GB912759A - Thrust applying mechanism - Google Patents

Thrust applying mechanism

Info

Publication number
GB912759A
GB912759A GB3634559A GB3634559A GB912759A GB 912759 A GB912759 A GB 912759A GB 3634559 A GB3634559 A GB 3634559A GB 3634559 A GB3634559 A GB 3634559A GB 912759 A GB912759 A GB 912759A
Authority
GB
United Kingdom
Prior art keywords
nut
screw
valve
rotation
coupling
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
GB3634559A
Inventor
Edward Blackwell Leach
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.)
Audco Ltd
Original Assignee
Audco Ltd
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 Audco Ltd filed Critical Audco Ltd
Priority to GB3634559A priority Critical patent/GB912759A/en
Publication of GB912759A publication Critical patent/GB912759A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H35/00Gearings or mechanisms with other special functional features
    • F16H35/10Arrangements or devices for absorbing overload or preventing damage by overload
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00Actuating devices; Operating means; Releasing devices
    • F16K31/12Actuating devices; Operating means; Releasing devices actuated by fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H2025/2062Arrangements for driving the actuator
    • F16H2025/2084Perpendicular arrangement of drive motor to screw axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H2025/2062Arrangements for driving the actuator
    • F16H2025/209Arrangements for driving the actuator using worm gears

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Reciprocating Pumps (AREA)

Abstract

912,759. Screw-and-nut gearing; step-bystep mechanisms. AUDCO Ltd. Oct. 14, 1960 [Oct. 27, 1959], No. 36345/59. Class 80 (3). [Also in Group XXIX] In a pneumatic or hydraulic system for imparting, automatically according to load, either a continuous or a step-by-step axial movement to a non-rotatable screw 12 operating a gate valve (not shown), the screw is moved either by rotation of a nut 14 coupled to gears 15, 18 driven through a fluid coupling 20, Fig. 3, or, if the load exceeds a predetermined amount, by limited and, if necessary, repeated axial movement of the nut 14 in its housing 17 by means of one or other of two annular pistons 22 engaging the ends of the nut, the axial movements of the nut being followed by rotary return movements and the pistons being actuated by the fluid pressure developed in the coupling 20 when rotation of its output gear 18 is resisted. The nut 14 is slidably keyed in a gear 15 driven by a worm 18, or alternatively by a pinion, on the output shaft of a gear pump coupling 20 having an input shaft 21, driven by hand or by electric motor, and two fluid output conduits 25. The two conduits 25 lead, respectively, to upper and lower valve pairs 24, 29 controlling the respective annular pistons 22. Normally, the valves 24 are so positioned by springs 28 that the two piston chambers 23 are connected through passages 26, 27 to a reservoir so that no force is exerted by the pistons on the nut 14. Rotation of shaft 21 in one or other direction then rotates worm 18 and nut 14 to move the screw 12, the nut reacting against the housing 17. Should rotation of worm 18 in one or other direction be resisted, the coupling 20 develops a pressure in one or other conduit 25 which shifts the upper or lower valve 24 so that the corresponding chamber 23 is connected to the pressure conduit 25 and causes joint axial movement of the nut and screw. The axial movement continues either (a) until the resistance is sufficiently diminished for the rotary drive to be effected, in which case the nut is screwed back to its normal position, the pressure in conduit 25 dropping and the valve 24 being returned by its spring 28, or (b) until the piston 22 reaches the end of its permitted stroke, whereupon the valve 29, which has been caused by its spring 30 to follow the piston, connects the pressure conduit 25 to the adjacent end of the valve 24 so that the latter is returned by its spring 28 to re-connect chamber 23 with the reservoir passage 27 and allow nut 14 to be rotated (under no load) back to its normal position. If movement of screw 12 is still resisted the sequence is repeated so that a step-by-step axial movement is imparted to the screw by alternate axial and rotary movements of the nut 14. A valve 32, Fig. 3, ensures that for either direction of rotation of shaft 21 the suction side of coupling 20 is connected to the reservoir by a passage 34. Pressure operated cut-out switches 35, Fig. 2, prevent the pump 20 developing excessive pressures.
GB3634559A 1959-10-27 1959-10-27 Thrust applying mechanism Expired GB912759A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3634559A GB912759A (en) 1959-10-27 1959-10-27 Thrust applying mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3634559A GB912759A (en) 1959-10-27 1959-10-27 Thrust applying mechanism

Publications (1)

Publication Number Publication Date
GB912759A true GB912759A (en) 1962-12-12

Family

ID=10387304

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3634559A Expired GB912759A (en) 1959-10-27 1959-10-27 Thrust applying mechanism

Country Status (1)

Country Link
GB (1) GB912759A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008121451A2 (en) * 2007-02-16 2008-10-09 Parker-Hannifin Corporation Aircraft flight control actuation system with direct acting, force limiting, actuator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008121451A2 (en) * 2007-02-16 2008-10-09 Parker-Hannifin Corporation Aircraft flight control actuation system with direct acting, force limiting, actuator
WO2008121451A3 (en) * 2007-02-16 2009-05-14 Parker Hannifin Corp Aircraft flight control actuation system with direct acting, force limiting, actuator
US8312783B2 (en) 2007-02-16 2012-11-20 Parker-Hannifin Corporation Aircraft flight control actuation system with direct acting, force limiting, actuator

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