Patent US4516909A successfully refreshed from Google Patents.
US4516909A
Expired / Lapsed
US
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Helicopter Rotor
Assignee: AUGUSTA SPA CASCINA COSTA DI SAMARATE (VARESE)
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Filing: 1983-03-02
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Granted: 1985-05-14
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Expires: 2003-03-02
Abstract
Abstract A helicopter rotor in which a central plate-like hub is provided with a plurality of axial apertures uniformly distributed around a central axis of rotation and each defined radially outwardly by a supporting peripheral bridge connected to a respective blade by a U-shape structure extending through the said aperture and coupled to the associated bridge by an elastomeric coupling; each U-shape structure being coupled to a respective radial projection of the hub by a further elastomeric coupling.
Inventors
- 👤 Vittorio Caramaschi
- 👤 Pier Luigi Castelli
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 23:02
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32; B64C27/322; B64C27/35
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
169 words
A helicopter rotor comprising: a central hub rotatable about its axis; a plurality of blades connected to and extending in a substantially radial direction outward form the hub, each blade having associated therewith: an attachment element (34) coupled to the blade and extending through an axial aperture (22) of the hub; a first elastomeric coupling adapted to provide cooperation between the attachment element (34) and an inner surface of a peripheral bridge element (23) of the hub; the peripheral bridge element (23) which closes the radially outward part of the aperture (22); the aperture (22) located radially outward of a central support structure (12) of the hub wherein a radial projection (45) extends into the aperture and towards the bridge element (23), and the projection (45) further extends through a radial hole (33) formed in the attachment element (34), the projection (45) being connected to the hole (33) in an axially slideable manner, a second elastomeric coupling (41) being disposed between the projection (45) and the radial hole (33).
Claim 2
Dependent Claim
169 words
A helicopter rotor comprising: a central hub rotatable about its axis; a plurality of blades connected to and extending in a substantially radial direction outward form the hub, each blade having associated therewith: an attachment element (34) coupled to the blade and extending through an axial aperture (22) of the hub; a first elastomeric coupling adapted to provide cooperation between the attachment element (34) and an inner surface of a peripheral bridge element (23) of the hub; the peripheral bridge element (23) which closes the radially outward part of the aperture (22); the aperture (22) located radially outward of a central support structure (12) of the hub wherein a radial projection (45) extends into the aperture and towards the bridge element (23), and the projection (45) further extends through a radial hole (33) formed in the attachment element (34), the projection (45) being connected to the hole (33) in an axially slideable manner, a second elastomeric coupling (41) being disposed between the projection (45) and the radial hole (33).
Claim 3
Dependent Claim
89 words
A rotor according to claim 1, characterised by the fact that each said attachment element (34) includes two plates (35, 36) extending in a substantially radial direction from the said hub (2) and disposed one above and the other below the associated said bridge element (23), and an element (32) substantially parallel to the said axis (4) and extending through the associated said aperture (22) to join together the inner ends of the said two plates (35,36); the said hole (33) being formed through the said connection element (32).
Claim 4
Dependent Claim
45 words
A rotor according to claim 1, characterised by the fact that each said second, elastomeric coupling includes a knee-joint (42) of elastomeric material housed within the associated said hole (33) and coupled to the associated said projection (45) by means of a splined coupling (43-44).
Claim 5
Dependent Claim
44 words
A rotor according to claim 3, characterised by the fact that each said knee (42) is housed within a tubular projection (40) lodged within the associated hole (33) and rigidly connected to an inner shoe (28) of the associated said first elastomeric coupling (27).
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-05-13 | 1988-11-12 | 1989-05-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-05-13 | 1992-11-12 | 1993-05-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-05-13 | 1996-11-12 | 1997-05-14 | $7700.00 | Window Closed / Lapsed |