CN109671550A - Towed electromagnetic actuator - Google Patents

Towed electromagnetic actuator Download PDF

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Publication number
CN109671550A
CN109671550A CN201811511803.8A CN201811511803A CN109671550A CN 109671550 A CN109671550 A CN 109671550A CN 201811511803 A CN201811511803 A CN 201811511803A CN 109671550 A CN109671550 A CN 109671550A
Authority
CN
China
Prior art keywords
iron core
pull rod
rear end
end cap
armature
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.)
Pending
Application number
CN201811511803.8A
Other languages
Chinese (zh)
Inventor
赵振平
郭子昂
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.)
AVIC Shanghai Aeronautical Measurement Controlling Research Institute
Original Assignee
AVIC Shanghai Aeronautical Measurement Controlling Research Institute
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 AVIC Shanghai Aeronautical Measurement Controlling Research Institute filed Critical AVIC Shanghai Aeronautical Measurement Controlling Research Institute
Priority to CN201811511803.8A priority Critical patent/CN109671550A/en
Publication of CN109671550A publication Critical patent/CN109671550A/en
Pending legal-status Critical Current

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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
    • H01F7/081Magnetic constructions
    • 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
    • H01F7/127Assembling
    • 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

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)

Abstract

The invention discloses a kind of towed electromagnetic actuator, including drive end bearing bracket (1), pull rod (2), armature (3), shell (4), spring (5), rear end cap (6), iron core (7), latch bracket (8), coil blocks (9).Wherein pull rod (2), armature (3) and latch bracket (8) form dynamic iron core, and rear end cap (6) and iron core (7) form static iron core.It when no power, under the effect of spring (5) precompression, is compressed inside the step of pull rod (2) and drive end bearing bracket (1), when energization, under electromagnetic action, armature (3) be bonded with iron core (7), armature (3) drive pull rod (2) movement, to play draw.Executing agency of the present invention has small in size, and light-weight, tractive force is big under equal volume, while the advantages that can adapt to aircraft various complicated flight environment of vehicle.

Description

Towed electromagnetic actuator
Technical field
The present invention relates to electromagnetic conversion field, in particular to a kind of electromagnetic actuator that can generate tractive force.
Background technique
A kind of traction executing agency involved in airplane air dropping goods and materials system needs body due to its special requirement Product is small, and light-weight, tractive force is big under equal volume, while can adapt to the various complicated flight environment of vehicle of aircraft, domestic at present to lack It can satisfy the product of requirements above less.
Summary of the invention
Present invention solves the technical problem that: provide a kind of small in size, light-weight, tractive force is big under equal volume, while energy Enough adapt to the towed electromagnetic actuator of the various complicated flight environment of vehicle of aircraft.
Technical solution of the present invention: a kind of towed electromagnetic actuator, including drive end bearing bracket, pull rod, armature, shell, bullet Spring, rear end cap, iron core, latch bracket, coil block.Wherein pull rod, armature and latch bracket form dynamic iron core, rear end cap and iron core group At static iron core.Iron core is connect with shell, and rear end cap is connect by screw thread with iron core, and coil block is located inside shell cavity, and one End is compressed with iron core, and the other end and drive end bearing bracket compress, and spring is located in rear end cap cavity, and one end is pushed down inside rear end cap, another End resists latch bracket, and latch bracket leads to pull rod to be threadedly coupled, and pull rod and armature interference fit connect, and pull rod passes through in drive end bearing bracket Hole, drive end bearing bracket are connect with shell, and drive end bearing bracket inner face pushes down the coil block other end.When no power, acted in pre-pressure of the spring Under, it is compressed inside the step of pull rod and drive end bearing bracket, when energization, under electromagnetic action, armature is bonded with iron core, armature drive pull rod It is mobile, to play draw.
The characteristics of dynamic iron core is: pull rod, armature and latch bracket form dynamic iron core, and wherein pull rod and armature are matched for interference It closes, pull-rod spring support is to be threadedly coupled.
The characteristics of static iron core is: rear end cap and iron core are connected through a screw thread composition static iron core.
The assembling and setting step of the towed electromagnetic actuator is: step 1 is that pull rod and armature are first carried out interference Cooperation assembly, step 2 are that pull rod screw one end is passed through to iron core mesoporous, and step 3 is that latch bracket is connected through a screw thread assembly Onto pull rod, step 4 is by the component of step 1 to three assembly loaded on inside shell cavity, and step 5 is by iron core and shell It is connected by screw to, step 6 is that coil block is placed in inside shell cavity, and core interior plane, coil are pushed down in an end face Component inner cavity and iron core outer circle cooperate, and step 7 is that the mesoporous of drive end bearing bracket is passed through pull rod, and inner face pushes down the another of coil block One end face, step 8 are that drive end bearing bracket is connect by screw with shell, and step 9 is to place the spring in rear end cap cavity, one end With latch bracket compression, the other end and rear end cap inside are compressed, and step 10 connect for rear end cap is passed through screw thread with iron core, in addition, The precompression of spring can be adjusted by adjusting the position of rear end cap.
Beneficial effects of the present invention: (1) dynamic iron core and static iron core are all fabricated structure, convenient for assembly, debugging, precompression It is adjustable.(2) there is bigger electromagnetic traction power under equal volume, environmental suitability is strong, high reliablity.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the towed electromagnetic actuator of the present invention.
Fig. 2 is dynamic iron core structure schematic diagram.
Fig. 3 is static iron core structural schematic diagram.
Specific embodiment
The invention is further explained in the following combination with the attached drawings of the specification.
As shown in Figure 1, a kind of towed electromagnetic actuator include drive end bearing bracket 1, pull rod 2, armature 3, shell 4, spring 5, Rear end cap 6, iron core 7, latch bracket 8, coil block 9.Wherein pull rod 2, armature 3 and latch bracket 8 form dynamic iron core, 6 He of rear end cap Iron core 7 forms static iron core.Iron core 7 is connect with shell 4, and rear end cap 6 is connect by screw thread with iron core 7, and coil block 9 is located at shell 4 inside cavities, one end and iron core 7 compress, and the other end and drive end bearing bracket 1 compress, and spring 5 is located in 6 cavity of rear end cap, and one end is pushed down Inside rear end cap 6, the other end resists latch bracket 8, and latch bracket 8 leads to pull rod 2 to be threadedly coupled, and pull rod 2 and the interference fit of armature 3 connect It connects, pull rod 2 passes through 1 mesoporous of drive end bearing bracket, and drive end bearing bracket 1 is connect with shell 4, and 1 inner face of drive end bearing bracket pushes down 9 other end of coil block.
As shown in Fig. 2, dynamic iron core is made of pull rod 2, armature 3 and latch bracket 8, wherein pull rod 2 is matched with armature 3 for interference It closes, 2 latch bracket 8 of pull rod is to be threadedly coupled.
As shown in figure 3, static iron core is connected through a screw thread and is formed by rear end cap 6 and iron core 7.
When the mechanism no power, under the effect of 5 precompression of spring, compresses, be powered inside the step and drive end bearing bracket 1 of pull rod 2 When, under electromagnetic action, armature 3 is bonded with iron core 7, and armature 3 drives pull rod 2 mobile, to play draw.

Claims (3)

1. a kind of towed electromagnetic actuator, it is characterized in that: including drive end bearing bracket (1), pull rod (2), armature (3), shell (4), Spring (5), rear end cap (6), iron core (7), latch bracket (8), coil block (9), wherein pull rod (2), armature (3) and latch bracket (8) dynamic iron core is formed, rear end cap (6) and iron core (7) form static iron core;Iron core (7) is connect with shell (4), and rear end cap (6) passes through Screw thread is connect with iron core (7), and coil block (9) is located at shell (4) inside cavity, and coil block (9) one end compresses iron core (7), Spring (5) is located in rear end cap (6) cavity, and rear end cap (6) inside is pushed down in spring (5) one end, and the other end resists latch bracket (8), Latch bracket (8) is connected through a screw thread with pull rod (2), and pull rod (2) and armature (3) interference fit connect, and pull rod (2) passes through drive end bearing bracket (1) mesoporous, drive end bearing bracket (1) are connect with shell (4), and drive end bearing bracket (1) inner face pushes down coil block (9) other end.
2. towed electromagnetic actuator according to claim 1, it is characterized in that, installation step is as follows:
Pull rod (2) and armature (3) are carried out interference fit by step 1;
Pull rod (2) screw thread one end is passed through iron core (7) mesoporous by step 2;
Latch bracket (8) is connected through a screw thread and is assembled on pull rod (2) by step 3;
The component of step 1 to three assembly is loaded on shell (4) inside cavity by step 4;
Iron core (7) and shell (4) are connected by screw to by step 5;
Coil block (9) is placed in shell (4) inside cavity by step 6, and iron core (7) inner plane, coil are pushed down in an end face Component (9) inner cavity and iron core (7) outer circle cooperate;
The mesoporous of drive end bearing bracket (1) is passed through pull rod (2) by step 7, and inner face pushes down another end face of coil block (9);
Step 8, drive end bearing bracket (1) are connect by screw with shell (4);
Spring (5) is placed in rear end cap (6) cavity by step 9, and one end and latch bracket (8) compress, the other end and rear end cap (6) Inside compresses;
Rear end cap (6) are connect by screw thread with iron core (7) by step 10.
3. towed electromagnetic actuator according to claim 1 or 2, it is characterized in that: by adjusting the position of rear end cap (6) It sets to adjust the precompression of spring (5).
CN201811511803.8A 2018-12-11 2018-12-11 Towed electromagnetic actuator Pending CN109671550A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811511803.8A CN109671550A (en) 2018-12-11 2018-12-11 Towed electromagnetic actuator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811511803.8A CN109671550A (en) 2018-12-11 2018-12-11 Towed electromagnetic actuator

Publications (1)

Publication Number Publication Date
CN109671550A true CN109671550A (en) 2019-04-23

Family

ID=66144713

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811511803.8A Pending CN109671550A (en) 2018-12-11 2018-12-11 Towed electromagnetic actuator

Country Status (1)

Country Link
CN (1) CN109671550A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1659321A1 (en) * 2004-11-18 2006-05-24 Eaton Corporation Solenoid operated valve assembly and method of making the same
CN203760244U (en) * 2014-03-12 2014-08-06 朱凤祥 Energy-saving type silicon steel body DC traction electromagnet
CN207690587U (en) * 2017-11-14 2018-08-03 西安庆安电气控制有限责任公司 A kind of towed DC electromagnet that position of output axle is controllable
CN108735420A (en) * 2017-04-17 2018-11-02 苏州耀德科电磁技术有限公司 Direct drive type electromagnet

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1659321A1 (en) * 2004-11-18 2006-05-24 Eaton Corporation Solenoid operated valve assembly and method of making the same
CN203760244U (en) * 2014-03-12 2014-08-06 朱凤祥 Energy-saving type silicon steel body DC traction electromagnet
CN108735420A (en) * 2017-04-17 2018-11-02 苏州耀德科电磁技术有限公司 Direct drive type electromagnet
CN207690587U (en) * 2017-11-14 2018-08-03 西安庆安电气控制有限责任公司 A kind of towed DC electromagnet that position of output axle is controllable

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Application publication date: 20190423