CN109986501A - A kind of aircraft stock class component assembly equipment and its application method - Google Patents
A kind of aircraft stock class component assembly equipment and its application method Download PDFInfo
- Publication number
- CN109986501A CN109986501A CN201910404170.9A CN201910404170A CN109986501A CN 109986501 A CN109986501 A CN 109986501A CN 201910404170 A CN201910404170 A CN 201910404170A CN 109986501 A CN109986501 A CN 109986501A
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- aircraft
- bracket
- stock class
- hydraulic
- adjustment
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B27/00—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The invention belongs to mechanical assembly technique field, it is related to a kind of aircraft stock class component assembly equipment and its application method.The device includes automatic delivery drive system, fluid power system and mechanical alignment system；Automatic delivery drive system includes universal knob, driving handle, Electric Motor Wheel, universal rolling wheel and automatically controlled dress；Fluid power system includes base bracket, sliding support, hydraulic strut device, pressure rod, hydraulic hand-pump, fuel tank and groove profile sliding rail, is adjusted for lifting one end of long component of rod category, and in inclination angle, up and down direction；Mechanical alignment system includes adjustment bracket, swivel bearing device, multi-directional rotation slide tray device, cylinder sliding rail, precision lead screw, baffle, the fixed ground pin device of gyrocompass and position, for carrying out accurate adjustment in the lateral direction to long component of rod category, reaches part assembling hole and aircraft pilot hole is overlapped.The invention patent mechanical structure is novel, the degree of automation is strong, and comprehensive assemble ability is strong.
Description
Technical field
The invention belongs to mechanical assembly technique field, it is related to a kind of aircraft stock class component assembly equipment and its user
Method.
Background technique
For aircraft in assembling process, there are many long component of rod category for needing to assemble, and weight and installation site are also each not phase
Together, but the weight of some long component of rod category has reached 100kg or more, in normal assembling process, needs this stock class zero first
Part lifts to the installation site of aircraft with about 8 people, then gets out relevant components again, and by 8 people by this stock class
Part, which is tilted more than 45 degree of angles, raises one end, then upper and lower, left and right adjustment stock class part assembling hole installation site,
And the big axis connection of pilot hole of the top pilot hole of long component of rod category and aircraft is got up by a people.But whole installation process by
It is especially big in the stock class pts wt, by the limit of part assembling hole and aircraft pilot hole assembly precision and installation space size
System, entire assembling process need lift the long component of rod category or so about 1 hour of 8 people, and in tilt angle, up and down
Be adjusted on direction, final adjustment is concentric, and by the component assembly to aircraft, not only time-consuming for such installation method,
And very big influence is also resulted in for the safety of installer, once someone for a long time lift it is motionless, it is possible to make zero
Part one end tilts and rolls down on ground, and part is easy to break, but also is easy to injure operator, causes industrial accident, sternly
Ghost image rings personal security and Aircraft Production period.
For these reasons, the aircraft stock class component assembly equipment has been invented, the tool structure is novel, and it is easy to operate,
The long component of rod category of aircraft can be adjusted for a long time, accurate centering from multi-faceted, and not need manpower and lift for a long time
It rises, labor intensity and personnel amount is greatly reduced, and improve working efficiency.
Summary of the invention
In view of the problems of the existing technology, the present invention proposes a kind of aircraft stock class component assembly equipment and its user
Method can adapt to the long component of rod category that weight is big, contour structures are complicated and install in narrow particular job region, stringent to protect
Demonstrate,prove accuracy, the high efficiency, low-intensity of part installation.
The technical solution of the present invention is as follows:
A kind of aircraft stock class component assembly equipment, including drive system, fluid power system and mechanical tune are consigned automatically
Whole system；Automatic delivery drive system includes universal knob 1, driving handle 2, Electric Motor Wheel 15, universal rolling wheel 17 and electric control gear
19, for providing delivery power；Fluid power system includes base bracket 3, sliding support 4, hydraulic strut device 11, adds
Compression bar 13, hydraulic hand-pump 14, fuel tank 18 and groove profile sliding rail 20, for lifting one end of long component of rod category, and inclination angle, on
Lower section is adjusted upwards, and long component of rod category is made to reach designated mounting position, lifts for a long time instead of manpower and adjustment is brought
Installation it is inconvenient；Mechanical alignment system includes adjustment bracket 5, swivel bearing device 6, multi-directional rotation slide tray device 7, circle
The fixed ground pin device 16 in column sliding rail 8, precision lead screw 9, baffle 10, gyrocompass 12 and position, is used for long component of rod category on a left side
Accurate adjustment is carried out in right direction, reaches part assembling hole and aircraft pilot hole is overlapped；
The base bracket 3 is cuboid framework, and the groove profile sliding rail 20 is set to 3 upper end of base bracket, the universal drawing
1 bottom end of hand is fixed on 3 right side of base bracket, and the driving handle 2 is mounted on 1 top of universal knob；3 bottom of base bracket
Electric Motor Wheel 15 is installed in left side, and universal rolling wheel 17 is installed on right side, and the fixed ground pin device 16 in 4 positions is installed at middle part；The position is solid
Determine ground pin device 16 can up and down adjustment, it is tight to contiguously face paste for adjusting, guarantee equipment cannot be slided on ground；The electricity
Control device 19 is fixed on right side in base bracket 3, for providing power for automatic delivery drive system；The hydraulic hand-pump 14
It is fixed on left side in base bracket 3 with fuel tank 18, for providing power for fluid power system, hydraulic hand-pump 14, which is equipped with, to be added
Compression bar 13；
The adjustment bracket 5 is rectangular frame, and 3 left side upper end of base bracket is fixed in left end, and right end passes through sliding branch
Support arrangement 4 is connect with groove profile sliding rail 20；The sliding support 4 be rectangular frame, upper end by swivel bearing device 6 with
It adjusts bracket 5 to connect, rotatable, lower end edge groove profile sliding rail 20 slides, for adjusting the upper and lower position of adjustment bracket 5；The liquid
5 left side of adjustment bracket is fixed in pressure 11 one end of brace apparatus, and the other end is fixed on sliding support lower end, for controlling sliding
Sliding of the support device 4 on groove profile sliding rail 20；The baffle 10 is set to 5 left side top of adjustment bracket, for being close to stock class
One end of part；The adjustment bracket 5 is equipped with parallel precision lead screw 9 and cylinder sliding rail 8, precision lead screw 9 and cylinder sliding rail 8
It is equipped with multi-directional rotation slide tray device 7；The multi-directional rotation slide tray device 7 is equipped with bracket, for placing
Long component of rod category；Described 9 one end of precision lead screw is equipped with gyrocompass 12, and it is sliding to adjust multi-directional rotation by adjusting gyrocompass 12
Dynamic position of the pallet apparatus 7 on precision lead screw 9, realizes the adjustment of long component of rod category left-right position, makes stock class component assembly
Hole and the accurate centering of aircraft pilot hole.
A kind of application method of aircraft stock class component assembly equipment is as follows:
Long component of rod category is lifted and is placed in the bracket of multi-directional rotation slide tray device 7, makes stock class by the first step
One end of part is close to baffle 10, opens electric control gear 19, is transported the part by controlling universal knob 1, driving handle 2
To the designated mounting position of aircraft, closes electric control gear 19 and switch；
Second step after reaching designated mounting position, the fixed ground pin device 16 in 4 positions is adjusted to contact ground and is close to,
Guarantee that the aircraft stock class component assembly equipment cannot be slided on ground；
The hydraulic selector of hydraulic hand-pump 14 is rotated to " lifting " position by third step, after opening " oil-supplying switch ", operation
Person shakes pressure rod 13, and the centering situation of stock class part assembling hole and aircraft pilot hole is observed by another operator；
4th step, when the installation end of long component of rod category is raised to the position of aircraft pilot hole, left and right directions is variant, then
Two gyrocompass 12 are adjusted, stock class part assembling hole and the accurate centering of aircraft pilot hole are made；
5th step, operator close " oil-supplying switch " of hydraulic hand-pump 14, then rotate to hydraulic selector " in
It is vertical " position, another operator connects stock class part assembling hole and aircraft pilot hole with big axis；
6th step, after big axis assembles, the hydraulic selector of hydraulic hand-pump 14 is rotated to " putting down " position by operator,
It opens " oil-supplying switch ", drops to the aircraft stock class component assembly equipment and be detached from long component of rod category, then by 4 positions
It sets fixed ground pin device 16 to be adjusted to be detached from ground, and the aircraft stock class component assembly equipment is moved to battery limits.
Beneficial effects of the present invention:
(1) the invention patent mechanical structure is novel, the degree of automation is strong, and comprehensive assemble ability is strong, so that entirely assembling
Journey personnel amount by 8 original people more than, be reduced to 3 people, labor intensity is reduced to original 1/5th, working efficiency and peace
Dress precision is increased substantially.
(2) equipment uses fluid pressure drive device, so that the installation end of long component of rod category is during lifting, it is flexible
Rise, specified mounting height may finally be reached, prevented to be lifted adjustment installation site for a long time as more people and caused by it is long
Component of rod category be easy slide and caused by industrial accident.
(3) equipment additionally uses the adjustment device that two gyrocompass 12, cylinder sliding rail 8, precision lead screw 9 form, and makes
Its long component of rod category can be adjusted after reaching designated mounting height by the flexibility of gyrocompass 12 in the lateral direction, into
One step ensure that installation accuracy.
(4) equipment uses electronic delivery drive system, can be moved to 100 kilograms or so of long component of rod category any
Position, instead of there are more people to carry big weight part originally and caused by hidden danger and quality problems.
(5) three systems that the equipment uses are independent mutually, are well defined, cheap, the later maintenance for equipment
It is very convenient with maintaining.
(6) flexibility of the equipment is high, by replacing the structure of multi-directional rotation slide tray device 7, may also adapt to
The inclination of long component of rod category of various shapes is installed.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of aircraft stock class component assembly equipment；
In figure: 1 universal knob；2 driving handles；3 base brackets；4 sliding supports；5 adjustment brackets；6 swivel bearings
Device；7 multi-directional rotation slide tray devices；8 cylinder sliding rails；9 precision lead screws；10 baffles；11 hydraulic strut devices；12 rotations
Compass；13 pressure rods；14 hydraulic hand-pumps；15 Electric Motor Wheels；Ground pin device is fixed in 16 positions；17 universal rolling wheels；18 fuel tanks；19 electricity
Control device；20 groove profile sliding rails.
Specific embodiment
Below in conjunction with attached drawing and technical solution, specific embodiments of the present invention are further illustrated.
As shown in Figure 1, a kind of aircraft stock class component assembly equipment, including drive system, hydraulic-driven system are consigned automatically
System and mechanical alignment system；Automatic delivery drive system includes 1, driving handle 2, Electric Motor Wheel 15, universal rolling wheel 17 of universal knob
With electric control gear 19, power is consigned for providing；Fluid power system includes base bracket 3, sliding support 4, hydraulic support
Lever apparatus 11, pressure rod 13, hydraulic hand-pump 14, fuel tank 18 and groove profile sliding rail 20, for lifting one end of long component of rod category, and
It is adjusted in inclination angle, up and down direction, long component of rod category is made to reach designated mounting position, lifted for a long time instead of manpower
It is inconvenient with adjustment bring installation；Mechanical alignment system includes adjustment bracket 5, swivel bearing device 6, multi-directional rotation sliding support
The fixed ground pin device 16 in disk device 7, cylinder sliding rail 8, precision lead screw 9, baffle 10, gyrocompass 12 and position, for stock
Class part carries out accurate adjustment in the lateral direction, reaches part assembling hole and aircraft pilot hole is overlapped；
The base bracket 3 is cuboid framework, and the groove profile sliding rail 20 is set to 3 upper end of base bracket, the universal drawing
1 bottom end of hand is fixed on 3 right side of base bracket, and the driving handle 2 is mounted on 1 top of universal knob；3 bottom of base bracket
Electric Motor Wheel 15 is installed in left side, and universal rolling wheel 17 is installed on right side, and the fixed ground pin device 16 in 4 positions is installed at middle part；The position is solid
Determine ground pin device 16 can up and down adjustment, it is tight to contiguously face paste for adjusting, guarantee equipment cannot be slided on ground；The electricity
Control device 19 is fixed on right side in base bracket 3, for providing power for automatic delivery drive system；The hydraulic hand-pump 14
It is fixed on left side in base bracket 3 with fuel tank 18, for providing power for fluid power system, hydraulic hand-pump 14, which is equipped with, to be added
Compression bar 13；
The adjustment bracket 5 is rectangular frame, and 3 left side upper end of base bracket is fixed in left end, and right end passes through sliding branch
Support arrangement 4 is connect with groove profile sliding rail 20；The sliding support 4 be rectangular frame, upper end by swivel bearing device 6 with
It adjusts bracket 5 to connect, rotatable, lower end edge groove profile sliding rail 20 slides, for adjusting the upper and lower position of adjustment bracket 5；The liquid
5 left side of adjustment bracket is fixed in pressure 11 one end of brace apparatus, and the other end is fixed on sliding support lower end, for controlling sliding
Sliding of the support device 4 on groove profile sliding rail 20；The baffle 10 is set to 5 left side top of adjustment bracket, for being close to stock class
One end of part；The adjustment bracket 5 is equipped with parallel precision lead screw 9 and cylinder sliding rail 8, precision lead screw 9 and cylinder sliding rail 8
It is equipped with multi-directional rotation slide tray device 7；The multi-directional rotation slide tray device 7 is equipped with bracket, for placing
Long component of rod category；Described 9 one end of precision lead screw is equipped with gyrocompass 12, and it is sliding to adjust multi-directional rotation by adjusting gyrocompass 12
Dynamic position of the pallet apparatus 7 on precision lead screw 9, realizes the adjustment of long component of rod category left-right position, makes stock class component assembly
Hole and the accurate centering of aircraft pilot hole.
A kind of application method of aircraft stock class component assembly equipment is as follows:
Long component of rod category is lifted and is placed in the bracket of multi-directional rotation slide tray device 7, makes stock class by the first step
One end of part is close to baffle 10, opens electric control gear 19, is transported the part by controlling universal knob 1, driving handle 2
To the designated mounting position of aircraft, closes electric control gear 19 and switch；
Second step after reaching designated mounting position, the fixed ground pin device 16 in 4 positions is adjusted to contact ground and is close to,
Guarantee that the aircraft stock class component assembly equipment cannot be slided on ground；
The hydraulic selector of hydraulic hand-pump 14 is rotated to " lifting " position by third step, after opening " oil-supplying switch ", operation
Person shakes pressure rod 13, and the centering situation of stock class part assembling hole and aircraft pilot hole is observed by another operator；
4th step, when the installation end of long component of rod category is raised to the position of aircraft pilot hole, left and right directions is variant, then
Two gyrocompass 12 are adjusted, stock class part assembling hole and the accurate centering of aircraft pilot hole are made；
5th step, operator close " oil-supplying switch " of hydraulic hand-pump 14, then rotate to hydraulic selector " in
It is vertical " position, another operator connects stock class part assembling hole and aircraft pilot hole with big axis；
6th step, after big axis assembles, the hydraulic selector of hydraulic hand-pump 14 is rotated to " putting down " position by operator,
It opens " oil-supplying switch ", drops to the aircraft stock class component assembly equipment and be detached from long component of rod category, then by 4 positions
It sets fixed ground pin device 16 to be adjusted to be detached from ground, and the aircraft stock class component assembly equipment is moved to battery limits.
The present invention is applied to assemble certain weight aboard the long component of rod category of 100KG or more the case where, holds up zero
While part, can for a long time, the angle of assembling of the big weight part of multi-faceted adjustment, and then guarantee assembly precision, improve work
Efficiency alleviates labor intensity and personnel amount.
In addition to the implementation, the present invention can also have other embodiments.It is all to use equivalent substitution or equivalent transformation shape
At technical solution, fall within the scope of protection required by the present invention.
Claims (2)
1. a kind of aircraft stock class component assembly equipment, which is characterized in that the aircraft stock class component assembly equipment includes
Automatic delivery drive system, fluid power system and mechanical alignment system；Automatic delivery drive system include universal knob (1),
Driving handle (2), Electric Motor Wheel (15), universal rolling wheel (17) and electric control gear (19), for providing delivery power；Hydraulic-driven system
System include base bracket (3), sliding support (4), hydraulic strut device (11), pressure rod (13), hydraulic hand-pump (14),
Fuel tank (18) and groove profile sliding rail (20), are adjusted for lifting one end of long component of rod category, and in inclination angle, up and down direction
It is whole, so that long component of rod category is reached designated mounting position, it is inconvenient to lift and adjust for a long time bring installation instead of manpower；It is mechanical
Adjustment system includes adjustment bracket (5), swivel bearing device (6), multi-directional rotation slide tray device (7), cylinder sliding rail
(8), precision lead screw (9), baffle (10), gyrocompass (12) and position are fixed ground pin device (16), for long component of rod category
Accurate adjustment is carried out in the lateral direction, reaches part assembling hole and aircraft pilot hole is overlapped；
The base bracket (3) is cuboid framework, and the groove profile sliding rail (20) is set to base bracket (3) upper end, described universal
Knob (1) bottom end is fixed on the right side of base bracket (3), and the driving handle (2) is mounted on universal knob (1) top；The base
Plinth bracket (3) bottom left installs Electric Motor Wheel (15), and universal rolling wheel (17) are installed on right side, and the fixed lower margin in 4 positions is installed at middle part
Device (16)；The position fixed ground pin device (16) can up and down adjustment, it is tight to contiguously face paste for adjusting, guarantee equipment
It cannot be slided on ground；The electric control gear (19) is fixed on right side in base bracket (3), for being automatic delivery drive system
Power is provided；The hydraulic hand-pump (14) and fuel tank (18) are fixed on left side in base bracket (3), for being hydraulic-driven system
System provides power, and hydraulic hand-pump (14) is equipped with pressure rod (13)；
The adjustment bracket (5) is rectangular frame, and upper end on the left of base bracket (3) is fixed in left end, and right end passes through sliding branch
Support arrangement (4) is connect with groove profile sliding rail (20)；The sliding support (4) is rectangular frame, and upper end passes through swivel bearing
Device (6) is connect with adjustment bracket (5), rotatable, lower end edge groove profile sliding rail (20) sliding, for adjusting adjustment bracket (5)
Upper and lower position；Described hydraulic strut device (11) one end is fixed on the left of adjustment bracket (5), and the other end is fixed on sliding support dress
Lower end is set, for controlling sliding of the sliding support (4) on groove profile sliding rail (20)；The baffle (10) is set to adjustment bracket
(5) left side top, for being close to one end of long component of rod category；Adjustment bracket (5) be equipped with parallel precision lead screw (9) and
Cylinder sliding rail (8), precision lead screw (9) and cylinder sliding rail (8) are equipped with multi-directional rotation slide tray device (7)；It is described multi-party
Position rotational slide pallet apparatus (7) is equipped with bracket, for placing long component of rod category；Described precision lead screw (9) one end is equipped with rotation
Turn compass (12), adjusts multi-directional rotation slide tray device (7) on precision lead screw (9) by adjusting gyrocompass (12)
The adjustment of long component of rod category left-right position is realized in position, makes stock class part assembling hole and the accurate centering of aircraft pilot hole.
2. a kind of application method of aircraft stock class component assembly equipment, it is characterised in that following steps:
Long component of rod category is lifted and is placed in the bracket of multi-directional rotation slide tray device (7), makes stock class zero by the first step
One end of part is close to baffle (10), is opened electric control gear (19), by control universal knob (1), driving handle (2) by this zero
Part transports the designated mounting position of aircraft, closes electric control gear (19) switch；
Second step after reaching designated mounting position, (4) a position fixed ground pin device (16) is adjusted to contact ground and is close to,
Guarantee that the aircraft stock class component assembly equipment cannot be slided on ground；
The hydraulic selector of hydraulic hand-pump (14) is rotated to " lifting " position by third step, after opening " oil-supplying switch ", operator
It shakes pressure rod (13), the centering situation of stock class part assembling hole and aircraft pilot hole is observed by another operator；
4th step, when the installation end of long component of rod category is raised to the position of aircraft pilot hole, left and right directions is variant, then adjusts
Two gyrocompass (12), make stock class part assembling hole and the accurate centering of aircraft pilot hole；
5th step, operator close " oil-supplying switch " of hydraulic hand-pump (14), and hydraulic selector is then rotated to " neutrality "
Position, another operator are connected stock class part assembling hole and aircraft pilot hole with big axis；
6th step, after big axis assembles, the hydraulic selector of hydraulic hand-pump (14) is rotated to " putting down " position by operator, is beaten
" oil-supplying switch " is opened, the aircraft stock class component assembly equipment is dropped to and is detached from long component of rod category, then by 4 positions
Fixed ground pin device (16) are adjusted to be detached from ground, and the aircraft stock class component assembly equipment is moved to battery limits.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910404170.9A CN109986501B (en) | 2019-05-16 | 2019-05-16 | Airplane long rod part assembly equipment and application method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910404170.9A CN109986501B (en) | 2019-05-16 | 2019-05-16 | Airplane long rod part assembly equipment and application method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109986501A true CN109986501A (en) | 2019-07-09 |
| CN109986501B CN109986501B (en) | 2023-07-28 |
Family
ID=67136391
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910404170.9A Active CN109986501B (en) | 2019-05-16 | 2019-05-16 | Airplane long rod part assembly equipment and application method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109986501B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406696A (en) * | 2019-08-07 | 2019-11-05 | 沈阳飞机工业（集团）有限公司 | Aircraft landing system intercepts the multi-functional resetting equipment of part |
| CN115626782A (en) * | 2022-10-20 | 2023-01-20 | 江西昌河航空工业有限公司 | Uniform pressing device and method for large-curvature front windshield of airplane |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202225188U (en) * | 2011-09-15 | 2012-05-23 | 北京卫星制造厂 | Five-degree-of-freedom adjustment platform for assembly of satellite capsule plate |
| US8911194B1 (en) * | 2011-05-18 | 2014-12-16 | Tronair, Inc. | Softcapture cradle |
| CN106514545A (en) * | 2016-10-26 | 2017-03-22 | 奇瑞汽车股份有限公司 | Inclined hole pressing device |
| CN206373564U (en) * | 2016-12-15 | 2017-08-04 | 浙江海洋大学东海科学技术学院 | A kind of adjustment structure of windshield positioning tool |
| CN108942201A (en) * | 2018-08-03 | 2018-12-07 | 郭芬 | A kind of converter transformer valve-side sleeve centralising device |
| CN210099893U (en) * | 2019-05-16 | 2020-02-21 | 沈阳飞机工业（集团）有限公司 | Aircraft stock class part rigging equipment |
-
2019
- 2019-05-16 CN CN201910404170.9A patent/CN109986501B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8911194B1 (en) * | 2011-05-18 | 2014-12-16 | Tronair, Inc. | Softcapture cradle |
| CN202225188U (en) * | 2011-09-15 | 2012-05-23 | 北京卫星制造厂 | Five-degree-of-freedom adjustment platform for assembly of satellite capsule plate |
| CN106514545A (en) * | 2016-10-26 | 2017-03-22 | 奇瑞汽车股份有限公司 | Inclined hole pressing device |
| CN206373564U (en) * | 2016-12-15 | 2017-08-04 | 浙江海洋大学东海科学技术学院 | A kind of adjustment structure of windshield positioning tool |
| CN108942201A (en) * | 2018-08-03 | 2018-12-07 | 郭芬 | A kind of converter transformer valve-side sleeve centralising device |
| CN210099893U (en) * | 2019-05-16 | 2020-02-21 | 沈阳飞机工业（集团）有限公司 | Aircraft stock class part rigging equipment |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406696A (en) * | 2019-08-07 | 2019-11-05 | 沈阳飞机工业（集团）有限公司 | Aircraft landing system intercepts the multi-functional resetting equipment of part |
| CN115626782A (en) * | 2022-10-20 | 2023-01-20 | 江西昌河航空工业有限公司 | Uniform pressing device and method for large-curvature front windshield of airplane |
| CN115626782B (en) * | 2022-10-20 | 2024-01-23 | 江西昌河航空工业有限公司 | Uniform pressing device and method for large-curvature front windshield of airplane |
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| Publication number | Publication date |
|---|---|
| CN109986501B (en) | 2023-07-28 |
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