US4650534A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Helicopter blade longitudinal member and relative manufacturing method
Assignee: AUGUSTA SPA CASCINA COSTA DI SAMARATE (VARESE)
•
Filing: 1984-10-16
•
Granted: 1987-03-17
•
Expires: 2004-10-16
Abstract
Abstract There is disclosed a longitudinal member for a helicopter blade made by placing inside an open mold an open outer covering on which covering and in contact with are arranged a number of uncured axial straps which define top and bottom backs of the longitudinal member itself; the straps being compacted, prior to closure of the mold, against a center core and a front nose by inserting a rear element made of prehardened synthetic composite material, the rear element having an essentially C-shaped section and the opposite side edges of the outer covering being folded thereover prior to closure of the mold.
Inventors
- 👤 Fiorenzo Mussi
- 👤 Emilio Pariani
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 17:50
CPC Classifications
B; B29; B29D; B29D99/00; B29D99/0025; B29D99/0028; B64; B64C; B64C27/00; B64C27/32; B64C27/46; B64C27/473; B29C; B29C33/00; B29C33/44; B64C2027/4733; B64C2027/4736
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
227 words
Method for manufacturing a longitudinal member (1) for a helicopter blade, the method being characterized by the fact that it comprises the steps of opening a curing mold (21) having an inner shape which matches the outer shape of the longitudinal member being formed; lining a portion of said mold with a portion of a number of cloth strips (7) made of uncured synthetic composite material to form an outer covering (6) for said longitudinal member; placing a nose (10), made of uncured synthetic composite material, on said cloth strips; laying a number of axial straps (17), made of uncured synthetic composite material, on said outer covering (6) and on opposite sides of a removal core (25) disposed in said mold and covered with a strip (5) to provide an inner core (4) for said longitudinal member and form top (15) and bottom (16) backs for said intermediate body (9); inserting into said mold a rear element (18), made of prehardened synthetic composite material and having a C-shaped section, and contacting the covered core (25) and laterally contacting said straps (17) therewith; applying pressure on said straps (17) against said nose (10) and said outer covering (6) and inner cover (4); folding the side edges of said outer strips (7) and overlapping the same with each other and with said rear element (18); and closing said mold.
Claim 2
Dependent Claim
227 words
Method for manufacturing a longitudinal member (1) for a helicopter blade, the method being characterized by the fact that it comprises the steps of opening a curing mold (21) having an inner shape which matches the outer shape of the longitudinal member being formed; lining a portion of said mold with a portion of a number of cloth strips (7) made of uncured synthetic composite material to form an outer covering (6) for said longitudinal member; placing a nose (10), made of uncured synthetic composite material, on said cloth strips; laying a number of axial straps (17), made of uncured synthetic composite material, on said outer covering (6) and on opposite sides of a removal core (25) disposed in said mold and covered with a strip (5) to provide an inner core (4) for said longitudinal member and form top (15) and bottom (16) backs for said intermediate body (9); inserting into said mold a rear element (18), made of prehardened synthetic composite material and having a C-shaped section, and contacting the covered core (25) and laterally contacting said straps (17) therewith; applying pressure on said straps (17) against said nose (10) and said outer covering (6) and inner cover (4); folding the side edges of said outer strips (7) and overlapping the same with each other and with said rear element (18); and closing said mold.
Claim 3
Dependent Claim
18 words
Method according to claim 1, characterized by the fact that said rear element (18) is prehardened by compacting.
Claim 4
Dependent Claim
18 words
Method according to claim 1, characterized by the fact that said rear element (18) is prehardened by curing.
Claim 5
Dependent Claim
25 words
Method according to claim 1, characterized by the fact that it includes a hot-curing stage for curing the uncured synthetic composite materials inside the mold.
Claim 6
Dependent Claim
29 words
Method according to claim 4, characterized by the fact that the core (25) comprises an elastomer bag (27) at least partly filled with material (28) which shrinks when heated.
Claim 7
Dependent Claim
15 words
Method according to claim 1, characterized by the fact that the nose (10) is prehardned.
References Cited (Backward Citations)
US3754840A
Cited
US3873654A
Cited
US3967996A
Cited
US4298417A
Cited
US4188171A
Cited
US4299540A
Cited
US4247348A
Cited
US4379013A
Cited
US4470862A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-03-16 | 1990-09-15 | 1991-03-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-16 | 1994-09-15 | 1995-03-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-16 | 1998-09-15 | 1999-03-17 | $7700.00 | Window Closed / Lapsed |