Variable-section nozzle, and aircraft turbojet engine nacelle equipped with such a nozzle

Abstract

A variable-section nozzle for an aircraft nacelle includes a deformable portion of which is movable between a narrow section position and a wide section position. In particular, the variable-section nozzle includes piezoelectric actuators and a controller to control the piezoelectric actuators in order to displace the deformable portion between the narrow and wide section positions. The piezoelectric actuators can be disposed on at least one faces of the deformable portion or be disposed end-to-end to form actuating rods.

Claims

1. A variable-section nozzle for an aircraft nacelle, the variable-section nozzle comprising at least one deformable portion which is movable between a narrow section position and a wide section position, the variable-section nozzle comprising: a displacement device configured for displacing said at least one deformable portion between said narrow section position and said wide section position, wherein said displacement device comprises piezoelectric actuators stacked inside a downstream edge of said at least one deformable portion, wherein said piezoelectric actuators cause displacement of said deformable portion when subjected to an electrical voltage, and wherein said displacement device further comprises a control device to control said piezoelectric actuators; and a plurality of piezoelectric sensors positioned with the piezoelectric actuators at the downstream edge and configured to detect movements of the downstream edge of the at least one deformable portion, wherein said at least one deformable portion comprises at least one hinged flap configured to rotate radially inwardly, with respect to a longitudinal axis extending through said variable-section nozzle, and wherein a movement amplification device is directly connected with said piezoelectric actuators and is operatively connected to the at least one hinged flap, the movement amplification device comprising a lever arm configured to convert a small displacement of said piezoelectric actuators into a predetermined displacement of said at least one hinged flap.

2. The variable-section nozzle according to claim 1, wherein the at least one deformable portion rotates around a corresponding axis which is substantially perpendicular to the longitudinal axis of the aircraft nacelle.

3. The variable-section nozzle according to claim 1, wherein said lever arm is hinged around an axis placed downstream of the aircraft nacelle.

4. The variable-section nozzle according to claim 1, wherein said control device for controlling comprise an electronic supervision module configured to send the electrical voltage into said piezoelectric actuators, and an electronic acquisition module configured to receive a position voltage from said piezoelectric sensors, said electronic supervision and electronic acquisition modules defining a servo loop.

5. The variable-section nozzle according to claim 1, wherein each piezoelectric actuator comprises a piezoelectric element which comprises a multilayer complex, formed with piezo-ceramic crystals sandwiched between at least two layers of epoxy.

6. The variable-section nozzle according to claim 5, wherein said at least two layers of epoxy are sandwiched between at least two layers of polyimides, each layer of polyimide comprising embedded electrodes.

7. A nacelle for an aircraft turbojet engine comprising said variable-section nozzle according to claim 1.

Description

DRAWINGS

(1) In order that the disclosure may be well understood, there will now be described various forms thereof, given by way of example, reference being made to the accompanying drawings, in which:

(2) FIG. 1 is a perspective view of a nacelle for an aircraft turbojet engine, equipped with a variable-section nozzle in accordance with the present disclosure;

(3) FIG. 2 is an exploded perspective view of a piezoelectric actuator equipping the nacelle of FIG. 1;

(4) FIG. 3 is a axial sectional schematic view of the actuating mechanism of the nozzle flaps of FIG. 1;

(5) FIGS. 4, 5 and 6 are views similar to those of FIG. 3 of other forms of a variable-section nozzle according to the present disclosure; and

(6) FIG. 7 is a schematic view of a control circuit of a variable-section nozzle according to the present disclosure.

(7) The drawings described herein are for illustration purposes only and are not intended to limit the scope of the present disclosure in any way.

DETAILED DESCRIPTION

(8) The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. It should be understood that throughout the drawings, corresponding reference numerals indicate like or corresponding parts and features.

(9) Referring now to FIG. 1, which shows a nacelle 1 for an aircraft turbojet engine of a longitudinal axis A, equipped with a variable-section nozzle 3 in accordance with the present disclosure.

(10) In this FIG. 1, the upstream of the nacelle is shown on the left-hand side, and the downstream of this nacelle on the right-hand side.

(11) Thus, in operation, air enters through the air inlet 5 of the nacelle, and exits through the variable-section nozzle 3.

(12) In the relevant field of art, it is desirable to vary the section of the nozzle 3, during the various phases of the aircraft flight.

(13) In the form shown in FIG. 1, this variation in the nozzle outlet section is obtained by rotating the movable flaps V1, V2, V3, . . . around respective axes A1, A2, A3, . . . , these axes being substantially perpendicular to the longitudinal A axis of the nacelle.

(14) Conventionally, this rotation is obtained by means of hydraulic or electromechanical actuators.

(15) In the present disclosure, these conventional actuators are replaced by piezoelectric actuators.

(16) FIG. 2 shows an example of piezoelectric element which may be involved in making these actuators.

(17) Such a piezoelectric element can typically comprise a multilayer complex, formed with piezo-ceramic crystals 7 sandwiched between two layers 9a, 9b of epoxy, these being likewise sandwiched between two layers of polyimides 11a, 11b, in which electrodes 13a, 13b are embedded.

(18) Such piezoelectric elements are marketed for example by the company SMART MATERIAL.

(19) When an electrical voltage is passed into the electrodes 13a, 13b, the piezo-ceramic fibers 7 are deformed, leading to a variation in the thickness of the element shown in FIG. 2.

(20) Conversely, when this element is subjected to stresses coming from the surrounding members, it causes a variation in the electrical voltage measured to the terminals of these electrodes 13a, 13b.

(21) The principle of the present disclosure consists in taking advantage of these properties of the piezoelectric element shown in FIG. 2, to allow displacement of the movable portions of the variable-section nozzle 3.

(22) Thus, in the form of FIG. 1, several piezoelectric elements P can be stacked so that when they are subjected to an electrical voltage, they cause a displacement of the flaps V1, V2, V3, . . . .

(23) More specifically, as is shown in FIG. 3, a system for amplifying the movements of the piezoelectric elements P can be considered, comprising, for example, an arm 15 hinged around an axis 17 placed downstream of the nacelle 1, interposed between on the one hand the piezoelectric stack P, and on the other hand each flap V1, V2, V3, . . . , hinged around its respective axis A1, A2, A3, . . . .

(24) The system shown in FIG. 3 allows thus, through a lever arm effect, imparting to the flaps V1, V2, V3, . . . the desired movement amplitude, both outwardly and inwardly of the nacelle, as indicated by the arrow F.

(25) In the alternative shown in FIG. 4, there is no longer any flap V as shown in FIG. 1, but the downstream edge B of the nacelle 1 is deformable.

(26) This may be obtained for example by making this edge in a fine thickness sheet.

(27) In this case, in order to allow the displacements of the downstream edge of the nozzle B so as to vary the nozzle outlet section, piezoelectric elements P1, P2, are fixed on the extrados and the intrados of the edge B.

(28) Note that we could consider fixing such piezoelectric elements only on one of the faces of this edge B.

(29) These piezoelectric elements can be fixed for example by bonding onto the edge B.

(30) In the event where the edge B is made of a composite material, we can consider embedding the piezoelectric elements P1, P2 in the mass of the composite.

(31) With appropriate electrical controls of these piezoelectric elements P1, P2, the edge B can be opened outwardly of the nacelle, or pushed inwardly thereof, thus providing the means for varying the outlet nozzle section of this nacelle.

(32) In the form of FIG. 5, the piezoelectric elements P1, P2 again allow deforming the edge B inwardly or outwardly of the nacelle, as indicated by the arrow F, while noting that in this case this edge B is guided in these displacements by a system of slides 19 slidably mounted inside the rails 21 integral with the nacelle 1.

(33) In the example shown in FIG. 6, the piezoelectric elements P are stacked inside the downstream edge B of the nacelle 1, so as to form the equivalent of actuating rods.

(34) Thus, by subjecting these piezoelectric elements to appropriate electrical voltages, the rods they form can extend or retract.

(35) By correctly arranging such rods inside the edge B of the nacelle 1, the desired deformations outwardly or inwardly of the nacelle can be obtained, as indicated by the arrows F and the dotted lines shown in FIG. 6.

(36) A set of controls of the variable-section nozzle in accordance with the present disclosure is shown in FIG. 7.

(37) As shown in this figure, this set of controls comprises an electronic supervision module electrically connected to the piezoelectric actuators P1, P2 by a circuit 25 and supplied with a power current by a circuit 27.

(38) This set of controls further comprises an electronic acquisition module 29, connected by an electrical circuit 31 to a plurality of piezoelectric sensors C1, C2.

(39) The electronic supervision module 23 and the electronic acquisition module 29 are interfaced with each other, so that the set shown in FIG. 7 forms a servo loop.

(40) More specifically, when it is desired to increase or reduce the variable-section nozzle, a command is sent to the electronic supervision circuit 23, which will send via the circuit 25 electrical information to the piezoelectric actuators P1, P2, allowing making the articulation or deformation of the rear edge of the nacelle 1, as indicated above.

(41) The piezoelectric sensors C1, C2, placed so as to be able to detect the movements of the displaced or deformed portion of the downstream edge of the nacelle, in turn send to the electronic acquisition modules 29 electric information representative of this displacement or of this deformation.

(42) Communication between the module 29 and the module 23 allows acting on the piezoelectric actuators P1, P2 until the desired position or deformation is obtained.

(43) As can therefore be understood, this set of controls uses the dual property of the piezoelectric elements, consisting not only in the ability to be deformed and thus to cause a movement when they are subjected to an electric field variation, but also the ability to generate such an electric field variation when they are subjected to displacing forces.

(44) As an indication, the voltages used with the piezoelectric elements range between 100 volts and 1500 volts.

(45) As can now be understood in the light of the foregoing description, the present disclosure provides extremely simple, lightweight and space-saving means, allowing varying the section of a nacelle nozzle.

(46) Such variation is obtained by simply sending an appropriate electrical voltage into correctly placed piezoelectric elements.

(47) The present disclosure is particularly suitable for next-generation nacelles, intended for engines with a very high dilution rate, which are thinner and shorter.

(48) So far, it has never been thought to use piezoelectric elements to make variable-section nozzles, because it was thought that the forces involved were incompatible with those that such elements allow to provide.

(49) It was during repeated experiments that the applicant realized that by stacking such elements, actuating forces entirely compatible with those required in the nacelle could be obtained, and this, with an overall weight of these elements significantly lower than that of the conventional hydraulic or electromechanical actuators.

(50) Of course, the present disclosure is not limited to the forms described and shown, provided as simple examples.