GB575663A - Improvements in or relating to variable-pitch propellers for aircraft and blowers - Google Patents
Improvements in or relating to variable-pitch propellers for aircraft and blowersInfo
- Publication number
- GB575663A GB575663A GB5882/44A GB588244A GB575663A GB 575663 A GB575663 A GB 575663A GB 5882/44 A GB5882/44 A GB 5882/44A GB 588244 A GB588244 A GB 588244A GB 575663 A GB575663 A GB 575663A
- Authority
- GB
- United Kingdom
- Prior art keywords
- main blade
- auxiliary flap
- aircraft
- blowers
- march
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D7/00—Rotors with blades adjustable in operation; Control thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/32—Blade pitch-changing mechanisms mechanical
- B64C11/34—Blade pitch-changing mechanisms mechanical automatic
- B64C11/343—Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
575,663. Propellers and impellers. ESCHER WYSS MASCHINENFABRIKEN AKT.-GES. March 30, 1944, No. 5882. Convention date, March 31, 1943. [Class 114] In a variable pitch propeller for aircraft or impeller for axial blowers, an auxiliary flap 3 is adjusted automatically on adjustment of the main blade 2 so that, for large and small pitch angles of the main blade, the auxiliary flap is, respectively, close to, and spaced away from, the hub end of the main blade. A lateral arm 5 on the main blade projects into a rectangular slot 4 in the auxiliary flap and its concave lower surface 11 engages a ball-bearing 10. An extension 6 of the auxiliary flap carries a roller 9 which engages a guide race 7 in an annular body 8 on the propeller or impeller hub 1.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH575663X | 1943-03-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB575663A true GB575663A (en) | 1946-02-27 |
Family
ID=4521180
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5882/44A Expired GB575663A (en) | 1943-03-31 | 1944-03-30 | Improvements in or relating to variable-pitch propellers for aircraft and blowers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB575663A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2746604A1 (en) * | 2012-12-21 | 2014-06-25 | SKF Aerospace France | Rolling bearing intended to undergo a surface fatigue phenomenon |
-
1944
- 1944-03-30 GB GB5882/44A patent/GB575663A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2746604A1 (en) * | 2012-12-21 | 2014-06-25 | SKF Aerospace France | Rolling bearing intended to undergo a surface fatigue phenomenon |
FR3000148A1 (en) * | 2012-12-21 | 2014-06-27 | Skf Aerospace France | BEARING FOR A SURFACE FATIGUE PHENOMENON |
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