FIXING SYSTEM FOR PANELS AND TURBOMACHINE ENCLOSURE COMPRISING SUCH SYSTEM

Abstract

A fixing system for a panel, particularly for a noise absorption panel, including an omega stringer having a substantially omega-shaped cross-section, wherein the omega stringer includes a central portion and two lateral foot portions; a flat bar longitudinally directly connected to the central portion of the omega stringer; a sealing gasket arranged longitudinally onto the lateral foot portions of the omega stringer or onto the flat bar; wherein height of omega stringer is selected so that, when a panel is clamped between the omega stringer and the flat bar, the sealing gasket is compressed between panel and fixing system.

Claims

1. A fixing system for a composite panel comprising: an omega stringer having a substantially omega-shaped cross-section, wherein the omega stringer comprises a central portion and two lateral foot portions; a flat bar longitudinally directly connected to the central portion of the omega stringer; a sealing gasket arranged longitudinally onto the lateral foot portions of the omega stringer or onto the flat bar; wherein height of omega stringer is selected so that, when a panel is clamped between the omega stringer and the flat bar, the sealing gasket is compressed between panel and fixing system.

2. The fixing system according to claim 1, further comprising a serif arranged on the foot portions of the omega stringer or onto the flat bar, the serif being configured to limit the compression of the sealing gasket when the panel is clamped between the omega stringer and the flat bar.

3. The fixing system according to claim 1, wherein the sealing gasket is compressed with a compression rate of at least 30% of the sealing gasket height.

4. The fixing system according to claim 1, wherein the flat bar is directly connected to the central portion of the omega stringer by means of a plurality of connecting means.

5. The fixing system according to claim 4, wherein the plurality of connecting means are bolts with nuts, rivets, nails or lever closure.

6. The fixing system according to claim 1, wherein the flat bar has a width higher than the width of the central portion of the omega stringer.

7. The fixing system according to claim 6, wherein the flat bar has a width substantially equal to the width of the omega stringer.

8. The fixing system according to claim 1, wherein thickness of omega stringer is substantially equal to the thickness of the bar.

9. The turbomachine enclosure comprising: a frame realized with fixing systems according to claim 1 connected each other; a plurality of panels; wherein the panels are clamped to the frame by means of the fixing systems and the frame is arranged so to cover the turbomachine.

10. The turbomachine enclosure according to claim 9 wherein the panels are noise absorption panels.

11. The turbomachine enclosure according to claim 9, wherein the enclosure is configured to be gastight.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Further details and specific embodiments will refer to the attached drawings, in which:

[0021] FIGS. 1 and 2 are schematic views of embodiments of a fixing system known from the prior art;

[0022] FIG. 3 is a perspective view of a first embodiment of a fixing system;

[0023] Figures from 3A to 3C show different embodiments of a fixing system;

[0024] FIG. 4 is a schematic view of a component of a fixing system;

[0025] FIG. 5 is a schematic view of the embodiment of FIG. 3;

[0026] FIG. 6 is a perspective view of a second embodiment of a fixing system;

[0027] FIG. 7 is a schematic view of the embodiment of FIG. 6;

[0028] FIG. 7A shows a component of the embodiment of FIG. 6;

[0029] FIG. 8 is a perspective view of a turbomachine enclosure comprising a fixing system.

DETAILED DESCRIPTION

[0030] The following description of exemplary embodiments refers to the accompanying drawings. The same reference numbers in different drawings identify the same or similar elements. The following detailed description does not limit the invention. Instead, the scope of the invention is defined by the appended claims.

[0031] Reference throughout the specification to one embodiment or an embodiment means that a particular feature, structure, or characteristic described in connection with an embodiment is included in at least one embodiment of the subject matter disclosed. Thus, the appearance of the phrases in one embodiment or in an embodiment in various places throughout the specification is not necessarily referring to the same embodiment. Further, the particular features, structures or characteristics may be combined in any suitable manner in one or more embodiments.

[0032] FIG. 3 shows an embodiment of a fixing system 10 for a panel 17 comprising an omega stringer 14 having a substantially omega-shaped cross-section.

[0033] The omega stringer 14 comprises in turn: [0034] a central portion 12; [0035] two lateral 11, 13 foot portions, in particular: a first foot portion 11 and a second foot portion 13 symmetric each other with respect to the axis 200 of symmetry of the omega stringer 14.

[0036] In one embodiment, the omega stringer 14 is a portion of the frame of the turbomachine enclosure.

[0037] The fixing system 10 further comprises a flat bar 15 longitudinally connected, namely along the direction concordant to the one indicated by the arrow 300, to the central portion 12 of the omega stringer 14. The omega stringer 14 and the flat bar 15 are directly connected and in contact each other. A sealing gasket 16 is arranged longitudinally onto the lateral foot portions 11, 13 of the omega stringer 14. For clarity reasons, just one side of the omega (the side of the foot portion 13) is shown accommodating a panel 17 and comprising the sealing gasket 16.

[0038] As shown in FIG. 3, the space 500 is defined between the outer portion 14a of the omega stringer 14, the gasket 16 and the flat bar 15. In the space 500, the panel 17 is firmly housed.

[0039] It is further appreciated that with this arrangement the panel 17 is flush with omega stringer 14.

[0040] Figures from 3A to 3C show different embodiments relating to different possible arrangements of the sealing gasket 16.

[0041] In FIG. 3A, the fixing system 10 has two sealing gaskets 16, both arranged on foot portions 11, 13 of the omega 14.

[0042] In FIG. 3B, the fixing system 10 has two sealing gaskets 16, one arranged on the flat bar 15 and one arranged on one foot portion 13 of the omega stringer 14.

[0043] In FIG. 3C, the fixing system 10 has two sealing gaskets 16, both arranged on the flat bar 15.

[0044] The height of the omega 14 stringer is selected so that when the panel 17 is clamped between the omega stringer 14 and the flat bar 15, the sealing gasket is compressed between the between panel 17 and the fixing system 10.

[0045] FIG. 4 shows the height of a omega stringer 14. In the embodiments described, the height 20 is defined as the distance between the upper surface 110, 130, considered with respect to a floor plane A, of the foot portions 11, 13 and the upper surface 12a of the central portion 12. Therefore, its height 20 is selected so that when a panel 17 is installed, the gasket 16 is compressed and the flat bar 15 is in abutment with the surface of the panel 17.

[0046] FIG. 5 shows a schematic view of the embodiment of FIG. 3. The foot portions 11, 13 of this embodiment have a substantially rectangular cross section. The height 20 of the omega 14 allows compressing the gasket 16 of a compression rate of at least 30% of its height.

[0047] Furthermore, as shown in the enlarged portion 400, the overlapping portions 15a and 17a between the flat bar 15 and the panel 17, namely the portion of flat bar in abutment with the portion of panel 17, is each time selected to ensure proper clamping of the panel 17 with the fixing system 10.

[0048] In one embodiment of the fixing system 10, the flat bar is connected to the central portion 12 of the omega 14 stringer by means of a plurality of connecting means 18.

[0049] The thickness of omega stringer 14 is substantially equal to the thickness of the bar 15.

[0050] In the embodiment shown in FIG. 5, such connecting means 18 are bolts with nuts. In one alternative embodiment, the connecting means 18 are rivets. In one alternative embodiment, the connecting means 18 are nails. In one alternative embodiment, the connecting means 18 are lever closures.

[0051] In use, the compressed gasket 16 brings about two effects. The first effect is to ensure a proper gastight. The second effect is to increase the frictional coefficient that the panel 17 experiences when a bending force is applied.

[0052] In this way, a proper gastight of the enclosure is ensured, as well as a good mechanical behavior.

[0053] FIG. 6 shows a further embodiment of a fixing system 10. The fixing system 10 of FIG. 6 is substantially similar to the one of FIG. 3, therefore the same considerations may be done. Except for the omega stringer 14, which comprises a serif 11a, 13a on the foot portions 11, 13 configured to limit the compression of the sealing gasket 16 when the panel 17 is clamped between the omega stringer 14 and the flat bar 15.

[0054] In one alternative embodiment, the serif may be defined on the flat bar 15.

[0055] FIG. 7 shows an embodiment of a fixing system 10 wherein the omega stringer 14 comprises serif 11a, 13a on its foot portions 11, 13. In particular the serif 13a is on the terminal part of the foot portion 13; as well as the serif 11a is on the terminal part of the foot portion 11. In use, the panel 17 is housed in the space 500 (see also FIG. 3). A portion of the upper surface 17a of the panel 17 is in abutment with a portion of the lower surface 15a of the flat bar 15. The serif 11a is in abutment with the lower surface 17b (opposite to the upper surface 17a) of the panel. The gasket 16 is compressed.

[0056] FIG. 7A shows a portion of omega 14 stringer with a serif 11a on its foot portion 11. It is noted that the overall height 20 of the omega 14 is defined in the same way of the omega 14 without serif of FIG. 4. Furthermore, the omega 14 with the serif 11a has an operative eight 21, wherein the panel may be housed. Such operative eight 21 is defined as the distance between the upper surface of the serif 11a and the upper surface of the central portion 12. In this way, the compression of the gasket 16 is controllable.

[0057] FIG. 8 shows an embodiment of a turbomachine enclosure 100 comprising:

[0058] a frame realized with fixing systems 10, of the type described above connected each other, a plurality of composite panels wherein the composite panels are clamped to the frame by means of the fixing systems 10 and the frame is arranged so to cover the turbomachine.

[0059] In one embodiment, the turbomachine enclosure described above is configured to be gastight.

[0060] This written description uses examples to disclose the invention, including the preferred embodiments, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal languages of the claims.