CN106091847A - A kind of guided missile quality center of mass and appearance and size integrated measurer - Google Patents
A kind of guided missile quality center of mass and appearance and size integrated measurer Download PDFInfo
- Publication number
- CN106091847A CN106091847A CN201610389866.5A CN201610389866A CN106091847A CN 106091847 A CN106091847 A CN 106091847A CN 201610389866 A CN201610389866 A CN 201610389866A CN 106091847 A CN106091847 A CN 106091847A
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- China
- Prior art keywords
- measurement
- afterbody
- outside diameter
- diameter measuring
- bullet
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
- F42B35/02—Gauging, sorting, trimming or shortening cartridges or missiles
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
Abstract
The invention discloses a kind of guided missile quality center of mass and appearance and size integrated measurer, including base, working plate and lowering or hoisting gear assembly, four measurement assembly line slideways are installed on working plate, it is connected with four outside diameter measuring assemblies and four span rudder exhibition measurement assemblies by measuring assembly slide block on four measurement assembly line slideways, working plate is fixedly connected with bullet measurement assembly along the one end in base length direction, and the other end is fixedly connected with afterbody measurement assembly；Lowering or hoisting gear assembly includes lifting base plate, lift and LOAD CELLS, lift top is provided with self-powered platform, two carriage assembly line slideways are installed on self-powered platform, two carriage assembly line slideways are connected with two carriage assemblies by carriage assembly slide block；The bottom of self-powered platform is fixedly connected with sensor bulb.Present configuration is compact, it is achieved convenient and low cost, uses simple operation, improves operating efficiency, alleviate labour intensity, practical.
Description
Technical field
The invention belongs to guided missile field of measuring technique, be specifically related to a kind of guided missile quality center of mass and appearance and size integrated test
Amount device.
Background technology
With the development of aerospace industries science and technology, the internal structure of guided missile is day by day complicated, leading after being completed
The quality of bullet, barycenter and appearance and size are the important parameters in general assembly, and its certainty of measurement has in Aerospace Engineering
Extremely important meaning, these parameters have strong influence to the initial disturbance of guided missile, flight attitude and accuracy at target, because of
This, quality center of mass and the shape dimension measurement of research guided missile are necessary.
Traditional quality center of mass test desk, is both needed to use manual hand manipulation, and after having measured quality center of mass, other
Appearance and size (such as rudder length degree, spanwise length, certain position diameter dimension of guided missile and length dimension) also need to individually enter
Row measurement, wastes substantial amounts of time and manpower, and the data measured can be because the operation technique of personnel produces error, measurement
Result directly affect the launch and flight of guided missile, therefore, study a fully automatic integral test desk and be very important.
Content of the invention
The technical problem to be solved is for above-mentioned deficiency of the prior art, provides a kind of guided missile quality
Barycenter and appearance and size integrated measurer, its compact conformation, novel in design reasonable, it is achieved convenient and low cost, use behaviour
It is convenient to make, and improves operating efficiency, alleviates labour intensity, practical, and using effect is good, it is simple to promote the use of.
For solving above-mentioned technical problem, the technical solution used in the present invention is: a kind of guided missile quality center of mass and appearance and size
Integrated measurer, it is characterised in that: include base and be fixedly connected on working plate and the lowering or hoisting gear of base top
Assembly, on described working plate, the length direction along base is provided with four measurement assembly line slideways, four described measurement groups
By being connected with four outside diameter measuring groups with the measurement assembly slide block that measurement assembly line slideway is slidably connected on part line slideway
Part and four span rudder exhibition measurement assemblies, described working plate is fixedly connected with bullet measurement group along the one end in base length direction
Part, described working plate is fixedly connected with afterbody measurement assembly along the other end in base length direction；Described lowering or hoisting gear assembly
Including lift base plate and the lift being arranged on lifting base plate and for measuring the LOAD CELLS of quality and barycenter, described
Lift top is provided with self-powered platform, and on described self-powered platform, the length direction along base is provided with two carriage assemblies
Line slideway, by sliding with the carriage assembly that carriage assembly line slideway is slidably connected on two described carriage assembly line slideways
Block is connected with two carriage assemblies for supporting measured guided missile；The bottom of described self-powered platform be fixedly connected with for
The sensor bulb that LOAD CELLS contacts.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described measurement group
It is provided with outside diameter measuring assembly latch segment and span rudder exhibition measurement assembly latch segment, described carriage assembly straight line on part line slideway
It is provided with the carriage assembly latch segment for position on carriage assembly line slideway for the locking tray assembly on guide rail；Described work
Make on platen, to be provided with measurement package traces block, described self-powered platform is provided with carriage assembly guide track block.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: at the bottom of described base
Portion is connected with multiple leveling block.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described external diameter is surveyed
Amount assembly includes outside diameter measuring support and the outside diameter measuring bullet measurement cylinder mounting plate being arranged on outside diameter measuring support, outer
Footpath measurement line slideway and outside diameter measuring guide track block, described outside diameter measuring bullet measurement cylinder mounting plate is provided with external diameter and surveys
Amount cylinder, described outside diameter measuring line slideway slidably connects outside diameter measuring guide rail slide block, the work of described outside diameter measuring cylinder
Stopper rod end is connected with fixes the outside diameter measuring cylinder promotion plate being connected, described outside diameter measuring cylinder with outside diameter measuring guide rail slide block
Promoting plate top to be fixedly connected with outside diameter measuring dial gauge heightening base, described outside diameter measuring dial gauge heightening base top is fixing to be connected
There is outside diameter measuring dial gauge installing plate, described outside diameter measuring dial gauge installing plate is provided with outside diameter measuring and resets and support seat, outer
Footpath measurement dial gauge and the outside diameter measuring gauge outfit for the gauge outfit of fixed outer diameter measurement dial gauge fix seat, and described outside diameter measuring is multiple
Position supports and is connected with outside diameter measuring reset sleeve on seat, and the gauge outfit end of described outside diameter measuring dial gauge is connected with to be surveyed through external diameter
Amount reset sleeve and outside diameter measuring reset and support the outside diameter measuring reset lever of seat, and described outside diameter measuring resets in supporting seat and arranges
Having for supporting the outside diameter measuring linear bearing installing outside diameter measuring reset lever, described outside diameter measuring reset lever is positioned at external diameter
Being set with outside diameter measuring back-moving spring in measurement reset sleeve one section, the end of described outside diameter measuring reset lever is connected with
Outside diameter measuring reset connecting plate, described outside diameter measuring reset connecting plate is connected with outside diameter measuring reset survey mass.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described span rudder
Exhibition measurement assembly includes that span measurement support and the span measurement bullet measurement cylinder being arranged on span measurement support are installed
Plate, span measurement line slideway and span measurement guide track block, described span measurement bullet measurement cylinder mounting plate is provided with
Cylinder is measured in the span, and described span measurement line slideway slidably connects span measurement slide block, described span measurement guide rail gear
Being connected with span measurement slide block block on block, the piston rod end of described span measurement cylinder is connected with solid with span measurement slide block
The fixed span measurement cylinder connecting promotes plate, and described span measurement cylinder promotes plate top to be fixedly connected with span measurement dial gauge
Heightening base, described span measurement dial gauge heightening base top is fixedly connected with span measurement dial gauge installing plate, and the described span is surveyed
Span measurement span guide plate is installed and for fixing the span of the gauge outfit of span measurement dial gauge on amount dial gauge installing plate
Measurement gauge outfit fixes seat, and the gauge outfit of described span measurement dial gauge passes through the span and measures span guide plate.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described bullet is surveyed
Amount assembly includes that bullet measurement support is installed rebound and is arranged on the bullet measurement that rebound top installed by bullet measurement support
Support, described bullet measurement support is provided with bullet measurement cylinder mounting plate, bullet measurement line slideway and bullet measurement and leads
Rail block, described bullet measurement cylinder mounting plate is provided with bullet measurement cylinder, described bullet measurement line slideway slides
It is connected with bullet measurement guide rail slide block, described bullet measurement guide track block is connected with bullet measurement slide block block, described bullet
The piston rod end of measurement cylinder is connected with and fixes the bullet measurement cylinder promotion plate being connected with bullet measurement guide rail slide block, described
Bullet measurement cylinder promotes plate top to be fixedly connected with bullet measurement dial gauge heightening base, and dial gauge heightening base measured by described bullet
Top is fixedly connected with bullet measurement dial gauge installing plate, and described bullet measurement dial gauge installing plate is provided with bullet measurement hundred
Table and the bullet measurement gauge outfit for fixing the gauge outfit of bullet measurement dial gauge is divided to fix seat, the table of described bullet measurement dial gauge
Cephalic par is connected with bullet measurement gauge outfit reference block.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described afterbody is surveyed
Amount assembly includes that afterbody measurement support is installed rebound and is arranged on the afterbody measurement that rebound top installed by afterbody measurement support
Support, described afterbody measurement support is provided with afterbody measurement cylinder mounting plate, afterbody measurement line slideway and afterbody measurement and leads
Rail block, described afterbody measurement cylinder mounting plate is provided with afterbody measurement cylinder, described afterbody measurement line slideway slides
It is connected with afterbody measurement guide rail slide block, described afterbody measurement guide track block is connected with afterbody measurement slide block block, described afterbody
The piston rod end of measurement cylinder is connected with and fixes the afterbody measurement cylinder promotion plate being connected with afterbody measurement guide rail slide block, described
Afterbody measurement cylinder promotes plate top to be fixedly connected with afterbody measurement dial gauge heightening base, and described afterbody measures dial gauge heightening base
Top is fixedly connected with afterbody measurement dial gauge installing plate, described afterbody measurement dial gauge installing plate is provided with afterbody measurement multiple
Position supports seat, afterbody measurement dial gauge and the afterbody measurement gauge outfit for fixing the gauge outfit of afterbody measurement dial gauge and fixes seat, institute
Stating and being connected with afterbody measurement reset sleeve on afterbody measurement reset support seat, the gauge outfit end of described afterbody measurement dial gauge connects
Having resets through afterbody measurement reset sleeve and afterbody measurement supports the afterbody measurement reset lever of seat, and the measurement of described afterbody resets
Being provided with in supporting seat for supporting the afterbody measurement linear bearing installing afterbody measurement reset lever, the measurement of described afterbody resets
Pull bar is positioned on one section of afterbody measurement reset sleeve and is set with afterbody measurement back-moving spring, and described afterbody measures reset lever
End be connected with afterbody measurement gauge outfit reference block.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described lifting dress
Put the motor adapter that assembly includes being arranged on lifting base plate, described motor adapter is provided with for driving lift liter
The decelerator that is connected with the output shaft of fire-proof motor of fire-proof motor of fall and for supporting the of the output shaft of installation fire-proof motor
One bearing, the quantity of described lift is to be provided with lift connecting shaft between two and two lifts, and described lift is even
Two short connecting bushings are passed through at the two ends of spindle respectively and the lifting drive power shaft of two lifts connects, described decelerator
It is connected with lifting drive connecting shaft by long connecting bushing on output shaft, described lifting drive connecting shaft is connected with the first tooth
Wheel, described lift connecting shaft is connected with the second gear engaging with the first gear, described lifting base plate is provided with for
Support and two the first rolling bearing units of lifting drive connecting shaft are installed and for supporting two second of installation lift connecting shaft
Rolling bearing units, the top of described lift is provided with lift top board, and described lift top board top is provided with jacking block and difference
Being positioned at two lift footstocks of jacking block both sides, described lifting base plate being provided with sensor base, described LOAD CELLS is pacified
Being contained in sensor base, described LOAD CELLS top is provided with the sensor backing plate for contacting with sensor bulb,
The quantity of described sensor base, LOAD CELLS, sensor backing plate and sensor bulb is three.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described lifting work
The bottom of station is connected with the jacking block seat for being connected together on jacking block；It is fixedly connected with for lift on described base
The travel switch assembly that detects of raising and lowering position, described travel switch assembly include travel switch fixed plate and
For upper stroke switch that the lifting position of lift is detected with for the down position of lift is detected
Lower stroke switch, described upper stroke switch is fixedly connected on travel switch fixed plate top, and described lower stroke switch is fixing to be connected
In travel switch fixed plate bottom；Be fixedly connected with on described lift with rise when with upper stroke switch touching and under
Stroke limit plate with lower stroke switch touching during fall.
Above-mentioned a kind of guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: described bracket group
Part includes bracket and is fixedly connected on two supporter roller seats of pallet top, is provided with between described supporter roller seat and bracket
Measurement and positioning block, described supporter roller seat is fixedly connected with deep groove ball bearing, described deep groove ball bearing and supporter roller seat it
Between be provided with roller spacer ring, described deep groove ball bearing is provided with roller shaft, described roller shaft is fixedly connected with roller.
The present invention compared with prior art has the advantage that
1st, the quality center of mass of guided missile and the measurement of appearance and size are integrated in one by the present invention, define a set of mass parameter and
Appearance and size composite measurement platform, compact conformation, novel in design reasonable, it is achieved convenient and low cost.
2nd, the use simple operation of the present invention.
3rd, the present invention just can be measured quality center of mass and the appearance and size of guided missile by once lifting, ensure that measurement
Accuracy and uniformity, improve operating efficiency, alleviate labour intensity.
4th, the present invention's is practical, and using effect is good, it is simple to promote the use of.
In sum, present configuration is compact, novel in design reasonable, it is achieved convenient and low cost, uses simple operation, carries
High operating efficiency, alleviates labour intensity, and practical, using effect is good, it is simple to promote the use of.
Below by drawings and Examples, technical scheme is described in further detail.
Brief description
Fig. 1 is the front view of the present invention.
Fig. 2 is the left view of Fig. 1.
Fig. 3 is the structural representation of outside diameter measuring assembly of the present invention.
Fig. 4 is the structural representation of span rudder of the present invention exhibition measurement assembly.
Fig. 5 is the structural representation of bullet of the present invention measurement assembly.
Fig. 6 is the structural representation of afterbody of the present invention measurement assembly.
Fig. 7 is the front view of lowering or hoisting gear assembly of the present invention.
Fig. 8 is the top view of Fig. 7.
Fig. 9 is the structural representation of travel switch assembly of the present invention.
Figure 10 is the front view of carriage assembly of the present invention.
Figure 11 is the left view of Figure 10.
Description of reference numerals:
1 base；2 span rudder exhibition measurement assembly latch segments；
3 working plates；4 bullet measurement assemblies；
Rebound installed by 4-1 bullet measurement support；Support measured by 4-2 bullet；
Cylinder mounting plate measured by 4-3 bullet；4-4 bullet measurement cylinder promotes plate；
Dial gauge heightening base measured by 4-5 bullet；Dial gauge installing plate measured by 4-6 bullet；
Gauge outfit reference block measured by 4-7 bullet；4-8 bullet measurement gauge outfit fixes seat；
Guide track block measured by 4-9 bullet；Slide block block measured by 4-10 bullet；
Slide block block measured by 4-11 bullet；Line slideway measured by 4-12 bullet；
Dial gauge measured by 4-13 bullet；Guide rail slide block measured by 4-14 bullet；
5 carriage assembly guide track block；6 carriage assembly latch segments；
7 carriage assemblies；7-1 bracket；
7-2 supporter roller seat；7-3 roller shaft；
7-4 roller；7-5 roller spacer ring；
7-6 measurement and positioning block；7-7 deep groove ball bearing；
8 outside diameter measuring assemblies；8-1 outside diameter measuring support；
8-2 outside diameter measuring dial gauge installing plate；8-3 outside diameter measuring resets and supports seat；
8-4 outside diameter measuring reset connecting plate；8-5 outside diameter measuring reset survey mass；
8-6 outside diameter measuring reset sleeve；8-7 outside diameter measuring reset lever；
8-8 outside diameter measuring gauge outfit fixes seat；8-9 outside diameter measuring dial gauge heightening base；
8-10 outside diameter measuring cylinder promotes plate；8-11 outside diameter measuring cylinder mounting plate；
8-12 outside diameter measuring guide track block；8-13 outside diameter measuring back-moving spring；
8-14 outside diameter measuring dial gauge；8-15 outside diameter measuring linear bearing；
8-16 outside diameter measuring cylinder；8-17 outside diameter measuring line slideway；
8-18 outside diameter measuring guide rail slide block；9 span rudder exhibition measurement assemblies；
Support is measured in the 9-1 span；Cylinder mounting plate is measured in the 9-2 span；
9-3 span measurement cylinder promotes plate；Dial gauge heightening base is measured in the 9-4 span；
Dial gauge installing plate is measured in the 9-5 span；9-6 span measurement gauge outfit fixes seat；
Guide track block is measured in the 9-7 span；Slide block block is measured in the 9-8 span；
Span guide plate is measured in the 9-9 span；Cylinder is measured in the 9-10 span；
Line slideway is measured in the 9-11 span；Dial gauge is measured in the 9-12 span；
Slide block is measured in the 9-13 span；10 outside diameter measuring assembly latch segments；
11 measurement package traces blocks；12 jacking block seats；
13 lowering or hoisting gear assemblies；13-1 lifts base plate；
13-2 lift footstock；13-3 lift top board；
The short connecting bushing of 13-4；13-5 sensor backing plate；
13-6 lift connecting shaft；13-7 the second rolling bearing units；
13-8 the first gear；13-9 lifting drive connecting shaft；
The long connecting bushing of 13-10；13-11 motor adapter；
13-12 sensor base；13-13 the second gear；
13-14 jacking block；13-15 the first rolling bearing units；
13-16 decelerator；13-17 fire-proof motor；
13-18 lift；13-19 LOAD CELLS；
13-20 clutch shaft bearing；13-21 stroke limit plate；
14 travel switch assemblies；14-1 travel switch assembly；
14-2 upper stroke switch；14-3 lower stroke switch；
15 sensor bulbs；16 leveling block；
17 afterbody measurement assemblies；Rebound installed by 17-1 afterbody measurement support；
17-2 afterbody measures support；17-3 afterbody measures cylinder mounting plate；
17-4 afterbody measurement cylinder promotes plate；17-5 afterbody measures dial gauge heightening base；
17-6 afterbody measures dial gauge installing plate；17-7 afterbody measurement gauge outfit fixes seat；
17-8 afterbody measures reset sleeve；17-9 afterbody measures reset lever；
The measurement of 17-10 afterbody resets and supports seat；17-11 afterbody measures gauge outfit reference block；
17-12 afterbody measures guide track block；17-13 afterbody measures slide block block；
17-14 afterbody measures linear bearing；17-15 afterbody measures cylinder；
17-16 afterbody measures line slideway；17-17 afterbody measures dial gauge；
17-18 afterbody measures guide rail slide block；17-19 afterbody measures back-moving spring；
18 self-powered platforms；19 measured guided missiles；
20 measurement assembly slide blocks；21 measurement assembly line slideways；
22 carriage assembly slide blocks；23 carriage assembly line slideways.
Detailed description of the invention
As depicted in figs. 1 and 2, the guided missile quality center of mass of the present invention and appearance and size integrated measurer, including base 1
And it is fixedly connected on working plate 3 and the lowering or hoisting gear assembly 13 at base 1 top, along the length of base 1 on described working plate 3
Degree direction be provided with four measurement assembly line slideways 21, four described measurement assembly line slideways 21 on by with measurement assembly
The measurement assembly slide block 20 that line slideway 21 is slidably connected is connected with four outside diameter measuring assemblies 8 and four span rudder exhibition measurement groups
Part 9, described working plate 3 is fixedly connected with bullet measurement assembly 4, described working plate 3 edge along one end of base 1 length direction
The other end of base 1 length direction is fixedly connected with afterbody measurement assembly 17；Described lowering or hoisting gear assembly 13 includes lifting base plate
13-1 and be arranged on lifting base plate 13-1 on lift 13-18 and for measuring the LOAD CELLS 13-of quality and barycenter
19, described lift 13-18 top is provided with self-powered platform 18, along the length direction of base 1 on described self-powered platform 18
Two carriage assembly line slideways 23 are installed, by leading with carriage assembly straight line on two described carriage assembly line slideways 23
The carriage assembly slide block 22 that rail 23 is slidably connected is connected with two carriage assemblies 7 for supporting measured guided missile 19；Described liter
The bottom of fall workbench 18 is fixedly connected with the sensor bulb 15 for contacting with LOAD CELLS 13-19.
As depicted in figs. 1 and 2, in the present embodiment, described measurement assembly line slideway 21 is provided with outside diameter measuring assembly
Latch segment 10 and span rudder exhibition measurement assembly latch segment 2, described carriage assembly line slideway 23 is provided with for locking tray
The carriage assembly latch segment 6 of position on carriage assembly line slideway 23 for the assembly 7；It is provided with measurement on described working plate 3
Package traces block 11, described self-powered platform 18 is provided with carriage assembly guide track block 5.Due to four outside diameter measuring assemblies
8 and four span rudders exhibition measurement assemblies 9 be slidably connected on measurement assembly line slideway 21 by measuring assembly slide block 20, therefore
Four outside diameter measuring assemblies 8 and the measurement position of four span rudder exhibition measurement assemblies 9 can be regulated according to practical measurement requirement；Logical
Cross and outside diameter measuring assembly latch segment 10 and span rudder exhibition measurement assembly latch segment 2 are set, behind the position of measurement well to be determined, by outward
Footpath measurement assembly latch segment 10 pins the position of outside diameter measuring assembly 8, and is locked by span rudder exhibition measurement assembly latch segment 2
Determine the position of span rudder exhibition measurement assembly 9, the measure error producing during measurement can be reduced because position is moved.Due to
Carriage assembly 7 is slidably connected on carriage assembly line slideway 23 by carriage assembly slide block 22, therefore, it is possible at carriage assembly
Arbitrarily slide on line slideway 23, according to actual needs the position of bracket assembly 7, ensure the steady of measured guided missile 19
Safety is placed；By arranging carriage assembly latch segment 6, behind the position of measurement well to be determined, pinned by carriage assembly latch segment 6
The position of carriage assembly 7, it can be ensured that security measurement.
As depicted in figs. 1 and 2, it, in the present embodiment, bottom described base 1, is connected with multiple leveling block 16.
As it is shown on figure 3, in the present embodiment, outside described outside diameter measuring assembly 8 includes outside diameter measuring support 8-1 and is arranged on
Outside diameter measuring bullet measurement cylinder mounting plate 8-11, outside diameter measuring line slideway 8-17 on footpath measurement support 8-1 and external diameter are surveyed
Amount guide track block 8-12, described outside diameter measuring bullet measurement cylinder mounting plate 8-11 is provided with outside diameter measuring cylinder 8-16, institute
State and on outside diameter measuring line slideway 8-17, slidably connect outside diameter measuring guide rail slide block 8-18, described outside diameter measuring cylinder 8-16's
Piston rod end is connected with to be fixed the outside diameter measuring cylinder that is connected and promotes plate 8-10 with outside diameter measuring guide rail slide block 8-18, described outside
Footpath measurement cylinder promotes plate 8-10 top to be fixedly connected with outside diameter measuring dial gauge heightening base 8-9, described outside diameter measuring dial gauge
Heightening base 8-9 top is fixedly connected with outside diameter measuring dial gauge installing plate 8-2, on described outside diameter measuring dial gauge installing plate 8-2
Outside diameter measuring reset is installed and supports seat 8-3, outside diameter measuring dial gauge 8-14 and for fixed outer diameter measurement dial gauge 8-14's
The outside diameter measuring gauge outfit of gauge outfit fixes seat 8-8, and described outside diameter measuring resets to support and is connected with outside diameter measuring reset sleeve on seat 8-3
8-6, the gauge outfit end of described outside diameter measuring dial gauge 8-14 is connected with through outside diameter measuring reset sleeve 8-6 and outside diameter measuring multiple
Position supports outside diameter measuring reset lever 8-7 of seat 8-3, and described outside diameter measuring resets in supporting seat 8-3 and is provided with for supporting peace
The outside diameter measuring linear bearing 8-15 of dress outside diameter measuring reset lever 8-7, described outside diameter measuring reset lever 8-7 is positioned at external diameter and surveys
It is set with outside diameter measuring back-moving spring 8-13, the end of described outside diameter measuring reset lever 8-7 in amount reset sleeve 8-6 one section
Portion is connected with outside diameter measuring reset connecting plate 8-4, described outside diameter measuring reset connecting plate 8-4 is connected with outside diameter measuring reset and surveys
Gauge block 8-5.
As shown in Figure 4, in the present embodiment, described span rudder exhibition measurement assembly 9 includes span measurement support 9-1 and installation
Span measurement bullet measurement cylinder mounting plate 9-2, span measurement line slideway 9-11 on span measurement support 9-1 and the span
Measurement guide track block 9-7, described span measurement bullet measurement cylinder mounting plate 9-2 is provided with span measurement cylinder 9-10, institute
State and on span measurement line slideway 9-11, slidably connect span measurement slide block 9-13, on described span measurement guide track block 9-7
Being connected with span measurement slide block block 9-8, the piston rod end of described span measurement cylinder 9-10 is connected with sliding with span measurement
The span measurement cylinder that block 9-13 fixes connection promotes plate 9-3, and described span measurement cylinder promotes plate 9-3 top to be fixedly connected with
Dial gauge heightening base 9-4 is measured in the span, and described span measurement dial gauge heightening base 9-4 top is fixedly connected with span measurement percentage
Table installing plate 9-5, described span measurement dial gauge installing plate 9-5 is provided with span measurement span guide plate 9-9 and for admittedly
The span measurement gauge outfit of the gauge outfit determining span measurement dial gauge 9-12 fixes seat 9-6, the table of described span measurement dial gauge 9-12
Head passes through the span and measures span guide plate 9-9.
As it is shown in figure 5, in the present embodiment, described bullet measurement assembly 4 include bullet measurement support install rebound 4-1 and
It is arranged on bullet measurement support and the bullet measurement support 4-2 at rebound 4-1 top, peace on described bullet measurement support 4-2 are installed
Equipped with bullet measurement cylinder mounting plate 4-3, bullet measurement line slideway 4-12 and bullet measurement guide track block 4-9, described bullet
Bullet measurement cylinder 4-11 is installed on measurement cylinder mounting plate 4-3, described bullet measurement line slideway 4-12 is slidably connected
There is bullet measurement guide rail slide block 4-14, described bullet measurement guide track block 4-9 is connected with bullet measurement slide block block 4-10, institute
State bullet measurement cylinder 4-11 piston rod end be connected with bullet measurement guide rail slide block 4-14 fix be connected bullet measurement
Cylinder promotes plate 4-4, and described bullet measurement cylinder promotes plate 4-4 top to be fixedly connected with bullet measurement dial gauge heightening base 4-5,
Described bullet measurement dial gauge heightening base 4-5 top is fixedly connected with bullet measurement dial gauge installing plate 4-6, and described bullet is measured
Bullet measurement dial gauge 4-13 is installed and for fixing the gauge outfit of bullet measurement dial gauge 4-13 on dial gauge installing plate 4-6
Bullet measurement gauge outfit fixes seat 4-8, and the gauge outfit end of described bullet measurement dial gauge 4-13 is connected with bullet measurement gauge outfit benchmark
Block 4-7.
As shown in Figure 6, in the present embodiment, described afterbody measurement assembly 17 includes that rebound 17-1 installed by afterbody measurement support
With the afterbody measurement support 17-2 being arranged on afterbody measurement support installation rebound 17-1 top, described afterbody measures support 17-2
On be provided with afterbody measurement cylinder mounting plate 17-3, afterbody measurement line slideway 17-16 and afterbody measurement guide track block 17-12,
Being provided with afterbody measurement cylinder 17-15 on described afterbody measurement cylinder mounting plate 17-3, described afterbody measures line slideway 17-16
On slidably connect afterbody measurement guide rail slide block 17-18, described afterbody measurement guide track block 17-12 is connected with afterbody measurement sliding
Block block 17-13, the piston rod end of described afterbody measurement cylinder 17-15 is connected with solid with afterbody measurement guide rail slide block 17-18
The fixed afterbody measurement cylinder connecting promotes plate 17-4, and described afterbody measurement cylinder promotes plate 17-4 top to be fixedly connected with afterbody and surveys
Amount dial gauge heightening base 17-5, described afterbody measurement dial gauge heightening base 17-5 top is fixedly connected with afterbody measurement dial gauge peace
Dress plate 17-6, described afterbody measurement dial gauge installing plate 17-6 is provided with afterbody measurement reset and supports seat 17-10, afterbody measurement
Dial gauge 17-17 and the afterbody measurement gauge outfit for fixing the gauge outfit of afterbody measurement dial gauge 17-17 fix seat 17-7, described tail
Portion's measurement resets to support and is connected with afterbody measurement reset sleeve 17-8 on seat 17-10, the table of described afterbody measurement dial gauge 17-17
The afterbody measurement reset that cephalic par is connected with through afterbody measurement reset sleeve 17-8 and afterbody measurement reset support seat 17-10 is drawn
Bar 17-9, the measurement of described afterbody resets to be provided with in supporting seat 17-10 and installs afterbody measurement reset lever 17-9 for supporting
Afterbody measures linear bearing 17-14, and described afterbody measurement reset lever 17-9 is positioned at the one of afterbody measurement reset sleeve 17-8
Being set with back-moving spring 17-15 on Duan, the end of described afterbody measurement reset lever 17-9 is connected with afterbody measurement gauge outfit benchmark
Block 17-11.
As shown in Figure 7 and Figure 8, in the present embodiment, described lowering or hoisting gear assembly 13 includes being arranged on lifting base plate 13-1
Motor adapter 13-11, described motor adapter 13-11 is provided with the anti-explosion electric for driving lift 13-18 to lift
Decelerator 13-16 that machine 13-17 is connected with the output shaft of fire-proof motor 13-17 and install fire-proof motor 13-17's for supporting
The clutch shaft bearing 13-20 of output shaft, the quantity of described lift 13-18 is to be provided with between two and two lift 13-18
Lift connecting shaft 13-6, the two ends of described lift connecting shaft 13-6 are risen by two short connecting bushing 13-4 and two respectively
The lifting drive power shaft of fall machine 13-18 connects, on the output shaft of described decelerator 13-16 by long connecting bushing 13-10 even
It is connected to lifting drive connecting shaft 13-9, described lifting drive connecting shaft 13-9 is connected with the first gear 13-8, described lift
It is connected with the second gear 13-13 engaging with the first gear 13-8 in connecting shaft 13-6, described lifting base plate 13-1 is provided with
For supporting two the first rolling bearing units 13-15 installing lifting drive connecting shaft 13-9 and connecting for supporting installation lift
Two second rolling bearing units 13-7 of axle 13-6, the top of described lift 13-18 is provided with lift top board 13-3, described liter
Fall machine top board 13-3 top is provided with jacking block 13-14 and lays respectively at two lift footstock 13-2 of jacking block 13-14 both sides, institute
Stating and being provided with sensor base 13-12 on lifting base plate 13-1, described LOAD CELLS 13-19 is arranged on sensor base 13-
On 12, described LOAD CELLS 13-19 top is provided with the sensor backing plate 13-5 for contacting, institute with sensor bulb 15
The quantity stating sensor base 13-12, LOAD CELLS 13-19, sensor backing plate 13-5 and sensor bulb 15 is three.
As it is shown in figure 9, in the present embodiment, the bottom of described self-powered platform 18 is connected with for being connected together at jacking block
Jacking block seat 12 on 13-14；It is fixedly connected with on described base 1 for the raising and lowering position of lift 13-18 is carried out
The travel switch assembly 14 of detection, described travel switch assembly 14 includes travel switch fixed plate 14-1 and for lift
Upper stroke switch 14-2 that the lifting position of 13-18 detects and for the down position of lift 13-18 is detected
Lower stroke switch 14-3, described upper stroke switch 14-2 is fixedly connected on travel switch fixed plate 14-1 top, described descending
Cheng Kaiguan 14-3 is fixedly connected on travel switch fixed plate 14-1 bottom；Be fixedly connected with on described lift 13-18 with
With upper stroke switch 14-2 touching the stroke limit plate 13-21 touching with lower stroke switch 14-3 when declining during rising.Institute
State and lift 13-18 lifting process uses jacking block 13-14 and jacking block seat 12 positioning and guiding, it is ensured that lifting is steadily.
As shown in Figure 10 and Figure 11, in the present embodiment, described carriage assembly 7 includes bracket 7-1 and is fixedly connected on bracket
Two supporter roller seat 7-2 at 7-1 top, are provided with measurement and positioning block 7-6 between described supporter roller seat 7-2 and bracket 7-1,
Be fixedly connected with on described supporter roller seat 7-2 deep groove ball bearing 7-7, described deep groove ball bearing 7-7 and supporter roller seat 7-2 it
Between be provided with roller spacer ring 7-5, described deep groove ball bearing 7-7 is provided with roller shaft 7-3, on described roller shaft 7-3 fixing even
It is connected to roller 7-4.
The present invention can be used in the length dimension to measured guided missile 19, outside dimension, span rudder exhibition size and quality matter
The heart measures, and concrete measurement process is:
1st, length dimension measurement: as depicted in figs. 1 and 2, when the lifting of measured guided missile 19 is placed on two groups of carriage assemblies 7
When, proceed by the measurement of appearance and size；As it is shown in figure 5, to bullet measurement cylinder 4-11 supply, promote bullet measurement guide rail sliding
Block 4-14 upper element advances along bullet measurement line slideway 4-12, when bullet measurement cylinder promotes plate 4-4 to measure with bullet
During slide block block 4-10 contact, slide and stop, the head of the measured guided missile 19 of bullet measurement gauge outfit reference block 4-7 contact, and push away
Head of moving measurement dial gauge 4-13 produces data；Meanwhile, as shown in Figure 6, to afterbody measurement cylinder 17-15 supply, promote
Afterbody measurement guide rail slide block 17-18 upper element advances along afterbody measurement line slideway 17-16, when afterbody measurement cylinder promotes
Plate 17-4 contacts with afterbody measurement slide block block 17-13, slides and stops, and afterbody measurement gauge outfit reference block 17-11 contact is measured
The afterbody of guided missile 19, promotes afterbody measurement dial gauge 17-17 to produce data by afterbody measurement reset lever 17-9；Bullet is measured
Data and the data of afterbody measurement dial gauge 17-17 generation that dial gauge 4-13 produces are transferred to computer, for computer to quilt
The length of measurement guided missile 19 calculates；After measurement terminates, bullet measurement cylinder 4-11 and afterbody measurement cylinder 17-15 resets,
Bullet measurement gauge outfit reference block 4-7 separates with the head of measured guided missile 19, at the beginning of bullet measurement dial gauge 4-13 automatically resets into
Beginning state, afterbody measurement gauge outfit reference block 17-11 separates with the afterbody of measured guided missile 19, and afterbody measurement dial gauge 17-17 leads to
Cross afterbody measurement back-moving spring 17-19 and reset to original state.
2nd, measuring outside diameter: as depicted in figs. 1 and 2, installs four outside diameter measuring assemblies 8 to measurement assembly line slideway
On 21, each two groups of left and right, measure the outside dimension of measured 19 two positions of guided missile；Adjust the position of outside diameter measuring assembly 8
Afterwards, being locked by outside diameter measuring assembly latch segment 10, it is ensured that during measurement, outside diameter measuring assembly 8 will not be surveyed moving influence
Amount result.As it is shown on figure 3, give outside diameter measuring cylinder 8-16 supply, promote outside diameter measuring guide rail slide block 8-18 upper element along
Outside diameter measuring line slideway 8-17 advances, when outside diameter measuring cylinder promotes plate 8-10 to contact with outside diameter measuring guide track block 8-12
When, sliding and stop, outside diameter measuring reset survey mass 8-5 touches measured guided missile 19 outside diameter measuring point, multiple by outside diameter measuring
Position pull bar 8-7 promotes outside diameter measuring dial gauge 8-14 to produce data, the outside diameter measuring percentage in the outside diameter measuring assembly 8 of two groups, left and right
The data that table 8-14 produces are transferred to computer, calculate for the external diameter to measured guided missile 19 for the computer.After being measured,
Outside diameter measuring cylinder 8-16 resets, and outside diameter measuring dial gauge 8-14 resets to initial shape by outside diameter measuring back-moving spring 8-13
State.
3rd, span rudder exhibition dimensional measurement: as depicted in figs. 1 and 2, installs four span rudder exhibition measurement assemblies 9 to measurement assembly
On line slideway 21, each two groups of left and right, measure the span of measured guided missile 19 and the length dimension of rudder exhibition respectively；Adjust the span
After the position of rudder exhibition measurement assembly 9, locked by span rudder exhibition measurement assembly latch segment 2, it is ensured that during measurement, span rudder
Exhibition measurement assembly 9 will not moving influence measurement result.As shown in Figure 4, to span measurement cylinder 9-10 supply, span measurement is promoted
Slide block 9-13 upper element advances along span measurement line slideway 9-11, when span measurement cylinder promotes plate 9-3 to survey with the span
During amount slide block block 9-8 contact, slide and stop, the span of the span measurement measured guided missile 19 of dial gauge 9-12 gauge outfit location contacts
Produce data, the data transmission that the span measurement dial gauge 9-12 in the span rudder exhibition measurement assembly 9 of two groups, left and right produces with rudder exhibition
To computer, calculate for spanwise length and rudder length degree to measured guided missile 19 for the computer.After being measured, the span is surveyed
Amount cylinder 9-10 resets, and span measurement dial gauge 9-12 automatically restores to original state.
4th, quality center of mass measurement: as depicted in figs. 1 and 2, after the shape dimension measurement of guided missile 19 to be measured completes, pass through
Self-powered platform 18 is fallen by lowering or hoisting gear assembly 13, until three sensor bulbs 15 smoothly fall at sensor cushion block 13-
On 5, self-powered platform 18 is kept completely separate with jacking block seat 12, and three LOAD CELLS 13-19 produce data, three LOAD CELLSs
The data that 13-19 produces are transferred to computer, calculate for the quality to measured guided missile 19 for the computer；Then, such as Fig. 5 institute
Show, to bullet measurement cylinder 4-11 supply, promote bullet measurement guide rail slide block 4-14 upper element to lead along bullet measurement straight line
Rail 4-12 advances, and when bullet measurement cylinder promotes plate 4-4 to contact with bullet measurement slide block block 4-10, slides and stops, bullet
The head of the measured guided missile 19 of measurement gauge outfit reference block 4-7 contact, promotes bullet measurement dial gauge 4-13 to produce data；Bullet is surveyed
The data that amount dial gauge 4-13 produces are transferred to computer, calculate for the barycenter to measured guided missile 19 for the computer；Then,
Bullet measurement cylinder 4-11 resets, and bullet measurement gauge outfit reference block 4-7 separates with the head of measured guided missile 19, bullet measurement hundred
Point table 4-13 automatically resets into original state, then by lowering or hoisting gear assembly 13 by self-powered platform 18 jack-up, allows sensor
Bulb 15 separates with sensor cushion block 13-5, is measured.
The above, be only presently preferred embodiments of the present invention, not impose any restrictions the present invention, every according to the present invention
Any simple modification, change and the equivalent structure change that above example is made by technical spirit, all still falls within skill of the present invention
In the protection domain of art scheme.
Claims (10)
1. a guided missile quality center of mass and appearance and size integrated measurer, it is characterised in that: include base (1) and fix
It is connected to working plate (3) and the lowering or hoisting gear assembly (13) at base (1) top, along base (1) on described working plate (3)
Length direction is provided with four measurements assembly line slideway (21), on four described measurements assembly line slideway (21) by with survey
Measurement assembly slide block (20) that amount assembly line slideway (21) is slidably connected is connected with four outside diameter measuring assemblies (8) and four wings
Exhibition rudder exhibition measurement assembly (9), described working plate (3) is fixedly connected with bullet measurement group along one end of base (1) length direction
Part (4), described working plate (3) is fixedly connected with afterbody measurement assembly (17) along the other end of base (1) length direction；Described
Lowering or hoisting gear assembly (13) include lifting base plate (13-1) and the lift (13-18) being arranged in lifting base plate (13-1) and
For measuring the LOAD CELLS (13-19) of quality and barycenter, described lift (13-18) top is provided with self-powered platform
(18), described self-powered platform (18) is provided with two carriage assembly line slideways (23) along the length direction of base (1), two
Carriage assembly slide block by being slidably connected with carriage assembly line slideway (23) on carriage assembly line slideway (23) described in root
(22) it is connected with two carriage assemblies (7) for supporting measured guided missile (19)；The bottom of described self-powered platform (18) is solid
Surely it is connected with the sensor bulb (15) for contacting with LOAD CELLS (13-19).
2. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
It is provided with outside diameter measuring assembly latch segment (10) and the exhibition measurement assembly locking of span rudder on described measurement assembly line slideway (21)
Block (2), described carriage assembly line slideway (23) is provided with for locking tray assembly (7) at carriage assembly line slideway
(23) the carriage assembly latch segment (6) of the position on；It is provided with measurement package traces block (11) on described working plate (3),
It is provided with carriage assembly guide track block (5) on described self-powered platform (18).
3. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
Described base (1) bottom is connected with multiple leveling block (16).
4. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
Described outside diameter measuring assembly (8) includes that outside diameter measuring support (8-1) and the external diameter being arranged on outside diameter measuring support (8-1) are surveyed
Amount bullet measurement cylinder mounting plate (8-11), outside diameter measuring line slideway (8-17) and outside diameter measuring guide track block (8-12), institute
State, on outside diameter measuring bullet measurement cylinder mounting plate (8-11), outside diameter measuring cylinder (8-16), described outside diameter measuring straight line are installed
Outside diameter measuring guide rail slide block (8-18), the tailpiece of the piston rod of described outside diameter measuring cylinder (8-16) is slidably connected on guide rail (8-17)
Portion is connected with the outside diameter measuring cylinder that be connected fixing with outside diameter measuring guide rail slide block (8-18) and promotes plate (8-10), and described external diameter is surveyed
Amount cylinder promotes plate (8-10) top to be fixedly connected with outside diameter measuring dial gauge heightening base (8-9), described outside diameter measuring dial gauge
Heightening base (8-9) top is fixedly connected with outside diameter measuring dial gauge installing plate (8-2), described outside diameter measuring dial gauge installing plate
(8-2) outside diameter measuring reset is installed on support seat (8-3), outside diameter measuring dial gauge (8-14) and measure hundred for fixed outer diameter
The outside diameter measuring gauge outfit dividing the gauge outfit of table (8-14) fixes seat (8-8), and described outside diameter measuring resets to support and is connected with on seat (8-3)
Outside diameter measuring reset sleeve (8-6), the gauge outfit end of described outside diameter measuring dial gauge (8-14) is connected with through outside diameter measuring multiple
Position sleeve (8-6) and outside diameter measuring reset and support the outside diameter measuring reset lever (8-7) of seat (8-3), and described outside diameter measuring resets
It is provided with in supporting seat (8-3) for supporting the outside diameter measuring linear bearing (8-15) installing outside diameter measuring reset lever (8-7),
Described outside diameter measuring reset lever (8-7) is positioned on one section of outside diameter measuring reset sleeve (8-6) and is set with outside diameter measuring again
Position spring (8-13), the end of described outside diameter measuring reset lever (8-7) is connected with outside diameter measuring reset connecting plate (8-4), institute
State and on outside diameter measuring reset connecting plate (8-4), be connected with outside diameter measuring reset survey mass (8-5).
5. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
Described span rudder exhibition measurement assembly (9) includes span measurement support (9-1) and the wing being arranged in span measurement support (9-1)
Exhibition measurement bullet measurement cylinder mounting plate (9-2), span measurement line slideway (9-11) and span measurement guide track block (9-7),
Being provided with span measurement cylinder (9-10) in described span measurement bullet measurement cylinder mounting plate (9-2), described span measurement is straight
Slidably connect span measurement slide block (9-13) on line guide rail (9-11), described span measurement guide track block (9-7) is connected with
Span measurement slide block block (9-8), the piston rod end of described span measurement cylinder (9-10) is connected with measures slide block with the span
(9-13) fixing the span measurement cylinder connecting and promoting plate (9-3), described span measurement cylinder promotes plate (9-3) top fixing even
Being connected to span measurement dial gauge heightening base (9-4), described span measurement dial gauge heightening base (9-4) top is fixedly connected with the span
Measurement dial gauge installing plate (9-5), described span measurement dial gauge installing plate (9-5) is provided with span measurement span guide plate
(9-9) and the span measurement gauge outfit of the gauge outfit that is used for fixing span measurement dial gauge (9-12) fixes seat (9-6), the described span is surveyed
The gauge outfit of amount dial gauge (9-12) passes through span measurement span guide plate (9-9).
6. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
Described bullet measurement assembly (4) include bullet measurement support install rebound (4-1) and be arranged on bullet measure support installed
Bullet measurement support (4-2) at cab apron (4-1) top, described bullet measurement support (4-2) is provided with bullet measurement cylinder peace
Dress plate (4-3), bullet measurement line slideway (4-12) and bullet measurement guide track block (4-9), described bullet measurement cylinder is installed
Bullet measurement cylinder (4-11) is installed on plate (4-3), described bullet measurement line slideway (4-12) slidably connects bullet
Measurement guide rail slide block (4-14), described bullet measurement guide track block (4-9) is connected with bullet measurement slide block block (4-10), institute
The piston rod end stating bullet measurement cylinder (4-11) is connected with the bullet that be connected fixing with bullet measurement guide rail slide block (4-14)
Measurement cylinder promotes plate (4-4), and described bullet measurement cylinder promotion plate (4-4) top is fixedly connected with bullet measurement dial gauge and increases
Dais (4-5), described bullet measurement dial gauge heightening base (4-5) top is fixedly connected with bullet measurement dial gauge installing plate (4-
6) it, described bullet measurement dial gauge installing plate (4-6) is provided with bullet measurement dial gauge (4-13) and be used for fixing bullet survey
The bullet measurement gauge outfit of the gauge outfit of amount dial gauge (4-13) fixes seat (4-8), the gauge outfit of described bullet measurement dial gauge (4-13)
End is connected with bullet measurement gauge outfit reference block (4-7).
7. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
Described afterbody measurement assembly (17) includes that afterbody measurement support is installed rebound (17-1) and is arranged on afterbody measurement support installation
Afterbody measurement support (17-2) at rebound (17-1) top, described afterbody measurement support (17-2) is provided with afterbody measurement gas
Cylinder installing plate (17-3), afterbody measurement line slideway (17-16) and afterbody measurement guide track block (17-12), described afterbody is measured
Being provided with afterbody measurement cylinder (17-15) on cylinder mounting plate (17-3), described afterbody measurement line slideway (17-16) is upper to slide
It is connected with afterbody measurement guide rail slide block (17-18), described afterbody measurement guide track block (17-12) is connected with afterbody measurement slide block
Block (17-13), the piston rod end of described afterbody measurement cylinder (17-15) is connected with measures guide rail slide block (17-with afterbody
18) fixing the afterbody measurement cylinder connecting and promoting plate (17-4), described afterbody measurement cylinder promotes plate (17-4) top fixing even
Being connected to afterbody measurement dial gauge heightening base (17-5), described afterbody measurement dial gauge heightening base (17-5) top is fixedly connected with tail
Portion's measurement dial gauge installing plate (17-6), described afterbody measurement dial gauge installing plate (17-6) is provided with afterbody measurement reset
Support seat (17-10), afterbody are measured dial gauge (17-17) and are used for fixing the afterbody of the gauge outfit of afterbody measurement dial gauge (17-17)
Measurement gauge outfit fixes seat (17-7), and the measurement of described afterbody resets to support and is connected with afterbody measurement reset sleeve on seat (17-10)
(17-8), described afterbody measurement dial gauge (17-17) gauge outfit end be connected with through afterbody measurement reset sleeve (17-8) and
Afterbody measurement resets and supports afterbody measurement reset lever (17-9) of seat (17-10), and the measurement of described afterbody resets and supports seat (17-
10) it is provided with in for supporting afterbody measurement linear bearing (17-14) installing afterbody measurement reset lever (17-9), described tail
Portion's measurement reset lever (17-9) is positioned on one section of afterbody measurement reset sleeve (17-8) and is set with afterbody measurement reset bullet
Spring (17-19), the end of described afterbody measurement reset lever (17-9) is connected with afterbody measurement gauge outfit reference block (17-11).
8. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
Described lowering or hoisting gear assembly (13) includes the motor adapter (13-11) being arranged in lifting base plate (13-1), and described motor turns
Fire-proof motor (13-17) for driving lift (13-18) to lift and fire-proof motor (13-are installed on joint chair (13-11)
17) decelerator (13-16) that output shaft connects and be used for supporting the clutch shaft bearing of the output shaft installing fire-proof motor (13-17)
(13-20), the quantity of described lift (13-18) is to be provided with lift between two and two lifts (13-18) to connect
Axle (13-6), the two ends of described lift connecting shaft (13-6) are respectively by two short connecting bushings (13-4) and two lifts
(13-18) lifting drive power shaft connects, by long connecting bushing (13-10) on the output shaft of described decelerator (13-16)
It is connected with lifting drive connecting shaft (13-9), described lifting drive connecting shaft (13-9) is connected with the first gear (13-8), institute
State and in lift connecting shaft (13-6), be connected with the second gear (13-13) engaging with the first gear (13-8), at the bottom of described lifting
It is provided with on plate (13-1) for supporting two the first rolling bearing units (13-15) installing lifting drive connecting shaft (13-9) and use
In two the second rolling bearing units (13-7) supporting installation lift connecting shaft (13-6), the top of described lift (13-18)
Being provided with lift top board (13-3), described lift top board (13-3) top is provided with jacking block (13-14) and lays respectively at top
Two lift footstocks (13-2) of block (13-14) both sides, described lifting base plate (13-1) is provided with sensor base (13-
12), described LOAD CELLS (13-19) is arranged in sensor base (13-12), described LOAD CELLS (13-19) top
Sensor backing plate (13-5) for contacting with sensor bulb (15) is installed, described sensor base (13-12), weighs
The quantity of sensor (13-19), sensor backing plate (13-5) and sensor bulb (15) is three.
9. according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, it is characterised in that:
The bottom of described self-powered platform (18) is connected with the jacking block seat (12) for being connected together on jacking block (13-14)；The described end
It is fixedly connected with the travel switch assembly for detecting the raising and lowering position of lift (13-18) on seat (1)
(14), described travel switch assembly (14) includes travel switch fixed plate (14-1) and for lift (13-18)
Rise the upper stroke switch (14-2) that detects of position and descending for detect the down position of lift (13-18)
Cheng Kaiguan (14-3), described upper stroke switch (14-2) is fixedly connected on travel switch fixed plate (14-1) top, described descending
Cheng Kaiguan (14-3) is fixedly connected on travel switch fixed plate (14-1) bottom；It is fixedly connected with on described lift (13-18)
With with when rising with upper stroke switch (14-2) touching the stroke limit touched with lower stroke switch (14-3) when declining
Plate (13-21).
10., according to a kind of guided missile quality center of mass described in claim 1 and appearance and size integrated measurer, its feature exists
In: two supporter roller seat (7-that described carriage assembly (7) includes bracket (7-1) and is fixedly connected on bracket (7-1) top
2) it, is provided with measurement and positioning block (7-6), described supporter roller seat (7-between described supporter roller seat (7-2) and bracket (7-1)
2) it is fixedly connected with deep groove ball bearing (7-7) on, be provided with between described deep groove ball bearing (7-7) and supporter roller seat (7-2)
Roller spacer ring (7-5), described deep groove ball bearing (7-7) is provided with roller shaft (7-3), the upper company of fixing of described roller shaft (7-3)
It is connected to roller (7-4).
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| CN201610389866.5A CN106091847B (en) | 2016-06-03 | 2016-06-03 | A kind of guided missile quality center of mass and appearance and size integrated measurer |
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| CN201610389866.5A CN106091847B (en) | 2016-06-03 | 2016-06-03 | A kind of guided missile quality center of mass and appearance and size integrated measurer |
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| CN112525020A (en) * | 2020-11-18 | 2021-03-19 | 中国人民解放军32181部队 | Shot rotating equipment |
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| CN109883277B (en) * | 2019-04-02 | 2020-05-15 | 重庆航天工业有限公司 | Automatic chamber closing detection machine |
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| CN110553555A (en) * | 2018-09-25 | 2019-12-10 | 湖北航鹏化学动力科技有限责任公司 | Bore closing detection device for rocket projectile with large length-diameter ratio |
| CN110553555B (en) * | 2018-09-25 | 2021-07-30 | 湖北航鹏化学动力科技有限责任公司 | Bore closing detection device for rocket projectile with large length-diameter ratio |
| CN112525020A (en) * | 2020-11-18 | 2021-03-19 | 中国人民解放军32181部队 | Shot rotating equipment |
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| CN106091847B (en) | 2018-03-09 |
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