US4547127A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Wing mounting for a rotary wing aircraft
Assignee: Airbus Helicopters Deutschland GmbH
•
Filing: 1983-10-24
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Granted: 1985-10-15
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Expires: 2003-10-24
Abstract
Abstract A flexible blade neck of a helicopter rotor blade is bridged by a torsion gid sleeve for the blade angle adjustments. The radially outer end of the blade neck and sleeve are rigidly connected to the wing section of the blade. The radially inner end of the blade neck forms a blade root which is secure to the rotor head or hub. Additionally, the radially inner ends of the blade root and of the sleeve are interconnected by a ball and socket arrangement permitting a universal movement between the sleeve and the blade neck, thereby decoupling sleeve movements from the blade neck and vice versa.
Inventors
- 👤 Hubert Frommlet
- 👤 Michael Hahn
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 17:04
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32; B64C27/33; B64C27/46; B64C27/473; B64C27/48
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
224 words
A wing mounting for a rotary wing aircraft, comprising a rotor head including a rotor and a number of blades secured to said rotor head, each blade having a longitudinal blade axis extending substantially radially relative to said rotor head, each blade including a radially outer wing section, a radially intermediate torsion yielding neck section, a radially inner blade root section having a recess (5) therein, and a sleeve bridging said neck section for blade angle adjustments, said sleeve being rigidly connected with its radially outer end to a radially inner end of said wing section, means operatively connecting said blade root section to said rotor head, and pivot means operatively located in said recess (5) for universally joining a radially inner end of said sleeve to a radially inner end of said blade root section, said pivot means comprising socket means, ball means operatively held in said socket means, and means operatively mounting said ball and socket means between said radially inner end of said sleeve and said blade root section, said mounting means including a stud having a longitudinal stud axis substantially coinciding with said longitudinal blade axis, said ball means being arranged for axially sliding on said stud reaching into said socket means for permitting a universal movement between said radially inner end of said sleeve and said blade root section.
Claim 2
Dependent Claim
224 words
A wing mounting for a rotary wing aircraft, comprising a rotor head including a rotor and a number of blades secured to said rotor head, each blade having a longitudinal blade axis extending substantially radially relative to said rotor head, each blade including a radially outer wing section, a radially intermediate torsion yielding neck section, a radially inner blade root section having a recess (5) therein, and a sleeve bridging said neck section for blade angle adjustments, said sleeve being rigidly connected with its radially outer end to a radially inner end of said wing section, means operatively connecting said blade root section to said rotor head, and pivot means operatively located in said recess (5) for universally joining a radially inner end of said sleeve to a radially inner end of said blade root section, said pivot means comprising socket means, ball means operatively held in said socket means, and means operatively mounting said ball and socket means between said radially inner end of said sleeve and said blade root section, said mounting means including a stud having a longitudinal stud axis substantially coinciding with said longitudinal blade axis, said ball means being arranged for axially sliding on said stud reaching into said socket means for permitting a universal movement between said radially inner end of said sleeve and said blade root section.
Claim 3
Dependent Claim
74 words
The mounting of claim 1, wherein said stud is rigidly secured to said radially inner end of said blade root section, and wherein said mounting means further include bracket means rigidly secured at one end thereof to said radially inner end of said sleeve and holding at the other end thereof said socket means in which said ball means are operatively received for said axial sliding on said stud to permit said universal movement.
Claim 4
Dependent Claim
36 words
The mounting of claim 2, wherein said mounting means further comprise a forked bracket having secured thereto said stud, and means rigidly securing said forked bracket to said radially inner end of said blade root section.
Claim 5
Dependent Claim
29 words
The mounting of claim 1, wherein said blade root section is divided into two mounting arms, said recess being formed between said mounting arms of said blade root section.
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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) | 1988-10-14 | 1989-04-15 | 1989-10-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-10-14 | 1993-04-15 | 1993-10-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-10-14 | 1997-04-15 | 1997-10-15 | $7700.00 | Window Closed / Lapsed |