GB601913A - Improvements in and relating to sustaining or sustaining and propulsive blades for helicopters - Google Patents
Improvements in and relating to sustaining or sustaining and propulsive blades for helicoptersInfo
- Publication number
- GB601913A GB601913A GB2005345A GB2005345A GB601913A GB 601913 A GB601913 A GB 601913A GB 2005345 A GB2005345 A GB 2005345A GB 2005345 A GB2005345 A GB 2005345A GB 601913 A GB601913 A GB 601913A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sustaining
- blades
- propulsive
- helicopters
- 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
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/16—Drive of rotors by means, e.g. propellers, mounted on rotor blades
- B64C27/18—Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
601,913. Jet propelled airscrew blades. ISACCO, V. Aug. 3, 1945, No. 20053. [Class 4] [Also in Group XXVI] The sustaining and propulsive blades of a helicopter, as described in Specifications 601,911 and 601,912, are equipped with jet propulsion units of their outer extremities. The axis of the unit is traversed to the blade 7 and may be set above or below the blade axis to counteract residual gyroscopic effect. The compressor 155 is driven by the turbine 156 through a direction reversing gear 161.
Publications (1)
Publication Number | Publication Date |
---|---|
GB601913A true GB601913A (en) | 1948-05-14 |
Family
ID=1735186
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2005345A Expired GB601913A (en) | 1945-08-03 | Improvements in and relating to sustaining or sustaining and propulsive blades for helicopters |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB601913A (en) |
-
1945
- 1945-08-03 GB GB2005345A patent/GB601913A/en not_active Expired
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