DE2150761C3 - Rotoranordnung für Drehflügelflugzeuge - Google Patents
Rotoranordnung für DrehflügelflugzeugeInfo
- Publication number
- DE2150761C3 DE2150761C3 DE19712150761 DE2150761A DE2150761C3 DE 2150761 C3 DE2150761 C3 DE 2150761C3 DE 19712150761 DE19712150761 DE 19712150761 DE 2150761 A DE2150761 A DE 2150761A DE 2150761 C3 DE2150761 C3 DE 2150761C3
- Authority
- DE
- Germany
- Prior art keywords
- blade
- rotor
- plane
- angle adjustment
- flapping
- 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
- 235000014676 Phragmites communis Nutrition 0.000 claims 1
- 241000446313 Lamella Species 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 241000239290 Araneae Species 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000035559 beat frequency Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 230000004043 responsiveness Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/33—Rotors having flexing arms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
- Wind Motors (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4900670 | 1970-10-15 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| DE2150761A1 DE2150761A1 (de) | 1972-06-15 |
| DE2150761B2 DE2150761B2 (de) | 1976-03-11 |
| DE2150761C3 true DE2150761C3 (de) | 1985-05-15 |
Family
ID=10450776
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19712150761 Expired DE2150761C3 (de) | 1970-10-15 | 1971-10-12 | Rotoranordnung für Drehflügelflugzeuge |
Country Status (5)
| Country | Link |
|---|---|
| CA (1) | CA952888A (enExample) |
| DE (1) | DE2150761C3 (enExample) |
| FR (1) | FR2110441B1 (enExample) |
| GB (1) | GB1310035A (enExample) |
| IT (1) | IT939542B (enExample) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1535391A (en) * | 1976-05-11 | 1978-12-13 | Westland Aircraft Ltd | Helicopter rotors |
| GB1534404A (en) * | 1976-07-15 | 1978-12-06 | Westland Aircraft Ltd | Helicopter rotors |
| DE102006042575A1 (de) * | 2006-09-11 | 2008-03-27 | Matthias Rupprecht | Rotorkopfeinheit |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2949967A (en) * | 1959-05-25 | 1960-08-23 | Hughes Tool Co | Blade-to-hub connector for thrust producing rotor |
| US3026942A (en) * | 1959-07-07 | 1962-03-27 | Bell Helicopter Corp | Helicopter rotor system |
| US3384185A (en) * | 1967-06-02 | 1968-05-21 | Aerojet General Co | Rotor hubs |
| US3926536A (en) * | 1970-10-15 | 1975-12-16 | Westland Aircraft Ltd | Semi-rigid rotor systems for rotary wing aircraft |
-
1970
- 1970-10-15 GB GB1310035D patent/GB1310035A/en not_active Expired
-
1971
- 1971-10-11 IT IT5340371A patent/IT939542B/it active
- 1971-10-12 DE DE19712150761 patent/DE2150761C3/de not_active Expired
- 1971-10-13 CA CA125,038A patent/CA952888A/en not_active Expired
- 1971-10-14 FR FR7136898A patent/FR2110441B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR2110441B1 (enExample) | 1976-02-13 |
| DE2150761B2 (de) | 1976-03-11 |
| DE2150761A1 (de) | 1972-06-15 |
| IT939542B (it) | 1973-02-10 |
| GB1310035A (en) | 1973-03-14 |
| FR2110441A1 (enExample) | 1972-06-02 |
| CA952888A (en) | 1974-08-13 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8281 | Inventor (new situation) |
Free format text: CIASTULA, TADEUSZ LEOPOLD ROGERS, VICTOR ALFRED BADEN BALMFORD, DAVID ERNEST HALL, YEOVIL, SOMERSET, GB |
|
| C3 | Grant after two publication steps (3rd publication) | ||
| 8339 | Ceased/non-payment of the annual fee |