GB752080A - Improvements in or relating to rotor blades for helicopters - Google Patents
Improvements in or relating to rotor blades for helicoptersInfo
- Publication number
- GB752080A GB752080A GB18158/53A GB1815853A GB752080A GB 752080 A GB752080 A GB 752080A GB 18158/53 A GB18158/53 A GB 18158/53A GB 1815853 A GB1815853 A GB 1815853A GB 752080 A GB752080 A GB 752080A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plate
- tip
- helicopters
- rotor blades
- relating
- 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
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/467—Aerodynamic features
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cleaning Of Streets, Tracks, Or Beaches (AREA)
- Toys (AREA)
- Food-Manufacturing Devices (AREA)
Abstract
752,080. Rotor blades for helicopters. WARTO, A. June 30. 1953 [July 18, 1952], No. 18158/53. Class 4. A helicopter rotor blade which has the planform profile shown in Fig. 1, comprises, as shown in sectional view, Fig. 4, a top-plate 1 connected adjacent the leading edge 5 by a middle plate 3 to a lower plate 2. The upper and middle plates 1, 3 include an obtuse angle at a point one-third of the length of the blade from the tip 9, the size of the angle gradually increasing in both directions from said point towards the tip and the root. The plate 1 is provided adjacent the tip with a portion 14 of reduced thickness formed by cutting away part of the underside of the plate.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BR752080X | 1952-07-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB752080A true GB752080A (en) | 1956-07-04 |
Family
ID=3997439
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18158/53A Expired GB752080A (en) | 1952-07-18 | 1953-06-30 | Improvements in or relating to rotor blades for helicopters |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB752080A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10316098A (en) * | 1997-05-15 | 1998-12-02 | Fuji Heavy Ind Ltd | Rotor blade of rotary-wing aircraft |
WO2017145563A1 (en) * | 2016-02-23 | 2017-08-31 | 国立研究開発法人宇宙航空研究開発機構 | Rotor blade, drone, and helicopter |
-
1953
- 1953-06-30 GB GB18158/53A patent/GB752080A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10316098A (en) * | 1997-05-15 | 1998-12-02 | Fuji Heavy Ind Ltd | Rotor blade of rotary-wing aircraft |
WO2017145563A1 (en) * | 2016-02-23 | 2017-08-31 | 国立研究開発法人宇宙航空研究開発機構 | Rotor blade, drone, and helicopter |
WO2017146028A1 (en) * | 2016-02-23 | 2017-08-31 | 国立研究開発法人宇宙航空研究開発機構 | Rotor blade, drone, and helicopter |
JPWO2017146028A1 (en) * | 2016-02-23 | 2018-12-13 | 国立研究開発法人宇宙航空研究開発機構 | Rotor blades, drones and helicopters |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB772532A (en) | Improvements in razor blades for use in safety razors | |
GB752080A (en) | Improvements in or relating to rotor blades for helicopters | |
GB1174955A (en) | Rotatable Aerofoil Assembly | |
GB1033759A (en) | Aerofoil-shaped blade | |
GB662110A (en) | Improvements in aircraft propeller and rotor blades | |
GB488942A (en) | Improvements in or connected with aerofoil surfaces for aircraft | |
GB550713A (en) | Improvements in or relating to aerofoils | |
GB706296A (en) | An improved cutting blade and cutting implement | |
GB548338A (en) | Improvements in or relating to airscrews | |
CA466336A (en) | Means for controlling the pitch of the blades of a helicopter rotor | |
GB543782A (en) | Improvements in or relating to safety razors | |
GB485041A (en) | Improvements in and relating to screw fans | |
GB673223A (en) | Improved blade for rotary hoes | |
GB551556A (en) | Improvements in or relating to metal airscrews | |
GB645289A (en) | Improvements in and relating to surgical operating appliances particularly for cutting thin layers of skin or corns | |
GB492013A (en) | Improvements relating to rotors for rotating wing aircraft | |
GB606305A (en) | Improvements in or relating to rotary wing aircraft | |
GB702632A (en) | Improvements in or relating to cutters for silage and other compacted materials | |
GB356602A (en) | Improvements in machines for cutting sugar cane and the like | |
GB731573A (en) | Blade particularly suitable for aircraft and manufacture thereof | |
GB792258A (en) | Improved hollow propeller blade | |
GB522308A (en) | Improvements in and relating to screw propellers | |
GB604404A (en) | Improvements in and relating to variable pitch propeller blades | |
GB668039A (en) | Improvements in or relating to screw propellers | |
GB1094265A (en) | Improvements in and relating to propeller blades |