second throat66. This locking can be completed by adding bolts to prevent the door from recoiling. The bolts are preferably disposed at about half the height of the door, to remain accessible, two bolts disposed in the rear and two others in the front.

The bolts are not described further, because they can take different forms, forms already known and used in the prior art.

InFIG. 6, there is shown an embodiment of the arm56. The different portions of the arm as well as the articulations are dimensioned so as to absorb forces and the different stresses exerted particularly by the door. As shown inFIG. 6, the portions of the arm can be present in the form of a simple element such as the second portion72or with openings as in the first portion70.

The positioning of the throats as well as the shapes of the lateral edges64and68of the door are determined such that the external surface of the door will be in prolongation of the fairing so as not to disturb the air flow about the nacelle when the door is closed.

Thus, the first throat62has a U shaped cross-section with one arm of the U disposed in prolongation of the fairing, the other arm being offset inwardly of the nacelle. As a supplement, the lateral front edge64of the door comprises a slight recess. Thus, when said edge64is disposed within the throat62, the rest of the surface of the door is disposed in prolongation of the fairing of the nacelle.

As a modification, the front lateral edge68can be slid below the surface of the nacelle.

The second throat66also has a U shaped cross-section whose ends of the branches are offset inwardly of the nacelle such that when the door comes into contact with said throat or the end of the branches of the U, the external surface of the door will be in prolongation of the fairing of the nacelle. As a supplement, the rear lateral edge68of the door is bent to substantially900so as to coact with the second throat66.

According to one embodiment, the first throat62can be prolonged at the level of the lower edge52and/or of the upper edge54of the opening. This configuration permits preventing the spacing of the door at the level of the upper and lower ends.

More generally, the front lateral edge of the door46and/or the front lateral edge of the opening44comprise means to prevent relative radial movement between these two elements and the side rear edge of the door46and/or the side rear edge of the opening44comprise means to prevent relative longitudinal movement (parallel to the axis of the nacelle) between these two elements.

The operation of the door will now be described with respect toFIGS. 4A to 4C,5,7A to7F and8A to8D.

In closed position, as shown inFIGS. 4A,7A and8A, the lateral edges64,68of the door are engaged in their respective throats62and66. In this position, the external surface of the door is disposed in prolongation of the fairing of the nacelle.

Once engaged in these two throats, the door cannot open with a simple movement.

To open the door46, after unlocking, the rear of the door has to be slightly pivoted, as shown inFIGS. 4B and 8B, so as to disengage the lateral rear edge68of the door from the second throat66.

After this step, the door46can translate rearwardly, as shown inFIGS. 4C,7B,7C and8C, so as to disengage the front lateral edge64from the first throat62.

The door46can then pivot, as shown inFIGS. 7D and 7E, so as to come before the opening44in the open position, as shown inFIGS. 5,7F and8D.

To close the door, the above steps should be carried out in reverse order, by beginning with engagement of the lateral front edge in the first throat, then the lateral rear edge in the second throat and finally by locking the door in the closed position.

Preferably, alignment pins can be provided to facilitate the engagement of the lateral edges of the door in their respective throats.

Preferably, the internal surface of the door comprises buffers so as not to damage the fairing of the nacelle when the door is disposed in open position.

According to another characteristic, the arm comprises a first portion70shorter than the second portion72. The shorter portion70permits small adjustments of the door as well as the clearance necessary to open the door completely. The longer portion72permits manipulating the door over wide movements.