GB1235508A - A rotor blade for a rotor craft - Google Patents
A rotor blade for a rotor craftInfo
- Publication number
- GB1235508A GB1235508A GB4327468A GB4327468A GB1235508A GB 1235508 A GB1235508 A GB 1235508A GB 4327468 A GB4327468 A GB 4327468A GB 4327468 A GB4327468 A GB 4327468A GB 1235508 A GB1235508 A GB 1235508A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- rotor
- lag
- lead
- loops
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/02—Gyroplanes
- B64C27/021—Rotor or rotor head construction
- B64C27/023—Construction of the blades; Coating of the blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,235,508. Helicopter rotor blades. MESSERSCHMITT - BOLKOW - BLOHM G.m.b.H. 11 Sept., 1968 [12 Sept., 1967], No. 43274/68. Heading B7W. In order that the bending forces arising from its lag-lead movement be less than the centrifugal forces acting along its length, a fibre reinforced plastics rotor blade may be provided with two fibre reinforced plastics root end loops 4, 5 lying side-by-side and enclosed by a metal fitting comprising two halves 7, 8. Bolts may pass through the loops lined with bushes 9 to connect the blade to a rotor hub. In a further embodiment which provides for a reduction in forces arising from lag-lead and flapping movement, a blade has a pair of double loops in which one pair is superimposed above the other. In another embodiment, a blade is provided with one loop lying in the lag-lead plane and one loop lying in the flapping plane.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19671531374 DE1531374A1 (en) | 1967-09-12 | 1967-09-12 | Rotor blade made of fiber-reinforced plastic with a loop-like blade root |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1235508A true GB1235508A (en) | 1971-06-16 |
Family
ID=5675484
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4327468A Expired GB1235508A (en) | 1967-09-12 | 1968-09-11 | A rotor blade for a rotor craft |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR1581324A (en) |
GB (1) | GB1235508A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2304090A (en) * | 1995-08-11 | 1997-03-12 | Deutsche Forsch Luft Raumfahrt | Load bearing structure, aircraft wing and wing attachment |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2252916B1 (en) * | 1973-11-30 | 1978-02-24 | Aerospatiale |
-
1968
- 1968-09-11 FR FR1581324D patent/FR1581324A/fr not_active Expired
- 1968-09-11 GB GB4327468A patent/GB1235508A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2304090A (en) * | 1995-08-11 | 1997-03-12 | Deutsche Forsch Luft Raumfahrt | Load bearing structure, aircraft wing and wing attachment |
US5924649A (en) * | 1995-08-11 | 1999-07-20 | Deutsch Forschungsanstalt Fur Luft-Und Raumfahrt E.V. | Aircraft with supporting wings having members for taking up tensile and compressive forces |
GB2304090B (en) * | 1995-08-11 | 2000-02-16 | Deutsche Forsch Luft Raumfahrt | Load-bearing structures such as aircraft wings |
Also Published As
Publication number | Publication date |
---|---|
FR1581324A (en) | 1969-09-12 |
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