This application is the U.S. National Stage of PCT/FR2021/051832, filed Oct. 20, 2021, which in turn claims priority to French patent application number 20 10781 filed Oct. 21, 2020. The content of these applications are incorporated herein by reference in their entireties.
The present invention relates to the manufacture of air intake lips of aeronautical engine nacelles.
The nacelles of aeronautical engines include an air intake cowl extended at the front by a lip having in section a U-shape open towards the rear. The air intake lip has in particular the function of ensuring the aerodynamic flow of the air, on the one hand, towards the fan channel and, on the other hand, towards the outside of the nacelle.
The large-sized air intake lips (diameter greater than one meter) are generally manufactured from several individual annular sectors assembled together subsequently, this in particular makes it easier to transport and repair the air intake lips.
The annular sectors are individually manufactured by sheet metal forming and more specifically by spin forming. The assembly of the sectors is carried out with fishplates arranged inside the sectors. Each fishplate is then fixed by screwing or riveting from the outside.
However, the manufacture of air intake lips by assembling annular sectors has drawbacks. Particularly, the assembly of the sectors leads to adjustment problems that can make it difficult to meet the geometric tolerances. Radial and/or axial offsets can occur between adjacent annular sectors, thereby affecting the aerodynamic profile of the air intake lip.
However, there is a need for the manufacture of air intake lips by assembling annular sectors for ensuring a precise adjustment between the annular sectors.
To this end, the invention proposes a method for manufacturing annular sectors of an air intake lip comprising:
Thus, by producing the annular sectors from a one-piece preform, a very good geometric and dimensional correspondence between the annular sectors is ensured, which allows precise assembly between the sectors without adjustment problems. The presence of a plunging on one of the assembly edges between two adjacent annular sectors simplifies and facilitates the assembly of the sectors together, in particular because it is no longer necessary to use fishplates. The advantages of the production of an air intake lip from annular sectors are thus retained, in particular in terms of transport and repair, while eliminating the problems of adjustment between the sectors during the production of the air intake lip.
According to one particular characteristic of the method of the invention, the three-dimensional forming surface has the shape of an ellipse with a diameter determined according to the final shape of the air intake lip. The geometry and the dimensions of the three-dimensional surface of the die are thus adapted according to the geometry and dimensions of the final air intake lip to be obtained in particular by taking into account the removal of the sacrificial portions and the overlapping of the adjacent edges of the assembled sectors.
According to another particular characteristic of the method of the invention, the revolution-shaped blank is formed of a plurality of sheet metal parts assembled together by weld beads, the revolution-shaped blank being arranged facing the three-dimensional forming surface of the die so that the position of at least part of the weld beads coincides with the position of sacrificial portions. Annular sectors devoid of weld beads are thus obtained, which makes it possible to obtain, after assembly, an air intake lip with a regular aerodynamic profile.
The object of the invention is also a method for manufacturing an air intake lip comprising the production of annular air intake lip sectors according to the invention and the assembly of the sectors by overlapping between the adjacent assembly edges and fixing of said adjacent assembly edges together so as to obtain an air intake lip. After assembly of the annular sectors, an air intake lip is thus obtained, having an improved aerodynamic profile compared to an air intake lip manufactured by assembling individually produced annular sectors, that is to say not initially extracted from the same piece.
According to one particular characteristic of the method of the invention, the fixing of the adjacent assembly edges is carried out with dismountable connecting members. This makes it possible to facilitate the repair of the lip, particularly the replacement of one or more damaged sectors.
Another object of the invention is an air intake lip comprising a plurality of annular sectors assembled together, the connection between two adjacent annular sectors comprising the overlapping between an assembly edge for one of the two annular sectors and a plunged assembly edge for the other annular sector and the fixing of said overlapping assembly edges. The presence of a plunging on one of the assembly edges between two adjacent annular sectors simplifies and facilitates the assembly of the sectors together, in particular because it is no longer necessary to use fishplates. The advantages of the production of an air intake lip from annular sectors are thus retained, in particular in terms of transport and repair, while reducing the adjustment problems between the sectors during the production of the air intake lip and lightening the overall mass of the lip.
According to one particular characteristic of the lip of the invention, each annular sector is devoid of weld beads. The air intake lip in this case has a regular aerodynamic profile.
According to another particular characteristic of the lip of the invention, the fixing of the adjacent assembly edges is carried out with dismountable connecting members.
The invention generally applies to the production of air intake lips for aeronautical engine nacelles.
As illustrated in
The sheet metal plate 10 is then cut to form a ring 20 illustrated in
The ring 20 is mechanically machined in thickness so as to obtain a constant sheet metal thickness after shaping (step S3).
A truncated cone 30 illustrated in
Once formed, the cone 30 is preformed, for example by embossing and/or stamping, into a lip blank 40 having a general shape similar to that of the final lip, that is to say already having in section a U-shape as represented in
In accordance with the invention, the final shaping of an air intake lip preform is then carried out by hydroforming (step S6). It is meant here by “hydroforming” any method that allows plastically deforming the blank by the action of a pressurized fluid, of a shock wave (EletroHydroForming (EHF), of a magnetic field (magneto-forming), etc. In the example described here and as illustrated in
Once the hydroforming is complete, a one-piece air intake lip preform 60 is obtained as illustrated in
The one-piece air intake lip preform is then cut into several annular sectors (step S7). In the example described here and as represented in
There is thus a plurality of annular sectors, in the example described here, two sectors 70 and 71, which have dimensions well suited in particular for the storage and the transport.
According to one particular aspect of the method of the invention, the position of the plunging cavities is made to coincide with all or part of the weld beads present on the lip blank such that, after the hydroforming, the weld bead(s) coincide with the position of the sacrificial portion(s). In the example described here, the blank 40 is arranged in the die 51 of the hydroforming tool so that the two weld beads 43 coincide respectively with the position of the plunging cavities 511 and 512 (
In the example described here, the annular sector 70 does not include a plunging at its ends while the annular sector 71 includes a plunging at each of its ends. Other variants of embodiment can of course be envisaged, such as, for example, providing annular sectors including an edge with plunging at one end and an edge without plunging at its other end.
Once the annular sectors have thus been produced, an air intake lip can then be manufactured by assembling the annular sectors together.
The cutting of the sacrificial portions can be carried out perpendicularly to the surface of the piece. In this case, as illustrated in
The geometry and/or the dimensions of the air intake lip vary with respect to the geometry and/or the dimensions of the air intake lip preform due to the removal of a sacrificial portion at the level of each cut-out (lengths 1610 and 1620 in
If it is desired to obtain a circular-shaped air intake lip, a die will be used, whose three-dimensional surface has circle portions corresponding to the annular sectors and extra-lengths between the circle portions corresponding to the sacrificial parts to be removed during the cutting of the sectors.
Number | Date | Country | Kind |
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2010781 | Oct 2020 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FR2021/051832 | 10/20/2021 | WO |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2022/084628 | 4/28/2022 | WO | A |
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Entry |
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Written Opinion of the International Searching Authority as issued in International Patent Application No. PCT/FR2021/051832, dated Jan. 28, 2022. |
International Search Report as issued in International Patent Application No. PCT/FR2021/051832, dated Jan. 28, 2022. |
Number | Date | Country | |
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20230302520 A1 | Sep 2023 | US |