CN110271688A - A kind of transporter large-scale antenna dome installation posture adjustment equipment - Google Patents
A kind of transporter large-scale antenna dome installation posture adjustment equipment Download PDFInfo
- Publication number
- CN110271688A CN110271688A CN201910412523.XA CN201910412523A CN110271688A CN 110271688 A CN110271688 A CN 110271688A CN 201910412523 A CN201910412523 A CN 201910412523A CN 110271688 A CN110271688 A CN 110271688A
- Authority
- CN
- China
- Prior art keywords
- vehicle frame
- layer
- fixed
- screw rod
- axis control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Support Of Aerials (AREA)
Abstract
The embodiment of the present invention provides a kind of transporter Large Radar cover installation posture adjustment equipment, comprising: lifting rack-layer vehicle frame 01, posture adjustment car body layer vehicle frame 02, guiding movement and fixation kit layer vehicle frame 03；Wherein, described 01 layer of vehicle frame of lifting rack-layer vehicle frame uses envelop-type structure, and described 01 layer of vehicle frame of lifting rack-layer vehicle frame is mounted on 02 layer of vehicle frame top of posture adjustment car body layer vehicle frame；Posture adjustment car body layer 02 layer of vehicle frame of vehicle frame uses multilayer vehicle frame stepped construction；02 layer of vehicle frame of posture adjustment car body layer vehicle frame can be in X (course direction), Y (spanwise) or Z (vertical direction layer vehicle frame linear movement, or in the rotary motion of X/Y plane and XZ plane；The 03 layer of vehicle frame setting of guiding movement and fixation kit layer vehicle frame for the short-distance movement of the equipment, fixation and enters initial installation station in lower car body.
Description
Technical field
The invention belongs to aero-manufacturing technology fields, are related to a kind of aircraft Large Radar cover installation posture adjustment equipment.
Background technique
Prior art scenario: the fixed large-scale overhead guard of certain two supporting leg of model early warning plane middle fuselage support, overhead guard shape are
Spherical surface body by DOME, radome and is defended exceedingly high irdome and is formed, and the pairing of radome and DOME are the important of overhead guard
One of assembly process.Before, beyond example, the installation posture adjustment equipment for developing large-scale antenna dome is for the installation of this large-scale antenna dome
This model technological equipment researches and develops one of big event.
Technical situation after innovation: pairing installation vehicle, which has, fast moves function, protects type frame by lifting, posture adjustment car body, moves
The parts such as dynamic and fixed device form, and body construction designs the adjustment function of top to bottom, left and right, front and rear direction linear movement and rotation
Can, posture adjustment car body uses multistory frame stepped construction, and linear guide and shaft is arranged, makes day by the regulating device of all directions
Irdome protects type frame and antenna house is driven to complete pairing installment work.Pairing installs vehicle province simple to operate, safe and reliable, time saving
Power.
Summary of the invention
Goal of the invention: provide it is a kind of meet transporter Large Radar cover posture adjustment assembly, and take into account working efficiency and labour
The method and equipment of intensity.The technical solution of the invention is as follows, suspender and car body integration；It fast moves；Product can be several
Controllable adjustment is carried out in a direction and plane.
In a first aspect, providing a kind of transporter Large Radar cover installation posture adjustment equipment, comprising: mast-up 01, posture adjustment car body
02, guiding movement and fixation kit 03；
Wherein, the mast-up 01 uses envelop-type structure, and the mast-up 01 is mounted on 02 top of posture adjustment car body；Posture adjustment
Car body 02 uses multilayer vehicle frame stepped construction；Posture adjustment car body 02 can be in X (course direction), Y (spanwise) or Z (vertical direction
Linear movement, or in the rotary motion of X/Y plane and XZ plane；Guiding movement and the setting of fixation kit 03 are used in lower car body
In the short-distance movement of the equipment, fixation and enter initial installation station.
Further, mast-up 01 includes frame body 01-01, end-fitting 01-02, the 01-03 that holds down assembly, hanging ring 01-04；
Wherein, end-fitting 01-02 is fixed on the end on the outside of frame body 01-01, for connecting the reserved threaded hole of cover；
The hold down assembly bottom end of 01-03 is fixed on the inside both ends of frame body 01-01；Antenna house is fixed on frame body by the 01-03 that holds down assembly
In the space that 01-01 is surrounded, hanging ring 01-04 is fixed on the outside of frame body 01-01.
Further, the 01-03 that holds down assembly include protective layer 01-03-01, wooden block 01-03-02, plate comer pieces 01-03-03,
First screw rod 01-03-04 and handwheel 01-03-05 with sleeve；Protective layer 01-03-01 is fixed at the top of wooden block 01-03-02,
The deformation of product is prevented, plate comer pieces 01-03-03 is fixed on the bottom of wooden block 01-03-02, and the first screw rod 01-03-04 is fixed on
The outer surface of plate comer pieces 01-03-03；The external screw thread of the internal screw thread of handwheel 01-03-05 with sleeve and the first screw rod 01-03-04
Cooperation realizes that the first screw rod 01-03-04 stretches in sleeve.
Further, posture adjustment car body 02 includes: first layer vehicle frame 02-01, second layer vehicle frame 02-02, third layer vehicle frame 02-
03, the 4th layer of vehicle frame 02-04, five layers of vehicle frame 02-05, X/Y plane rotational control assemblies 02-06, X-axis control assembly 02-07, Z axis
Control assembly 02-08, Y-axis control assembly 02-09；
Wherein, X/Y plane rotational control assemblies 02-06 be fixed on first layer vehicle frame 02-01 and second layer vehicle frame 02-02 it
Between, X/Y plane rotational control assemblies 02-05 is adjusted, rotates one layer of vehicle frame along X/Y plane relative to two layers of vehicle frame；X-axis control assembly
02-07 is fixed between second layer vehicle frame 02-02 and third layer vehicle frame 02-03, is adjusted X-axis control assembly 02-07, is made two layers of vehicle
Frame moves along the x axis relative to three layers of vehicle frame；Z axis control assembly 02-08 is fixed on third layer vehicle frame 02-03 and the 4th layer of vehicle frame
Between 02-04, Z axis control assembly 02-08 is adjusted, moves three layers of vehicle frame along Z-direction relative to four layers of vehicle frame, while also in XZ
Plane small angle rotation；Y-axis control assembly 02-09 is fixed between the 4th layer of vehicle frame 02-04 and five layers of vehicle frame 02-05, adjusts Y
Axis control assembly 02-09 moves four layers of vehicle frame along the y axis relative to five layers of vehicle frame.
Further, X/Y plane rotational control assemblies 02-06 include: castor 02-06-01, it is dead axle 02-06-02, first straight
Line guide rail 02-06-03, the second screw rod 02-06-04, handwheel sleeve 02-06-05.Wherein castor 02-06-01 is with dead axle 02-06-
02 is in the symmetrical centre of first layer vehicle frame 02-01, and castor 02-06-01 is in the first layer lower part vehicle frame 02-01 with dead axle 02-06-
02 is center of circle circle distribution；First straight line guide rail 02-06-03 is fixed on the lower part side of first layer vehicle frame 02-01, first straight line
One end of the sliding block of guide rail 02-06-03 and the second screw rod 02-06-04 are fixed, and handwheel sleeve 02-06-05 is fixed on second layer vehicle
The side surface upper part of body 02-02, the second screw rod 02-06-04 and handwheel sleeve 02-06-05 cooperation, make the second screw rod 02-06-04 exist
It stretches in handwheel sleeve 02-06-05, so that sliding block slides in first straight line guide rail 02-06-03, pushes first layer vehicle frame 02-
01 along System of Rotating about Fixed Axis.
Further, X-axis control assembly 02-07 includes second straight line guide rail 02-07-01, third screw rod 02-07-02, spiral shell
Cover 02-07-03)；
Wherein, second straight line guide rail 02-07-01 is fixed between second layer vehicle frame 02-02 and third layer vehicle frame 02-03
Opposite side end, swivel nut 02-07-03) it is fixed on the centre of the bottom second layer vehicle frame 02-02；Second straight line guide rail 02-07-01 with
One end of third screw rod 02-07-02 is fixed, third screw rod 02-07-02 and swivel nut 02-07-03) cooperation, make third screw rod 02-
07-02 stretches in swivel nut 02-07-03), moves second layer vehicle frame 02-02 on second straight line guide rail 02-07-01.
Further, Y-axis control assembly 02-09 is identical as X-axis control assembly 02-07 composed structure, Y-axis control assembly
The opposite side end between the 4th layer of vehicle frame 02-04 and layer 5 vehicle frame 02-05 is arranged in 02-09.
Further, first layer vehicle frame 02-01, second layer vehicle frame 02-02, third layer vehicle frame 02-03, the 4th layer of vehicle frame
The height of 02-04 and layer 5 vehicle frame 02-05 successively reduce.
The utility model has the advantages that transporter Large Radar cover of the present invention installs attitude-adjusting method compared with art methods and equipment
And equipment uses simple control means, realizes the controllability that product is assembled in posture adjustment, effectively improves aircraft Large Radar
The precision of cover posture adjustment assembly, shortens the posture adjustment assembly period of transporter Large Radar cover, the labour of operator is effectively reduced
Intensity improves work efficiency.
Detailed description of the invention
The present invention includes 7 attached drawings, and attached drawing and Detailed description of the invention are as follows:
Fig. 1 is aircraft Large Radar cover installation posture adjustment equipment overall structure diagram of the present invention；
Fig. 2 is mast-up structural schematic diagram；
Fig. 3 is the structural schematic diagram that holds down assembly；
Fig. 4 is posture adjustment body construction schematic diagram；
Fig. 5 is X/Y plane rotational control assemblies structural schematic diagram；
Fig. 6 is X-axis control assembly structural schematic diagram；
Fig. 7 is the structural schematic diagram of guiding movement and fixation kit.
Wherein, 01 be mast-up, 01-01 be frame body, 01-02 be end-fitting, 01-03 be hold down assembly, 01-03-01
It is protective layer, 01-03-02 be wooden block, 01-03-03 be plate comer pieces, 01-03-04 be screw rod, 01-03-05 is the hand with sleeve
Wheel, 01-04 be hanging ring, 02 be posture adjustment vehicle frame, 02-01 be one layer of vehicle frame, 02-02 be two layers of vehicle frame, 02-03 be three layers of vehicle frame,
It is five layers of vehicle frame, 02-06 be X/Y plane rotational control assemblies, 02-06-01 is castor, 02- that 02-04, which is four layers of vehicle frame, 02-05,
It is linear guide, 02-06-04 be screw rod, 02-06-05 be handwheel sleeve, 02-07 is X-axis control that 06-02, which is dead axle, 02-06-03,
Component processed, 02-07-01 be linear guide, 02-07-02 be screw rod, 02-07-03 be swivel nut, 02-08 be Z axis control assembly,
02-09 is Y-axis control assembly, 03 is guiding movement and fixation kit, 03-01 be draw bar, 03-02 be castor, 03-03 are branch
Foot.
Specific implementation
The present invention is described in further details below.
Referring to Fig. 1, a kind of transporter Large Radar cover installation attitude-adjusting method of the present invention and equipment comprising mast-up
01,03 3 posture adjustment car body 02, guiding movement and fixation kit parts form.The mast-up 01 uses envelop-type structure, can
Product to be come out to from container hanging in the case where not destroying product shape and is mounted on 02 top of posture adjustment car body；The tune
Appearance car body 02 uses multilayer vehicle frame stepped construction, completes posture adjustment car body 02 in X (boat by the adjusting screw component of all directions
To direction), Y (spanwise), Z (vertical direction linear movement and X/Y plane and XZ plane rotary motion；Guiding movement and
The setting of fixation kit 03 is in lower car body, for installing the initial installation station of short-distance movement, fixation and entrance of vehicle.
Referring to Fig. 2, the mast-up 01 is by frame body 01-01, end-fitting 01-02, the 01-03 that holds down assembly, hanging ring 01-
04 equal composition.Wherein end-fitting 01-02 is fixed on the end on the outside of frame body 01-01, for connecting the reserved threaded hole of cover；
The 01-03 that holds down assembly, which is individually fixed in frame body 01-01, must control two sides up and down, indeformable for protective enclosure.
Referring to Fig. 3, the 01-03 that holds down assembly is provided at 8 altogether, by protective layer 01-03-01, wooden block 01-03-02,
Plate comer pieces 01-03-03, the first screw rod 01-03-04 and with sleeve handwheel 01-03-05 composition；Protective layer 01-03-01 is fixed
At the top of wooden block 01-03-02, the deformation of product can be prevented.
Referring to Fig. 4, the posture adjustment car body 02 is by first layer vehicle frame 02-01, second layer vehicle frame 02-02, third layer vehicle frame
02-03, the 4th layer of vehicle frame 02-04, five layers of vehicle frame 02-05, X/Y plane rotational control assemblies 02-06, X-axis control assembly 02-07,
The composition such as Z axis control assembly 02-08, Y-axis control assembly 02-09.Wherein X/Y plane rotational control assemblies 02-06 is fixed on first
Between layer vehicle frame 02-01 and second layer vehicle frame 02-02, X/Y plane rotational control assemblies 02-05 is adjusted, one layer of vehicle frame can be made opposite
Two layers of vehicle frame are rotated along X/Y plane；X-axis control assembly 02-07 be fixed on second layer vehicle frame 02-02 and third layer vehicle frame 02-03 it
Between, X-axis control assembly 02-07 is adjusted, two layers of vehicle frame can be made to move along the x axis relative to three layers of vehicle frame；Z axis control assembly 02-
08 is fixed between third layer vehicle frame 02-03 and the 4th layer of vehicle frame 02-04, adjusts Z axis control assembly 02-08, can make three layers of vehicle
Frame is moved relative to four layers of vehicle frame along Z-direction, while can also be in XZ plane small angle rotation；Y-axis control assembly 02-09 is fixed on
Between 4th layer of vehicle frame 02-04 and five layers of vehicle frame 02-05, Y-axis control assembly 02-09 is adjusted, four layers of vehicle frame can be made with respect to five layers
Vehicle frame moves along the y axis.
Referring to Fig. 5, the X/Y plane rotational control assemblies 02-06 includes castor 02-06-01, dead axle 02-06-02,
One linear guide 02-06-03, the second screw rod 02-06-04, handwheel sleeve 02-06-05.Wherein castor 02-06-01 is with dead axle
Centered on 02-06-02, circle distribution.
Referring to Fig. 6, the X-axis control assembly 02-07 includes second straight line guide rail 02-07-01, third screw rod 02-07-
02, swivel nut 02-07-03).Wherein second straight line guide rail 02-07-01 is fixed on frame two sides end, swivel nut 02-07-03) it is fixed
Between in the frame；The Y-axis control assembly 02-09 is identical as X-axis control assembly 02-07 composed structure, but installation site is different.
The Y-axis control assembly 02-09 is identical as X-axis control assembly 02-07 composed structure, but installation site is different.
Referring to Fig. 7, the guiding movement and fixation kit 03 include draw bar 03-01, castor 03-02, stabilizer blade 03-
03。
Claims (8)
1. a kind of transporter Large Radar cover installation posture adjustment equipment characterized by comprising type frame (01), posture adjustment vehicle are protected in lifting
Body (02), guiding movement and fixation kit (03)；
Wherein, the lifting protects type frame (01) and uses envelop-type structure, and the lifting protects type frame (01) and is mounted on posture adjustment car body
(02) top；Posture adjustment car body (02) uses multilayer vehicle frame stepped construction；Posture adjustment car body (02) can be in course direction X, spanwise Y
Or vertical direction Z linear movement, or in the rotary motion of X/Y plane and XZ plane；Guiding movement and fixation kit (03) setting
In lower car body, for the short-distance movement of the equipment, fixation and enter initial installation station.
2. equipment according to claim 1, which is characterized in that it includes that frame body (01-01), end connect that type frame (01) is protected in lifting
Head (01-02) holds down assembly (01-03), hanging ring (01-04)；
Wherein, end-fitting (01-02) is fixed on the end on the outside of frame body (01-01), for connecting the reserved threaded hole of cover；
The hold down assembly bottom end of (01-03) is fixed on the inside both ends of frame body (01-01)；Hold down assembly (01-03) antenna house is fixed
In in the space that frame body (01-01) is surrounded, hanging ring (01-04) is fixed on the outside of frame body (01-01).
3. equipment according to claim 2, which is characterized in that hold down assembly (01-03) include protective layer (01-03-01),
Wooden block (01-03-02), plate comer pieces (01-03-03), the first screw rod (01-03-04) and the handwheel (01-03-05) with sleeve；It is anti-
Sheath (01-03-01) is fixed at the top of wooden block (01-03-02), prevents the deformation of product, plate comer pieces (01-03-03) is fixed on
The bottom of wooden block (01-03-02), the first screw rod (01-03-04) are fixed on the outer surface of plate comer pieces (01-03-03)；Band sleeve
Handwheel (01-03-05) internal screw thread and the first screw rod (01-03-04) external screw thread cooperation, realize the first screw rod (01-03-
04) it stretches in sleeve.
4. equipment according to claim 1, which is characterized in that posture adjustment car body (02) include: first layer vehicle frame (02-01),
Second layer vehicle frame (02-02), third layer vehicle frame (02-03), the 4th layer of vehicle frame (02-04), five layers of vehicle frame (02-05), X/Y plane
Rotational control assemblies (02-06), X-axis control assembly (02-07), Z axis control assembly (02-08), Y-axis control assembly (02-09)；
Wherein, X/Y plane rotational control assemblies (02-06) are fixed on first layer vehicle frame (02-01) and second layer vehicle frame (02-02)
Between, it adjusts X/Y plane rotational control assemblies (02-05), rotates one layer of vehicle frame along X/Y plane relative to two layers of vehicle frame；X-axis control
Component (02-07) is fixed between second layer vehicle frame (02-02) and third layer vehicle frame (02-03), adjusts X-axis control assembly (02-
07) two layers of vehicle frame are moved along the x axis relative to three layers of vehicle frame；Z axis control assembly (02-08) is fixed on third layer vehicle frame
Between (02-03) and the 4th layer of vehicle frame (02-04), adjusts Z axis control assembly (02-08), make with respect to four layers vehicle frame of three layers of vehicle frame
It is moved along Z-direction, while also in XZ plane small angle rotation；Y-axis control assembly (02-09) is fixed on the 4th layer of vehicle frame (02-
04) it between five layers of vehicle frame (02-05), adjusts Y-axis control assembly (02-09), makes with respect to five layers vehicle frame of four layers of vehicle frame along Y-axis side
To movement.
5. equipment according to claim 4, which is characterized in that X/Y plane rotational control assemblies (02-06) include: castor
(02-06-01), dead axle (02-06-02), first straight line guide rail (02-06-03), the second screw rod (02-06-04), handwheel sleeve
(02-06-05).Wherein castor (02-06-01) is in the symmetrical centre of first layer vehicle frame (02-01) with dead axle (02-06-02),
Castor (02-06-01) is in the first layer vehicle frame lower part (02-01) with dead axle (02-06-02) for center of circle circle distribution；First straight line
Guide rail (02-06-03) is fixed on the lower part side of first layer vehicle frame (02-01), the sliding block of first straight line guide rail (02-06-03)
It is fixed with one end of the second screw rod (02-06-04), handwheel sleeve (02-06-05) is fixed on the side of second layer car body (02-02)
Face top, the second screw rod (02-06-04) and handwheel sleeve (02-06-05) cooperation, make the second screw rod (02-06-04) in handwheel
It stretches in sleeve (02-06-05), so that sliding block sliding in first straight line guide rail (02-06-03), pushes first layer vehicle frame
(02-01) is along System of Rotating about Fixed Axis.
6. equipment according to claim 4, which is characterized in that X-axis control assembly (02-07) includes second straight line guide rail
(02-07-01), third screw rod (02-07-02), swivel nut (02-07-03)；
Wherein, second straight line guide rail (02-07-01) is fixed between second layer vehicle frame (02-02) and third layer vehicle frame (02-03)
Opposite side end, swivel nut (02-07-03) is fixed on the centre of the bottom second layer vehicle frame (02-02)；Second straight line guide rail (02-
07-01) one end with third screw rod (02-07-02) is fixed, third screw rod (02-07-02) and swivel nut (02-07-03) cooperation,
So that third screw rod (02-07-02) is stretched in swivel nut (02-07-03), makes second layer vehicle frame (02-02) in second straight line guide rail
It is moved on (02-07-01).
7. equipment according to claim 4, which is characterized in that Y-axis control assembly (02-09) and X-axis control assembly (02-
07) composed structure is identical, and Y-axis control assembly (02-09) is arranged in the 4th layer of vehicle frame (02-04) and layer 5 vehicle frame (02-05)
Between opposite side end.
8. equipment according to claim 4, which is characterized in that first layer vehicle frame (02-01), second layer vehicle frame (02-02),
The height of third layer vehicle frame (02-03), the 4th layer of vehicle frame (02-04) and layer 5 vehicle frame (02-05) successively reduces.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910412523.XA CN110271688A (en) | 2019-05-17 | 2019-05-17 | A kind of transporter large-scale antenna dome installation posture adjustment equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910412523.XA CN110271688A (en) | 2019-05-17 | 2019-05-17 | A kind of transporter large-scale antenna dome installation posture adjustment equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110271688A true CN110271688A (en) | 2019-09-24 |
Family
ID=67959941
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910412523.XA Pending CN110271688A (en) | 2019-05-17 | 2019-05-17 | A kind of transporter large-scale antenna dome installation posture adjustment equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110271688A (en) |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101203443A (en) * | 2005-05-31 | 2008-06-18 | 法国航空公司 | Container for stocking and transporting a radome |
| CN101570249A (en) * | 2008-10-17 | 2009-11-04 | 浙江大学 | Radome installation bogie based on array absorption unit |
| CN102059549A (en) * | 2010-11-12 | 2011-05-18 | 浙江大学 | Airplane engine attitude regulation installation system based on four numerical control positioners and use method thereof |
| CN103204248A (en) * | 2013-03-25 | 2013-07-17 | 大连理工大学 | Numerical-control electric frame truck for airplane engine mounting |
| CN105538200A (en) * | 2016-02-02 | 2016-05-04 | 华中科技大学 | Tool clamp with workpiece shape protecting function |
| CN106184815A (en) * | 2016-08-25 | 2016-12-07 | 长沙市天映机械制造有限公司 | Gate loading, unloading work platforms and application process thereof after aircraft |
| CN205873767U (en) * | 2016-07-15 | 2017-01-11 | 郑州飞机装备有限责任公司 | Aircraft ventral antenna house installation car |
| CN206155819U (en) * | 2016-10-10 | 2017-05-10 | 深圳市劲拓自动化设备股份有限公司 | Appearance equipment is transferred to high accuracy with remove function |
| CN107336844A (en) * | 2017-07-04 | 2017-11-10 | 西安飞机工业（集团）有限责任公司 | A kind of multiple material stringer of aircraft, wall panel skin upset docking equipment and docking calculation |
| CN107352043A (en) * | 2017-06-26 | 2017-11-17 | 大连理工大学 | A kind of six axle posture adjustment platforms for aircraft engine whole machine installation |
| CN108673393A (en) * | 2018-07-28 | 2018-10-19 | 江西省东龙实业股份有限公司 | A kind of movement assembly station plate |
| CN109131930A (en) * | 2018-09-29 | 2019-01-04 | 西安飞机工业（集团）有限责任公司 | A kind of radome of fighter installation pose_adjuster |
| CN109318154A (en) * | 2018-11-07 | 2019-02-12 | 昌河飞机工业（集团）有限责任公司 | A kind of hinge class part positioning clamping device |
| CN109747863A (en) * | 2019-01-11 | 2019-05-14 | 清华大学 | Coupled Rigid-flexible posture adjusting system and its attitude-adjusting method |
-
2019
- 2019-05-17 CN CN201910412523.XA patent/CN110271688A/en active Pending
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101203443A (en) * | 2005-05-31 | 2008-06-18 | 法国航空公司 | Container for stocking and transporting a radome |
| CN101570249A (en) * | 2008-10-17 | 2009-11-04 | 浙江大学 | Radome installation bogie based on array absorption unit |
| CN102059549A (en) * | 2010-11-12 | 2011-05-18 | 浙江大学 | Airplane engine attitude regulation installation system based on four numerical control positioners and use method thereof |
| CN103204248A (en) * | 2013-03-25 | 2013-07-17 | 大连理工大学 | Numerical-control electric frame truck for airplane engine mounting |
| CN105538200A (en) * | 2016-02-02 | 2016-05-04 | 华中科技大学 | Tool clamp with workpiece shape protecting function |
| CN205873767U (en) * | 2016-07-15 | 2017-01-11 | 郑州飞机装备有限责任公司 | Aircraft ventral antenna house installation car |
| CN106184815A (en) * | 2016-08-25 | 2016-12-07 | 长沙市天映机械制造有限公司 | Gate loading, unloading work platforms and application process thereof after aircraft |
| CN206155819U (en) * | 2016-10-10 | 2017-05-10 | 深圳市劲拓自动化设备股份有限公司 | Appearance equipment is transferred to high accuracy with remove function |
| CN107352043A (en) * | 2017-06-26 | 2017-11-17 | 大连理工大学 | A kind of six axle posture adjustment platforms for aircraft engine whole machine installation |
| CN107336844A (en) * | 2017-07-04 | 2017-11-10 | 西安飞机工业（集团）有限责任公司 | A kind of multiple material stringer of aircraft, wall panel skin upset docking equipment and docking calculation |
| CN108673393A (en) * | 2018-07-28 | 2018-10-19 | 江西省东龙实业股份有限公司 | A kind of movement assembly station plate |
| CN109131930A (en) * | 2018-09-29 | 2019-01-04 | 西安飞机工业（集团）有限责任公司 | A kind of radome of fighter installation pose_adjuster |
| CN109318154A (en) * | 2018-11-07 | 2019-02-12 | 昌河飞机工业（集团）有限责任公司 | A kind of hinge class part positioning clamping device |
| CN109747863A (en) * | 2019-01-11 | 2019-05-14 | 清华大学 | Coupled Rigid-flexible posture adjusting system and its attitude-adjusting method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104985596B (en) | Five-freedom hybrid robot with multi-axis rotation brackets | |
| CN103287587B (en) | A kind of vertical take-off and landing aircraft (VTOL aircraft) ground simulated flight test platform | |
| CN101386146B (en) | Numerical control polishing mechanical hand of optical elements of large caliber | |
| CN109231065A (en) | A kind of six degree of freedom posture adjusting system based on Omni-mobile module | |
| CN106826180B (en) | Manual butt joint assembly quality of gas suspension | |
| CN204720557U (en) | A kind of symmetrical three freedom redundancy drives parallel antenna structure system | |
| CN105151298B (en) | The empennage regulating mechanism and flapping-wing aircraft that a kind of achievable pitching and yaw independently regulate and control | |
| CN204913901U (en) | It changes movable support's five degree of freedom series -parallel connection robots to contain multiaxis | |
| CN104029199A (en) | Translational half-decoupling service robot | |
| CN107762179B (en) | A kind of waiting booth with seat adjusting and high temperature sunstroke prevention function | |
| CN104669964A (en) | Water-land-air triphibious unmanned investigation device | |
| CN107775611A (en) | Spacecraft posture adjustment cantilevered multi-axis turntable | |
| CN208948597U (en) | The double column gantries of numerical control spread strip winding machine | |
| CN105292514B (en) | Manual bomb truck | |
| CN103078184A (en) | Plate-like antenna adjustment device | |
| CN107200053B (en) | A kind of rib storing unit | |
| CN108994846A (en) | A kind of good automatic patrol security robot of protecting effect | |
| CN110271688A (en) | A kind of transporter large-scale antenna dome installation posture adjustment equipment | |
| CN107933417A (en) | A kind of Portable unmanned machine launching platform installed in automobile top | |
| CN106654510A (en) | Large working space variable driving parallel antenna seat mechanism | |
| CN207034553U (en) | A kind of portable manual levelling device | |
| CN108748606A (en) | A kind of hyperbaric oxygen chamber 3D printing method | |
| CN204625001U (en) | A kind of simple and easy multidirectional hanging apparatus | |
| CN208992648U (en) | The air bearing four-dimension adjusts platform | |
| CN203150707U (en) | Plate-shaped antenna adjustment device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190924 |