CN107917809A - Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering - Google Patents

Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering Download PDF

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Publication number
CN107917809A
CN107917809A CN201711369110.5A CN201711369110A CN107917809A CN 107917809 A CN107917809 A CN 107917809A CN 201711369110 A CN201711369110 A CN 201711369110A CN 107917809 A CN107917809 A CN 107917809A
Authority
CN
China
Prior art keywords
fixed seat
resistance test
fluid resistance
hydraulic actuator
test fixture
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
CN201711369110.5A
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Chinese (zh)
Inventor
苏廷江
颜明华
杨晨
李正江
周维维
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.)
AECC Guizhou Liyang Aviation Power Co Ltd
Original Assignee
AECC Guizhou Liyang Aviation Power Co 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 AECC Guizhou Liyang Aviation Power Co Ltd filed Critical AECC Guizhou Liyang Aviation Power Co Ltd
Priority to CN201711369110.5A priority Critical patent/CN107917809A/en
Publication of CN107917809A publication Critical patent/CN107917809A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00Testing of engines
    • G01M15/02Details or accessories of testing apparatus
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M10/00Hydrodynamic testing; Arrangements in or on ship-testing tanks or water tunnels

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

Fluid Resistance Test fixture before being welded the invention discloses a kind of whole welding type hydraulic actuator, including the left bolt (8) and right bolt (12) for being coaxially set and being threadedly coupled respectively with left fixed seat (9) and right fixed seat (11), positioning seat (7) is provided between left fixed seat (9) and right fixed seat (11), positioning seat (7) upper end is connected with fuel inlet fitting (10), and positioning seat is provided with through hole on (7).The present invention can make the physical dimension matching of the part of influence flow by finely tuning finishing part region of interest physical dimension during experiment, it is ensured that flow is not less than 530ml/s before welding, and then ensures that the flow of part postwelding meets the requirement not less than 500ml/s.

Description

Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering
Technical field
The present invention relates to assembling test technical field, more particularly to during a kind of whole welding type hydraulic actuator assembling test Fixture before weldering used in Fluid Resistance Test.
Background technology
Hydraulic actuator is one of significant components in nozzle of aircraft engine tail, its function be stretched by piston, contract come Control the expansion of nozzle, receive, adjust the thrust of engine to a certain extent.Such as figure one is certain h type engine h hydraulic actuation barrel structure Schematic diagram, design document requirement carries out Fluid Resistance Test with fuel oil RP-3 to the E chambers runner of pressurized strut, as outlet pressure PGo out= (0.883~1.08) MPa, pressure difference is Δ P=(0.206~0.265) MPa, when piston is in stretching state, pressurized strut E chamber streams Amount is not less than 500ml/s.
At present, the Fluid Resistance Test in industry for whole welding type pressurized strut carries out after welding fabrication, i.e., Component without Fluid Resistance Test, but uses this Technological Experiment Scheme before welding fabrication, the E chamber flows after components welding It is less than 500ml/s always, is unsatisfactory for design document requirement.Since component belongs to whole welding type structure, stream of the postwelding to component Amount performance can not be adjusted, therefore the concession processing that can only go through the formalities of the overproof component of flow uses, and overproof more scraps.It is comprehensive On, existing assembling test scheme cannot meet whole welding type pressurized strut Fluid Resistance Test requirement.
The content of the invention
The technical problem to be solved in the present invention is:Fluid is carried out before a kind of weldering for whole welding type hydraulic actuator is provided The fixture of resistance test, is conveniently adjusted each position physical dimension of start barrel part, with ensure the flow before components welding be in by Control state, so as to ensure the flow performance after components welding.
To solve the above problems, a kind of fixture of Fluid Resistance Test before whole welding type hydraulic actuator weldering need to be provided, To implement E chamber Fluid Resistance Tests, by finely tuning finishing part region of interest physical dimension (such as double oil-way pipes during experiment The size of the crescent of holder assembly, throttling nozzle aperture, bushing, piston etc.), make the physical dimension matching of the part of influence flow, really Flow is not less than 530ml/s before protecting welding, and then ensures that the flow of part postwelding meets the requirement not less than 500ml/s.
Technical scheme is as follows:
Fluid Resistance Test fixture before a kind of weldering of whole welding type hydraulic actuator, including be coaxially set and respectively with a left side The left bolt and right bolt that fixed seat and right fixed seat are threadedly coupled, positioning seat is provided between left fixed seat and right fixed seat, Positioning seat upper end is connected with fuel inlet fitting, and through hole is provided with positioning seat.
The left fixed seat and right fixed seat are a pair of parallel and with screw hole tablet.
The positioning seat is one piece of L shaped plate parallel with left fixed seat and right fixed seat.
The right fixed seat can be moved along right bolt axis direction.
The left fixed seat and right fixed seat are connected with tailstock system, and tailstock system includes a tabular upper surface, upper end There is a pair of parallel sliding slot in right bolt axis direction on face, have a sliding block above sliding slot, the side of sliding block is provided with a notch.
The through hole is square hole.
The realization principle of the present invention is as follows:
1) design first and make Fluid Resistance Test fixture before a set of weldering, welding flow test fixture is by tailstock system (i.e. clamp body), positioning seat, left and right fixed seat, left and right bolt, fuel inlet fitting composition;
2) by the fixture of design, set at piston rod place to be welded with double oil circuit tube sockets, piston cavity and conduit close Sealing, applies opposite active force by left and right bolt, completes parts fixation positioning, while by opposite active force, make close Sealing deformation reaches sealing function, it is ensured that passage forms and external leakage does not occur;
With existing Fluid Resistance Test Technical comparing, its advantage is mainly reflected in:
1) Fluid Resistance Test is carried out to component before welding using the fixture, by finely tuning finishing part during experiment Region of interest physical dimension (replaces different component combination forms), makes the physical dimension matching of the part of influence flow, really Flow is not less than 530ml/s before protecting welding, and then ensures that the flow of part postwelding meets the requirement not less than 500ml/s;
2) the flow debugging technique before whole welding type pressurized strut welding is broken through, further gropes E chamber runner streams for the later stage Amount debugging, the geometrical factor for finding influence flow and its matching create condition.
Brief description of the drawings
Fig. 1 is whole welding type pressurized strut schematic diagram;
Fig. 2 is M-M schematic cross-sections in Fig. 1;
Fig. 3 is Fluid Resistance Test fixture schematic diagram before welding;
Fig. 4 is the clamping schematic diagram before implementation pressurized strut welding during flow test;
In figure, 1 is double oil circuit tube sockets, and 2 be bushing, and 3 be piston, and 4 be pipe, and 5 be pressurized strut cylinder, and 6 be lid, and 7 are Positioning seat, 8 be left bolt, and 9 be left fixed seat, and 10 be fuel inlet fitting, and 11 be right fixed seat, and 12 be right bolt, and 13 be tailstock system System, 14 be plastic sealing piece, and 15 be caulking gum plug.
Embodiment
Technical scheme is further described below in conjunction with the accompanying drawings, but claimed scope is not limited to institute State.
As shown in figure 3, Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering, including be coaxially set And the left bolt 8 and right bolt 12 being threadedly coupled respectively with left fixed seat 9 and right fixed seat 11, left fixed seat 9 and right fixed seat 11 be a pair of parallel and with screw hole tablet, and left fixed seat 9 and right fixed seat 11 are connected with tailstock system 13, and tailstock system 13 is wrapped A tabular upper surface is included, has a pair of parallel sliding slot in right 12 axis direction of bolt on upper surface, has a pair of of cunning above sliding slot Block, sliding block are positioned on the chute by bolt and nut, and the side of sliding block is provided with a notch, and right 11 lower end both sides of fixed seat are stuck in In notch, so that right fixed seat 11 can be moved along right 12 axis direction of bolt.It is provided between left fixed seat 9 and right fixed seat 11 Positioning seat 7, positioning seat 7 are one piece of L shaped plate parallel with left fixed seat 9 and right fixed seat 11,7 upper end of positioning seat and fuel inlet fitting 10 are connected, and square through hole is provided with positioning seat 7.
Certain type whole welding type pressurized strut schematic diagram as depicted in figs. 1 and 2, including double oil circuit tube sockets 1, bushing 2, piston 3, Pipe 4, pressurized strut cylinder 5, lid 6,3 component of piston are welded with double 1 component of oil circuit tube socket, 3 component of piston and pipes 4, formed E chamber runners, piston 3 move in the cavity of pressurized strut cylinder 5 in a certain range, but cannot decompose.Now set using the present invention Fluid Resistance Test fixture before the welding of meter manufacture, the process of Fluid Resistance Test carries out before being welded to whole welding type pressurized strut Description:
Such as Fig. 4, the cylinder assembly for assembling piston 3 is installed into fixture, is connected at fuel inlet fitting 10 and P, pressurized strut is small In the square through hole of the aspect insertion positioning seat 7 of end four, lateral bolster is by the vertical plane of positioning seat 7;
Plastic sealing piece 14 is assembled on 3 component of piston, double 1 components of oil circuit tube socket are assembled to 3 inner cavity of piston afterwards In, screw left bolt 8 and screw, double 1 components of oil circuit tube socket are deformed with the sealing of 3 place to be welded of piston, realize sealing;
Caulking gum plug 15 is assembled to the corresponding position of piston 3, right bolt 12 is screwed and screws, by caulking gum Plug 15 is assembled in piston head inner cavity, and sealing is realized in the deformation of caulking gum plug 15;
The fixture for being assembled with start cartridge module is connected with exerciser, carries out flow examination;
Part is decomposed, completes experiment.

Claims (6)

  1. A kind of 1. Fluid Resistance Test fixture before whole welding type hydraulic actuator weldering, it is characterised in that:Including being coaxially set And the left bolt (8) and right bolt (12) being threadedly coupled respectively with left fixed seat (9) and right fixed seat (11), left fixed seat (9) Positioning seat (7) is provided between right fixed seat (11), positioning seat (7) upper end is connected with fuel inlet fitting (10), on positioning seat (7) It is provided with through hole.
  2. 2. Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering according to claim 1, its feature It is:The left fixed seat (9) and right fixed seat (11) are a pair of parallel and with screw hole tablet.
  3. 3. Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering according to claim 1, its feature It is:The positioning seat (7) is one piece of L shaped plate parallel with left fixed seat (9) and right fixed seat (11).
  4. 4. Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering according to claim 1, its feature It is:The right fixed seat (11) can move along right bolt (12) axis direction.
  5. 5. Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering according to claim 1, its feature It is:The left fixed seat (9) and right fixed seat (11) are connected with tailstock system (13), and tailstock system (13) includes a tabular Upper surface, has a pair of parallel sliding slot in right bolt (12) axis direction on upper surface, has a sliding block, the side of sliding block above sliding slot Face is provided with a notch.
  6. 6. Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering according to claim 1, its feature It is:The through hole is square hole.
CN201711369110.5A 2017-12-18 2017-12-18 Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering Pending CN107917809A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711369110.5A CN107917809A (en) 2017-12-18 2017-12-18 Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711369110.5A CN107917809A (en) 2017-12-18 2017-12-18 Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering

Publications (1)

Publication Number Publication Date
CN107917809A true CN107917809A (en) 2018-04-17

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CN201711369110.5A Pending CN107917809A (en) 2017-12-18 2017-12-18 Fluid Resistance Test fixture before a kind of whole welding type hydraulic actuator weldering

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CN (1) CN107917809A (en)

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202571742U (en) * 2012-05-23 2012-12-05 广州飞机维修工程有限公司 Installation centering device of airplane pneumatic control valve actuator cylinder
CN103267638A (en) * 2013-05-10 2013-08-28 西安航空动力股份有限公司 Aero-engine elbow nozzle auxiliary oil way pre-welding test clamp
CN104236682A (en) * 2014-09-30 2014-12-24 四川泛华航空仪表电器有限公司 Universal flowmeter vibration test clamp
CN104459189A (en) * 2014-12-05 2015-03-25 四川凌峰航空液压机械有限公司 Actuator cylinder piston rod travel speed measurement device
CN204935428U (en) * 2015-07-03 2016-01-06 贵州红林机械有限公司 Baffle plate assembly tightness test fixture in a kind of aero-engine
CN105927617A (en) * 2016-06-12 2016-09-07 广州飞机维修工程有限公司 General test platform for large hydraulic actuator cylinder of airplane
CN106370370A (en) * 2016-08-17 2017-02-01 中国航空工业集团公司西安飞行自动控制研究所 Rapidly changeable actuator vibration test clamp
CN106402077A (en) * 2016-11-29 2017-02-15 四川凌峰航空液压机械有限公司 Hydraulic actuator cylinder output speed controllable hydraulic loop system
CN106736137A (en) * 2016-11-29 2017-05-31 沈阳黎明航空发动机(集团)有限责任公司 A kind of adjustable linkage mechanism for the welding of pressurized strut pipeline

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202571742U (en) * 2012-05-23 2012-12-05 广州飞机维修工程有限公司 Installation centering device of airplane pneumatic control valve actuator cylinder
CN103267638A (en) * 2013-05-10 2013-08-28 西安航空动力股份有限公司 Aero-engine elbow nozzle auxiliary oil way pre-welding test clamp
CN104236682A (en) * 2014-09-30 2014-12-24 四川泛华航空仪表电器有限公司 Universal flowmeter vibration test clamp
CN104459189A (en) * 2014-12-05 2015-03-25 四川凌峰航空液压机械有限公司 Actuator cylinder piston rod travel speed measurement device
CN204935428U (en) * 2015-07-03 2016-01-06 贵州红林机械有限公司 Baffle plate assembly tightness test fixture in a kind of aero-engine
CN105927617A (en) * 2016-06-12 2016-09-07 广州飞机维修工程有限公司 General test platform for large hydraulic actuator cylinder of airplane
CN106370370A (en) * 2016-08-17 2017-02-01 中国航空工业集团公司西安飞行自动控制研究所 Rapidly changeable actuator vibration test clamp
CN106402077A (en) * 2016-11-29 2017-02-15 四川凌峰航空液压机械有限公司 Hydraulic actuator cylinder output speed controllable hydraulic loop system
CN106736137A (en) * 2016-11-29 2017-05-31 沈阳黎明航空发动机(集团)有限责任公司 A kind of adjustable linkage mechanism for the welding of pressurized strut pipeline

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Application publication date: 20180417

RJ01 Rejection of invention patent application after publication