Method for applying a cover to an aircraft wing and aircraft wing obtained by said method
US-2024182153-A1 · Jun 6, 2024 · US
US2021285496A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2021285496-A1 |
| Application number | US-202117196323-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 9, 2021 |
| Priority date | Mar 16, 2020 |
| Publication date | Sep 16, 2021 |
| Grant date | — |
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A housing element having a casing provided with a spherical seat, a bearing unit located inside the spherical seat of the casing and provided with a radially inner ring, and a plastic end cover provided with a radial through-hole so that a machine shaft can be inserted inside it, the end cover being integral with the shaft and rotatable with the shaft, and the end cover being provided with an elastomeric seal for forming a static seal on the shaft.
Opening claim text (preview).
What is claimed is: 1 . A housing element configured for use in a manufacturing machinery comprising: a casing provided with a spherical seat, a bearing unit located inside the spherical seat of the casing, a plastic end cover provided with an axial hole, passing through, and configured so that a machinery shaft is insertable inside, wherein the end cover is constrained to the shaft and rotatable together with the shaft, and wherein the end cover is provided with an elastomeric sealing means configured to achieve a static seal on the shaft. 2 . The housing element according to claim 1 , further comprising a first interference between a radially inner edge of the end cover and two protrusions of the sealing means, protruding radially externally on the sealing means and placed on opposite sides with respect to the radially inner edge, so as to be configured to carry out the assembly of the sealing means on the end cover. 3 . The housing element according to claim 1 , wherein the sealing means is overmoulded on the end cover. 4 . The housing element according to claim 1 , wherein the material of the elastomeric sealing means comprises polytetrafluoroethylene. 5 . The housing element according to claim 4 , wherein the material of the sealing means comprises a polytetrafluoroethylene resistant to temperatures up to 150° C. 6 . The housing element according to claim 1 , wherein the plastic material of the end cover comprises a polyamide. 7 . The housing element according to claim 1 , wherein the end cover is provided with two recesses radially recessed from a radially internal surface of the end cover and disposed on opposite halves of the end cover with respect to an axis of symmetry (Y) of the end cover. 8 . The housing element according to claim 2 , further comprising a second interference between a radially external surface of a radially inner ring of the bearing unit and the radially inner surface of the end cover so as to be configured to carry out the assembly of the end cover on the radially inner ring. 9 . The housing element according to claim 8 , wherein the second interference has a value ranging between 0 mm and 0.085 mm. 10 . A housing element configured for use in a manufacturing machinery comprising: a casing provided with a spherical seat, a bearing unit located inside the spherical seat of the casing, a plastic end cover provided with an axial hole, passing through, and configured so that a machinery shaft is insertable inside, wherein the end cover is constrained to the shaft and rotatable together with the shaft, a first interference between a radially inner edge of the end cover and two protrusions of the sealing means, protruding radially externally on the sealing means and placed on opposite sides with respect to the radially inner edge, so as to be configured to carry out the assembly of the sealing means on the end cover; and wherein the end cover is provided with an elastomeric sealing means configured to achieve a static seal on the shaft; further wherein the sealing means is overmoulded on the end cover, further wherein the material of the elastomeric sealing means comprises polytetrafluoroethylene. 11 . A housing element configured for use in a manufacturing machinery comprising: a casing provided with a spherical seat, a bearing unit located inside the spherical seat of the casing, a plastic end cover provided with an axial hole, passing through, and configured so that a machinery shaft is insertable inside, wherein the end cover is constrained to the shaft and rotatable together with the shaft, a first interference between a radially inner edge of the end cover and two protrusions of the sealing means, protruding radially externally on the sealing means and placed on opposite sides with respect to the radially inner edge, so as to be configured to carry out the assembly of the sealing means on the end cover; a second interference between a radially external surface of a radially inner ring of the bearing unit and the radially inner surface of the end cover so as to be configured to carry out the assembly of the end cover on the radially inner ring, wherein the second interference has a value ranging between 0 mm and 0.085 mm; and wherein the end cover is provided with an elastomeric sealing means configured to achieve a static seal on the shaft.
mounted to the inner race, e.g. a flinger to use centrifugal effect · CPC title
of the mounting region · CPC title
sliding on a complementary spherical surface · CPC title
with a single row or balls · CPC title
characterised by material · CPC title
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