GB303819A - Sustaining helicopter having oscillating blades - Google Patents
Sustaining helicopter having oscillating bladesInfo
- Publication number
- GB303819A GB303819A GB2427728A GB2427728A GB303819A GB 303819 A GB303819 A GB 303819A GB 2427728 A GB2427728 A GB 2427728A GB 2427728 A GB2427728 A GB 2427728A GB 303819 A GB303819 A GB 303819A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- helicopter
- sustaining
- referred
- shaft
- 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
- B64C27/37—Rotors having articulated joints
- B64C27/41—Rotors having articulated joints with flapping hinge or universal joint, common to the blades
- B64C27/43—Rotors having articulated joints with flapping hinge or universal joint, common to the blades see-saw type, i.e. two-bladed rotor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Abstract
303,819. Oehmichen, E. Oct. 7, 1927. Divided on 302,752. Screw propellers. - Helicopters with blades which oscillate and which have a cyclical changing pitch are provided with an elongated body oscillating and turning with the blades whereby a variable inclination of the latter causes an incidence change in the blades. Blades 1, 1<1> are mounted on a ring 2 carried by a shaft 6 through an intermediate ring 5. Bars 7, 7<1> are in line with the short axles 3, 3<1> and carry heavy weights 8, 8<1>. Reaction springs 9, 9<1> connect the blades with the shaft. The blades are controlled in the plane of 90‹ to the maximum unbalance as referred to in Specification 272,871. Specification 302,752 also is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2427728A GB303819A (en) | 1927-10-07 | 1927-10-07 | Sustaining helicopter having oscillating blades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2427728A GB303819A (en) | 1927-10-07 | 1927-10-07 | Sustaining helicopter having oscillating blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB303819A true GB303819A (en) | 1929-01-07 |
Family
ID=10209179
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2427728A Expired GB303819A (en) | 1927-10-07 | 1927-10-07 | Sustaining helicopter having oscillating blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB303819A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2510006A (en) * | 1946-04-05 | 1950-05-30 | Bell Aircraft Corp | Rotating wing aircraft |
EP1441945A2 (en) * | 2001-11-07 | 2004-08-04 | Rehco, LLC | Propellers, propeller stabilizers, and propeller related vehicles |
-
1927
- 1927-10-07 GB GB2427728A patent/GB303819A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2510006A (en) * | 1946-04-05 | 1950-05-30 | Bell Aircraft Corp | Rotating wing aircraft |
EP1441945A2 (en) * | 2001-11-07 | 2004-08-04 | Rehco, LLC | Propellers, propeller stabilizers, and propeller related vehicles |
EP1441945A4 (en) * | 2001-11-07 | 2005-01-19 | Rehco Llc | Propellers, propeller stabilizers, and propeller related vehicles |
CN1318263C (en) * | 2001-11-07 | 2007-05-30 | 瑞科有限公司 | Propellers, propeller stabilizers, and propeller related vehicles |
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