GB1369596A - Solenoid device - Google Patents

Solenoid device

Info

Publication number
GB1369596A
GB1369596A GB4759870A GB4759870A GB1369596A GB 1369596 A GB1369596 A GB 1369596A GB 4759870 A GB4759870 A GB 4759870A GB 4759870 A GB4759870 A GB 4759870A GB 1369596 A GB1369596 A GB 1369596A
Authority
GB
United Kingdom
Prior art keywords
core
sleeve
port
deflection
block
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
GB4759870A
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.)
National Research Development Corp UK
Original Assignee
National Research Development Corp UK
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 National Research Development Corp UK filed Critical National Research Development Corp UK
Priority to GB4759870A priority Critical patent/GB1369596A/en
Priority to US00186932A priority patent/US3742407A/en
Priority to DE19712150118 priority patent/DE2150118A1/en
Publication of GB1369596A publication Critical patent/GB1369596A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00Magnets
    • H01F7/06Electromagnets; Actuators including electromagnets
    • H01F7/08Electromagnets; Actuators including electromagnets with armatures
    • H01F7/088Electromagnets; Actuators including electromagnets with armatures provided with means for absorbing shocks
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00Magnets
    • H01F7/06Electromagnets; Actuators including electromagnets
    • H01F7/08Electromagnets; Actuators including electromagnets with armatures
    • H01F7/13Electromagnets; Actuators including electromagnets with armatures characterised by pulling-force characteristics
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F7/00Magnets
    • H01F7/06Electromagnets; Actuators including electromagnets
    • H01F7/08Electromagnets; Actuators including electromagnets with armatures
    • H01F7/16Rectilinearly-movable armatures
    • H01F7/1607Armatures entering the winding

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Magnetically Actuated Valves (AREA)

Abstract

1369596 Brake valves, valves NATIONAL RESEARCH DEVELOPMENT CORP 5 Oct 1971 [7 Oct 1970] 47598/70 Headings F2V and F2F [Also in Division H1] A solenoid 6 (Fig. 1) has an axially sliding core 7 with a push-rod 8 sliding within sleeve 10 threaded into housing 1 and cap 12 to carry a metal indenter 14 with coned face engaging a resilient rubber block 15 as the core moves on energization; the block developing a non- linearly variable force with a deflection opposed to the non-linearly variable force developed during the travel of the core, so that the latter assumes a variable position in working range dependent on coil current. This is supplied as rectangular pulses of constant amplitude and mark/space modulation from a shaping circuit 33 controlled by, e.g. a brake pedal 34. The remote end of the core is connected over pushrod 16 to a a valve spool 17 moving within a slidable sleeve 18 of housing 1, travel being limited by the abutment of indenter 13 on sleeve 9 and adjusting screw 19. A diaphragm 28 carried by the sleeve 18 defines chambers to which atmosphere is admitted over 20, 21. As shown the force patterns of core 7 and block 15 are balanced and core and sleeve 7, 9 are in abutment separated by nonmagnetic spacer 31. Port 5 connected to the active side of a brake servo (not shown) is disconnected from port 20 but connected to the vacuum port 4 of the servo so that brakes are not applied, due to the vacuum on both sides of the diaphragm. Deflection of core 7 to the left causes edge 24 of the valve spool 17 to cover port 23 of the outer sleeve 18 to disconnect spaces 2, 3. Further such movement admits air from port 20 to space 3 over 25, 26, 77; destroying pressure equality and applying the brakes. Diaphragm 28 is deflected to the left, and sleeve 18 deflects spring 29 and closes port 27 to disconnect ports 20 and 5; the system then assuming a stable state of brake application dependent on the deflection of core 7, and linearly related to the mark/space ratio of the coil energization. On interruption of the latter the core and spool valve deflect to the right, and spring 29 restores the sleeve 18, so that brakes are released; the restoration being assisted by gravity if the device is mounted vertically. A spiral variable rate spring may replace block 15. Alternatively (Figs. 2, 3, not shown) the solenoid has three coils in series to reduce capacitance, with two indenter members on a centre pivoted bridge carried on the end of the core, which bear on a annular resilient forcetransducer of linear characteristics, the signal from which representing the force thereon and being fed as input to the mark/space shaping circuit together with a control signal; the shaping circuit being programmed to convert the linear transducer signal to a nonlinear signal of flow corresponding to that of the core deflection. The solenoid is then energized by the error between this signal and the control signal. Non- linear resilient blocks may replace the transducer, as before, and the device of Fig. 1 may be combined with a positional feedback system to compensate hysteresis error. The required characteristics of the nonlinear block are described (Fig. 4, not shown).
GB4759870A 1970-10-07 1970-10-07 Solenoid device Expired GB1369596A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB4759870A GB1369596A (en) 1970-10-07 1970-10-07 Solenoid device
US00186932A US3742407A (en) 1970-10-07 1971-10-06 Solenoid device
DE19712150118 DE2150118A1 (en) 1970-10-07 1971-10-07 Solenoid device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4759870A GB1369596A (en) 1970-10-07 1970-10-07 Solenoid device

Publications (1)

Publication Number Publication Date
GB1369596A true GB1369596A (en) 1974-10-09

Family

ID=10445555

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4759870A Expired GB1369596A (en) 1970-10-07 1970-10-07 Solenoid device

Country Status (3)

Country Link
US (1) US3742407A (en)
DE (1) DE2150118A1 (en)
GB (1) GB1369596A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5278119A (en) * 1975-12-24 1977-07-01 Nissan Motor Electromagnetic valve
US5238202A (en) * 1992-04-15 1993-08-24 Intronics, Inc. Yarn tensioning apparatus
US6443422B1 (en) * 2001-06-08 2002-09-03 Eaton Corporation Apparatus and method for adjusting an actuator on a real-time basis
US9852834B2 (en) * 2013-12-31 2017-12-26 Parker-Hannifin Corporation Adjustable center pole

Also Published As

Publication number Publication date
DE2150118A1 (en) 1972-04-13
US3742407A (en) 1973-06-26

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees