GB460912A - Improvements in and relating to screw propellers for driving air-craft and water-craft - Google Patents
Improvements in and relating to screw propellers for driving air-craft and water-craftInfo
- Publication number
- GB460912A GB460912A GB22311/35A GB2231135A GB460912A GB 460912 A GB460912 A GB 460912A GB 22311/35 A GB22311/35 A GB 22311/35A GB 2231135 A GB2231135 A GB 2231135A GB 460912 A GB460912 A GB 460912A
- Authority
- GB
- United Kingdom
- Prior art keywords
- control
- craft
- governor
- imposed
- throttle
- 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
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/305—Blade pitch-changing mechanisms characterised by being influenced by other control systems, e.g. fuel supply
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
Abstract
460,912. Screw propellers. JUNKERSMOTORENBAU GES. Aug. 7, 1935, No. 22311. Convention date, Aug. 17, 1934. [Class 114] A variable-pitch screw propeller is provided with an automatic pitch adjustment which has an over-riding hand control and this latter is combined with the control of the throttle of the engine driving the propeller. Each screw propeller blade 4 is coupled to a sleeve 15 under the control of a centrifugal governor 13 and spring 14. The over-riding hand control comprises a lever 33 which through linkages adjusts the position of the spring abutment collar 16 on the governor spindle. This linkage includes a floating arm 30 to which also a control rod 34 is linked which sets the throttle 36 of the engine. In a modification the governor operates a valve 45 in an oil pressure circuit controls the move ments of a piston 42 which is linked to the blades 4. In order that excessive movements may not be imposed on the parts the passages 56, 57 from the control valve are broadened at their connection with the cylinder 41 so that when the piston is forced to one end of its stroke it provides a through passage and further motion is not imposed on the rod 40.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE460912X | 1934-08-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB460912A true GB460912A (en) | 1937-02-08 |
Family
ID=6539803
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22311/35A Expired GB460912A (en) | 1934-08-17 | 1935-08-07 | Improvements in and relating to screw propellers for driving air-craft and water-craft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB460912A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE741575C (en) * | 1937-11-30 | 1943-11-12 | Ver Deutsche Metallwerke Ag | Adjustment device for the blade angle of adjustment propellers |
DE742417C (en) * | 1938-11-25 | 1944-02-24 | Messerschmitt Boelkow Blohm | Device to limit the adjustment range of the screw blades on adjustment screws with a hydraulically operated adjustment motor |
DE912418C (en) * | 1939-06-16 | 1954-05-28 | Gen Motors Corp | Self-contained regulator for a propeller with adjustable blades |
WO2002016739A3 (en) * | 2000-08-21 | 2002-06-27 | Bombardier Rotax Gmbh | Turbocharger control system and propeller control system by stepper motor |
US7086230B2 (en) | 2000-08-21 | 2006-08-08 | Brp-Rotax Gmbh & Co. Kg | Pop-off valve for an aircraft engine having a turbocharger control system and propeller control system by stepper motor |
-
1935
- 1935-08-07 GB GB22311/35A patent/GB460912A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE741575C (en) * | 1937-11-30 | 1943-11-12 | Ver Deutsche Metallwerke Ag | Adjustment device for the blade angle of adjustment propellers |
DE742417C (en) * | 1938-11-25 | 1944-02-24 | Messerschmitt Boelkow Blohm | Device to limit the adjustment range of the screw blades on adjustment screws with a hydraulically operated adjustment motor |
DE912418C (en) * | 1939-06-16 | 1954-05-28 | Gen Motors Corp | Self-contained regulator for a propeller with adjustable blades |
WO2002016739A3 (en) * | 2000-08-21 | 2002-06-27 | Bombardier Rotax Gmbh | Turbocharger control system and propeller control system by stepper motor |
US6637202B2 (en) | 2000-08-21 | 2003-10-28 | Bombardier-Rotax Gmbh & Co. Kg | Turbocharger control system and propeller control system by stepper motor |
US6938418B2 (en) | 2000-08-21 | 2005-09-06 | Brp-Rotax Gmbh & Co. Kg | Turbocharger control system and propeller control system by stepper motor |
US7086230B2 (en) | 2000-08-21 | 2006-08-08 | Brp-Rotax Gmbh & Co. Kg | Pop-off valve for an aircraft engine having a turbocharger control system and propeller control system by stepper motor |
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