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GB511930A - Improvements in and connected with the regulation of super-charged internal combustion engines, particularly aircraft engines - Google Patents

Improvements in and connected with the regulation of super-charged internal combustion engines, particularly aircraft engines

Info

Publication number
GB511930A
GB511930A GB8938/39A GB893839A GB511930A GB 511930 A GB511930 A GB 511930A GB 8938/39 A GB8938/39 A GB 8938/39A GB 893839 A GB893839 A GB 893839A GB 511930 A GB511930 A GB 511930A
Authority
GB
United Kingdom
Prior art keywords
lever
blower
pressure
factor
governor
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
Application number
GB8938/39A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Daimler Benz AG filed Critical Daimler Benz AG
Publication of GB511930A publication Critical patent/GB511930A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D29/00Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2700/00Mechanical control of speed or power of a single cylinder piston engine
    • F02D2700/07Automatic control systems according to one of the preceding groups in combination with control of the mechanism receiving the engine power

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)

Abstract

511,930. Fluid-pressure servomotor-control systems. DAIMLER-BENZ AKT.-GES. March 21. 1939, No. 8938. Convention date, March 24, 1938. [Class 135] [Also in Group XXVII] In supercharged engines, particularly of aircraft, wherein two working factors are positively varied by a manual control, one factor (e.g., changing pressure) being dependent on atmospheric pressure and also upon the other factor (e.g., speed) means are provided whereby, when the atmospheric pressure falls too low to maintain the first factor, the second factor is adjusted so as to restore the first to its desired value. The Figure shows a pilot's control lever 17 connected (a) to a capsule 21 which is subjected to the changing pressure of a blower 12 and controls a throttle 14 in the blower discharge by means of a servomotor 24, 27, and (b) to the sleeve 11 of a centrifugal governor 8 controlling the pitch of the propeller blades 4. Adjustment of the lever 17 from A to D displaces the capsule 21 to increase the blower pressure, and at the same time adjusts the sleeve 11 to increase the load on the governor and thereby the speed. When atmospheric pressure becomes decreased at altitudes, the changing pressure of the blower falls below the prescribed value, and to restore the changing pressure an aneroid 31 is provided which, under such conditions, contracts the toggle linkage 28, 29 so as to increase the speed of the engine and therefore also of the blower. When the lever 17 is in the idling position A, it contacts with a lever 18 connected to an idling throttle 15. At the position B, the lever 18 is prevented from moving farther by a stop 19, the throttle 15 being then fully open. When the lever 17 is moved beyond the fulloutput position D for starting, a further lever 40 is actuated to increase the fuel supply by means of a connection 42, 38 to the fuel pump 16. This pump is also under the control of a piston 36 acted on by the changing pressure. In a modification, the lever 17 is also connected to the aneroid 31 so as to displace it bodily; an adjustable arm may be introduced between the lever 17 and the aneroid. A relay may be provided between the linkage 28, 29 and the governor. Also cams may be provided between the control lever 17 and the connections to the blower and governor controls, so as to vary the relative adjustments of each.
GB8938/39A 1938-03-24 1939-03-21 Improvements in and connected with the regulation of super-charged internal combustion engines, particularly aircraft engines Expired GB511930A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE511930X 1938-03-24

Publications (1)

Publication Number Publication Date
GB511930A true GB511930A (en) 1939-08-25

Family

ID=6547971

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8938/39A Expired GB511930A (en) 1938-03-24 1939-03-21 Improvements in and connected with the regulation of super-charged internal combustion engines, particularly aircraft engines

Country Status (1)

Country Link
GB (1) GB511930A (en)

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