GB592458A - Variable pitch aircraft propeller - Google Patents

Variable pitch aircraft propeller

Info

Publication number
GB592458A
GB592458A GB11042/45A GB1104245A GB592458A GB 592458 A GB592458 A GB 592458A GB 11042/45 A GB11042/45 A GB 11042/45A GB 1104245 A GB1104245 A GB 1104245A GB 592458 A GB592458 A GB 592458A
Authority
GB
United Kingdom
Prior art keywords
cylinder
spring
speed
port
pitch
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
GB11042/45A
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.)
Engineering & Res Corp
ENGINEERING AND RESEARCH Corp
Original Assignee
Engineering & Res Corp
ENGINEERING AND RESEARCH Corp
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 Engineering & Res Corp, ENGINEERING AND RESEARCH Corp filed Critical Engineering & Res Corp
Publication of GB592458A publication Critical patent/GB592458A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/32Blade pitch-changing mechanisms mechanical
    • B64C11/34Blade pitch-changing mechanisms mechanical automatic
    • B64C11/343Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on the blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)

Abstract

592,458. Variable - pitch propellers. ENGINEERING & RESEARCH CORPORATION. May 1, 1945, No. 11042. Convention date, June 1, 1944. [Class 114] In a constant-speed, variable-pitch propellermechanism for aircraft in which propeller blades 16 are journalled in a hub 4 and rotated by axial movement, of a cylinder 20, the cylinder being actuated by pressure fluid under control of a valve 56 adjusted by the opposing forces of a spring 110 and a centrifugal governor 102, the force exerted by one member, e.g. the spring 110, is varied when the speed of the propeller attains a predetermined figure and the speed maintained thereafter at a different predetermined figure. Fig.. 1 shows the idling position with the cylinder 20 at its extreme right-hand position, the blades 16 set for minimum pitch and the valve 56 held at its extreme left position by the spring 110. A stationary piston 22 divides the cylinder 20 into two compartments. Lubricating oil &c. from a pressure chamber 28 in the crank-shaft 2, to which the hub 4 is secured, communicates through a passage 80, a port 82 in the piston 22, an annular space surrounding a reduced part of the valve 56 and a port 86 with the righthand chamber of the cylinder 20 to maintain the minimum pitch. On acceleration, the governor 102 displaces the valve 56 to the right and a land 64 thereon blocks the port 82. Further acceleration moves the land past the port permitting pressure fluid to enter the lefthand compartment of the cylinder 20 and displace the cylinder to the left, increasing the blade pitch. The resulting decrease in speed permits the spring 110 to move the land 64 to close the port 82. At its end remote from the governor 102, the spring 110 abuts against a flanged sleeve 156, Fig. 3, slidable on a second flanged sleeve 152 which is screwed on a tube 24 itself mounted in the hub 4 coaxially with the crank-shaft 2. At low speeds, the sleeves are held apart by balls 160 retained between a V-shaped groove formed by bevelling the edges of the flanges and a cylindrical member 120 secured to the cylinder 20. With increasing speed, the balls 160 move inwards along the inside of the member 120 and at a predetermined speed enter a groove in the member which partially frees them from the V-shaped groove permitting the spring to slide the first sleeve 156 into contact with the screwed sleeve 152 to increase the effective length of the spring, reduce the force with which it opposes the governor 102 and adjust the mechanism for a higher running speed. Successively deeper grooves may provide additional selected'speeds. To avoid excessive pitch change in any selected range, movement of the cylinder 20 is limited by stops 127, 124 on a sleeve 122, which are engaged by a flange 126 on the cylindrical member 120.
GB11042/45A 1944-06-01 1945-05-01 Variable pitch aircraft propeller Expired GB592458A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US592458XA 1944-06-01 1944-06-01

Publications (1)

Publication Number Publication Date
GB592458A true GB592458A (en) 1947-09-18

Family

ID=22021742

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11042/45A Expired GB592458A (en) 1944-06-01 1945-05-01 Variable pitch aircraft propeller

Country Status (1)

Country Link
GB (1) GB592458A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112498640A (en) * 2020-11-20 2021-03-16 惠阳航空螺旋桨有限责任公司 Oil distribution device for lubricating oil pipe for propeller

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112498640A (en) * 2020-11-20 2021-03-16 惠阳航空螺旋桨有限责任公司 Oil distribution device for lubricating oil pipe for propeller

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