GB476852A - Improvements in or relating to variable pitch propellers automatically regulated to constant speed - Google Patents
Improvements in or relating to variable pitch propellers automatically regulated to constant speedInfo
- Publication number
- GB476852A GB476852A GB12890/37A GB1289037A GB476852A GB 476852 A GB476852 A GB 476852A GB 12890/37 A GB12890/37 A GB 12890/37A GB 1289037 A GB1289037 A GB 1289037A GB 476852 A GB476852 A GB 476852A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propeller
- valve
- pump
- oil
- pipe
- 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
-
- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09B—ORGANIC DYES OR CLOSELY-RELATED COMPOUNDS FOR PRODUCING DYES, e.g. PIGMENTS; MORDANTS; LAKES
- C09B39/00—Other azo dyes prepared by diazotising and coupling
-
- 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
- B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
- B64C11/40—Blade pitch-changing mechanisms fluid, e.g. hydraulic automatic
Abstract
476,852. Fluid-pressure servomotorcontrol systems. SIEMENS APPARATE UND MASCHINEN GES. May 5, 1937, No. 12890. Convention date, May 6, 1936. [Class 135] [Also in Group XXXIII] A variable-pitch propeller which is automatically regulated hydraulically to constant speed and including a closed oil circuit containing an oil pump, a regulating valve and an oil motor and with means for connecting these with the blades for varying the angle is characterized by the accommodation of the whole of this apparatus within the hub of the propeller, the oil pump being driven by a wind-mill screw. The blades 11 of the screw propeller are coupled by gearing 6 with an oil motor 5 adapted to be driven by an oil pump 2 which is in turn actuated by a wind-mill screw 3. The pipe connections between the pump and the motor are controlled by a valve 8 disposed in the hub so that on rotation of the propeller centrifugal force tends to move the valve, such tendency being under the constraint of an adjustable spring 19. Under normal conditions, the valve is positioned as shown and no oil passes to the pump 5. With rise or fall of propeller revolutions, the valve moves so as to couple up either the pipe 13 or the pipe 14 to the delivery side of the pump 2, thereby changing the pitch and remaining operative till the propeller revolutions are back to normal. For minimum pitch position a cam or projection 15 on the blade root actuates a bell-crank lever 16 and contacts with a pin 17 so as to move the control piston valve 8 back to the position in Fig. 1.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE476852X | 1936-05-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB476852A true GB476852A (en) | 1937-12-16 |
Family
ID=6542053
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB12890/37A Expired GB476852A (en) | 1936-05-06 | 1937-05-05 | Improvements in or relating to variable pitch propellers automatically regulated to constant speed |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR476852A (en) |
GB (1) | GB476852A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2416516A (en) * | 1939-08-26 | 1947-02-25 | Everel Propeller Corp | Variable pitch propeller |
US2635699A (en) * | 1949-02-21 | 1953-04-21 | United Aircraft Corp | Propeller control means |
DE912418C (en) * | 1939-06-16 | 1954-05-28 | Gen Motors Corp | Self-contained regulator for a propeller with adjustable blades |
US3156301A (en) * | 1962-12-07 | 1964-11-10 | Hartzell Propeller Inc | Variable pitch propeller |
-
1914
- 1914-07-20 FR FR476852D patent/FR476852A/en not_active Expired
-
1937
- 1937-05-05 GB GB12890/37A patent/GB476852A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE912418C (en) * | 1939-06-16 | 1954-05-28 | Gen Motors Corp | Self-contained regulator for a propeller with adjustable blades |
US2416516A (en) * | 1939-08-26 | 1947-02-25 | Everel Propeller Corp | Variable pitch propeller |
US2635699A (en) * | 1949-02-21 | 1953-04-21 | United Aircraft Corp | Propeller control means |
US3156301A (en) * | 1962-12-07 | 1964-11-10 | Hartzell Propeller Inc | Variable pitch propeller |
Also Published As
Publication number | Publication date |
---|---|
FR476852A (en) | 1915-09-07 |
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