GB1367197A - Advanced geometry main rotor blade - Google Patents
Advanced geometry main rotor bladeInfo
- Publication number
- GB1367197A GB1367197A GB2311872A GB2311872A GB1367197A GB 1367197 A GB1367197 A GB 1367197A GB 2311872 A GB2311872 A GB 2311872A GB 2311872 A GB2311872 A GB 2311872A GB 1367197 A GB1367197 A GB 1367197A
- Authority
- GB
- United Kingdom
- Prior art keywords
- root
- tip
- blade
- curve
- decreasing
- 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
- 230000003247 decreasing effect Effects 0.000 abstract 3
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
- 230000007423 decrease Effects 0.000 abstract 1
- 238000009998 heat setting Methods 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US00143970A US3799700A (en) | 1971-05-17 | 1971-05-17 | Main rotor blade construction |
| US00143850A US3829240A (en) | 1971-05-17 | 1971-05-17 | Advanced geometry main rotor blade |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1367197A true GB1367197A (en) | 1974-09-18 |
Family
ID=26841459
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2311872A Expired GB1367197A (en) | 1971-05-17 | 1972-05-17 | Advanced geometry main rotor blade |
Country Status (5)
| Country | Link |
|---|---|
| AU (1) | AU459383B2 (enrdf_load_stackoverflow) |
| DE (1) | DE2223567A1 (enrdf_load_stackoverflow) |
| FR (1) | FR2137921B1 (enrdf_load_stackoverflow) |
| GB (1) | GB1367197A (enrdf_load_stackoverflow) |
| IT (1) | IT957890B (enrdf_load_stackoverflow) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2363774A (en) * | 2000-06-09 | 2002-01-09 | Cartercopters Llc | Aircraft rotor aerofoil suitable for forward and reverse flow |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4275994A (en) * | 1978-04-03 | 1981-06-30 | Textron, Inc. | Roll formed blade structure |
| DE3310937C2 (de) * | 1982-10-09 | 1984-10-31 | Dornier Gmbh, 7990 Friedrichshafen | Propellerblatt, insbesondere für den Vortrieb von Luftfahrzeugen |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1369600A (fr) * | 1963-07-23 | 1964-08-14 | Electric Auto Lite Co | Hélice, notamment pour avions à décollage et atterrissage verticaux |
-
1972
- 1972-05-08 AU AU42011/72A patent/AU459383B2/en not_active Expired
- 1972-05-15 DE DE19722223567 patent/DE2223567A1/de not_active Withdrawn
- 1972-05-16 FR FR7217394A patent/FR2137921B1/fr not_active Expired
- 1972-05-16 IT IT5027772A patent/IT957890B/it active
- 1972-05-17 GB GB2311872A patent/GB1367197A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2363774A (en) * | 2000-06-09 | 2002-01-09 | Cartercopters Llc | Aircraft rotor aerofoil suitable for forward and reverse flow |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2137921A1 (enrdf_load_stackoverflow) | 1972-12-29 |
| AU459383B2 (en) | 1975-03-27 |
| AU4201172A (en) | 1973-11-15 |
| DE2223567A1 (de) | 1972-12-07 |
| FR2137921B1 (enrdf_load_stackoverflow) | 1976-08-06 |
| IT957890B (it) | 1973-10-20 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1331025A (en) | Helicopter rotor blades | |
| US4459083A (en) | Shapes for rotating airfoils | |
| US4248572A (en) | Helicopter blade | |
| GB1514828A (en) | Tail rotor arrangement for helicopters | |
| ES413589A1 (es) | Perfeccionamientos introducidos en aeronaves. | |
| GB989990A (en) | Propeller blade for vtol aircraft | |
| US5584661A (en) | Forward sweep, low noise rotor blade | |
| GB1391939A (en) | Helicopter rotor blades | |
| ES429779A1 (es) | Perfeccionamientos en dispositivos de ala delgada para ae- ronaves. | |
| GB1328167A (en) | Rotor blade for a gas turbine engine | |
| GB1526433A (en) | Helicopter rotor blades | |
| FR2246444A1 (en) | Aircraft with slow landing speed - wing section is variable between thin and thick in flight | |
| GB1367197A (en) | Advanced geometry main rotor blade | |
| GB1391940A (en) | Helicopter rotor blades | |
| US3902821A (en) | Helicopter rotor | |
| GB1308023A (en) | Bladed rotors | |
| IL44661A (en) | Helicopter blade for high speed forward flight | |
| GB872687A (en) | Improvements relating to propellers | |
| CN209479973U (zh) | 一种横流风扇增升自转旋翼机 | |
| GB546621A (en) | Improvements in or relating to variable-pitch airscrews | |
| GB919776A (en) | Improvements in or relating to rotor blades | |
| US3392788A (en) | Rotor blade | |
| GB832164A (en) | Reversible propeller | |
| GB1047568A (en) | Improvements in or relating to aircraft rotors | |
| Schillings et al. | The Effect of Airframe Aerodynamics on V‐22 Rotor Loads |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |