US4352631A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Hingeless rotor, especially for a helicopter
Assignee: Airbus Helicopters Deutschland GmbH
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Filing: 1980-04-17
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Granted: 1982-10-05
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Expires: 2000-04-17
Abstract
Abstract A connecting element for securing a rotor blade to the rotor hub of a helicopter rotor comprises at least two components arranged at an angle relative to each other. At least one component extends outside the boundary of the other component on both sides of the other component. Slots are arranged in at least one of the components and these slots extend substantially toward the shearing center or rather toward the central shearing axis. Additionally, each connecting element has a flattened zone adjacent to the rotor hub to function as a flapping hinge. The connecting element also functions as a lead-lag hinge and as a torsion hinge.
Inventors
- 👤 Wolfgang Buchs
- 👤 Franz Nowak
- 👤 Rudolf Woerndle
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 17:10
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32; B64C27/33
Claims Analysis
Total Claims: 20
Claim 1
Independent Claim
149 words
A connecting element (4) for securing a rotor blade (2) to a rotor hub (3) without hinging means, especially for a helicopter, comprising a torsion hinge zone (7) including at least two components (10, 11, 12, 13) connected to each other so that the components include an angle and form a common shearing axis (14), said components of said torsion hinge zone (7) being so dimensioned in their respective cross-section that at least one component extends with two sides outside of the other component whereby the other component is substantially enclosed and contacted by said one component, and slot means (15, 16) extending longitudinally through the connecting element at least in one of said two components, said slot means extending substantially radially toward said central shearing axis (14), whereby each connecting element functions as a flapping hinge (5), as a lead-lag hinge (6), and as a torsion hinge (7).
Claim 2
Dependent Claim
149 words
A connecting element (4) for securing a rotor blade (2) to a rotor hub (3) without hinging means, especially for a helicopter, comprising a torsion hinge zone (7) including at least two components (10, 11, 12, 13) connected to each other so that the components include an angle and form a common shearing axis (14), said components of said torsion hinge zone (7) being so dimensioned in their respective cross-section that at least one component extends with two sides outside of the other component whereby the other component is substantially enclosed and contacted by said one component, and slot means (15, 16) extending longitudinally through the connecting element at least in one of said two components, said slot means extending substantially radially toward said central shearing axis (14), whereby each connecting element functions as a flapping hinge (5), as a lead-lag hinge (6), and as a torsion hinge (7).
Claim 3
Dependent Claim
81 words
The connecting element of claim 1, wherein each of said components is made of fiber compound materials, each component comprising at least one shearing web capable of transmitting shearing loads, said shearing web having its fibers arranged in a cross-over relationship so that the fibers are inclined relative to the longitudinal axis of the connecting element, each component further comprising tension transmitting belt means, the fibers of which extend substantially longitudinally in parallel to said longitudinal axis of the connecting element.
Claim 4
Dependent Claim
29 words
The connecting element of claim 1, wherein said angle included by said components of each connecting element is a right angle whereby the components extend perpendicularly to one another.
Claim 5
Dependent Claim
30 words
The connecting element of claim 1, wherein said components form a T-shaped section of the respective connecting element, said T-shaped section including a leg (18) and a cross-bar (11, 12).
Claim 6
Dependent Claim
42 words
The connecting element of claim 6, wherein said common shearing axis (14) forms a main inertia axis, said slot means (15) extending radially toward said main inertia axis, said slot means further extending longitudinally along substantially the entire torsion hinge zone (7).
Claim 7
Dependent Claim
58 words
The connecting element of claim 4 or 5, comprising further slot means (16) extending substantially radially inwardly at the junction of the components forming the T-shaped section and also substantially radially inwardly in the central plane of symmetry of the cross-bar (11, 12) of the T-shaped section and also longitudinally along substantially the entire torsion hinge zone (7).
Claim 8
Dependent Claim
14 words
The connecting element of claim 1, wherein said components form a symmetric cross-shaped section.
Claim 9
Dependent Claim
46 words
The connecting element of claim 7, wherein said common shearing axis (14) forms a main central inertia axis (14), said slot means (15) extending radially toward said main central inertia axis, said slot means (15) further extending longitudinally along substantially the entire torsion hinge zone (7).
Claim 10
Dependent Claim
56 words
The connecting element of claim 7 or 8, comprising further slots means (16) extending radially inwardly at the junction of the components forming the cross-shaped section, said further slot means (16) extending in planes (21) substantially evenly dividing the angle enclosed by two adjacent components and also longitudinally along substantially the entire torsion hinge zone (7).
Claim 11
Dependent Claim
24 words
The connecting element of claim 1, wherein each component comprises shearing web means, said slot means (15) being arranged in said shearing web means.
Claim 12
Dependent Claim
36 words
The connecting element of claim 1, comprising tension transmitting belt means (18, 19) and further slot means (16) in said belt means, said further slot means also extending substantially radially toward said common shearing axis (14).
Claim 13
Dependent Claim
26 words
The connecting element of claim 1, wherein said common shearing axis forms a main inertia axis located in the plane of rotation of the rotor blade.
Claim 14
Dependent Claim
31 words
The connecting element of claim 1, wherein said common shearing axis forms a main inertia axis located in a plane extending perpendicularly to the plane of rotation of the rotor blade.
Claim 15
Dependent Claim
24 words
The connecting element of claim 1, having a main inertia plane extending at an angle to the plane of rotation of the rotor blade.
Claim 16
Dependent Claim
59 words
The connecting element of claim 1, wherein said rotor blade comprises a blade root, said connecting element comprising a radially outer end merging into said blade root, said blade root having a twist therein for applying a biassing torsion load to the blade root whereby the torsion stress level between the blade and the respective connecting element is reduced.
Claim 17
Dependent Claim
158 words
A connecting element (4) for securing a rotor blade (2) to a rotor hub (3) without hinging means, especially for a helicopter, comprising a torsion hinge zone (7) including at least two components (10, 11; 12, 13) connected to each other so that the components include an angle and form a common shearing axis (14), each component comprising shearing load resistant web means (17) for taking up shearing loads and tension load transmitting belt means (18, 19), said shearing load resistant web means being substantially enclosed and contacted by said tension load transmitting belt means (18, 19) except at a radially outer end or edge of each shearing load resistant web means (17), and slot means (15) extending radially in said shearing load resistant web means (17) radially toward said common shearing axis (14), said slot means (15) determining a desired low torsion stiffness of the connecting element without affecting a desired bending stiffness of the connecting element.
Claim 18
Dependent Claim
158 words
A connecting element (4) for securing a rotor blade (2) to a rotor hub (3) without hinging means, especially for a helicopter, comprising a torsion hinge zone (7) including at least two components (10, 11; 12, 13) connected to each other so that the components include an angle and form a common shearing axis (14), each component comprising shearing load resistant web means (17) for taking up shearing loads and tension load transmitting belt means (18, 19), said shearing load resistant web means being substantially enclosed and contacted by said tension load transmitting belt means (18, 19) except at a radially outer end or edge of each shearing load resistant web means (17), and slot means (15) extending radially in said shearing load resistant web means (17) radially toward said common shearing axis (14), said slot means (15) determining a desired low torsion stiffness of the connecting element without affecting a desired bending stiffness of the connecting element.
Claim 19
Dependent Claim
28 words
The connecting element of claim 16, wherein said slot means (15) begin at the radially outer end or edge of the respective shearing load resistant web means (17).
Claim 20
Dependent Claim
32 words
The connecting element of claim 16 or 17, comprising further slot means (16) also extending substantially radially through the tension load transmitting belt means (18, 19) toward said common shearing axis (14).
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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) | 1985-10-04 | 1986-04-05 | 1986-10-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-10-04 | 1990-04-05 | 1990-10-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-10-04 | 1994-04-05 | 1994-10-05 | $7700.00 | Window Closed / Lapsed |