CN209521884U - A kind of aircraft wing installation leveling unit - Google Patents
A kind of aircraft wing installation leveling unit Download PDFInfo
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- CN209521884U CN209521884U CN201920064545.7U CN201920064545U CN209521884U CN 209521884 U CN209521884 U CN 209521884U CN 201920064545 U CN201920064545 U CN 201920064545U CN 209521884 U CN209521884 U CN 209521884U
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- 230000007246 mechanism Effects 0.000 claims abstract description 93
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- 230000008569 process Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 238000011900 installation process Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
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Abstract
The utility model discloses a kind of aircraft wings to install leveling unit, mass movement mechanism and the leveling mechanisms at different levels on movement mechanism, leveling mechanisms at different levels include level(l)ing mechanism, the leveling mechanism on level(l)ing mechanism and the wing fixed mechanism on leveling mechanism；Level(l)ing mechanism includes the lateral adjustment on movement mechanism and the longitudinal adjusting mechanism in lateral adjustment.The utility model structure is simple, facilitate the transport of aircraft wing, during aircraft wing installation, can lateral position to aircraft, lengthwise position, height and be adjusted in parallel, to improve the installation effectiveness of aircraft wing, it can facilitate simultaneously and various sizes and wing of various shapes are fixed, there is stronger practicability.
Description
Technical field
The utility model relates to aircraft correlative technology fields more particularly to a kind of aircraft wing to install leveling unit.
Background technique
Carry-on wing is mainly used for the main component that aircraft makes aircraft generate lift in flight course.One
As be divided into left and right two aerofoils, be symmetrically arranged at fuselage both sides.Some positions of wing are mainly that leading edge and rear can live
It is dynamic.These parts of pilot control can change the shape of wing, control the distribution of airfoil lift or resistance, be risen with reaching to increase
Power or the purpose for changing aspect.On wing common movable wing have various front and rear edge high lift devices, aileron, spoiler,
Flap, elevon etc..
Itself having the characteristics that length is longer due to wing, the fixed installation of this wing produces large effect,
Wing is transported to aircraft body side using dedicated transport device such as hanging apparatus when the wing installation of Large Scale Space Vehicle,
After carrying out slow position adjustment, wing is mounted in aircraft body, this mode of operation can install wing
In the main body of aircraft, but in operating process, Yao Jinhang is constantly positioned, and installation could be completed, to greatly influence
Aircraft packaging efficiency.
Simultaneously also mostly also in this way for the wing installation of small aircraft, small part uses dedicated wing
Mounting device, this device only facilitate the transport of wing, while the fine tuning being able to carry out on some direction during installation, still
The problem of facing in actual installation process, not only some direction of wing need to carry out all directions in adjustment
Adjustment, while wing mounting device quality in the prior art is larger, therefore increases the difficulty of wing transport, it is most important that
Greatly reduce wing packaging efficiency.
Utility model content
The utility model provides a kind of aircraft wing installation leveling unit, to solve above-mentioned the deficiencies in the prior art, side
Just the transport of aircraft wing, during aircraft wing installation, can lateral position to aircraft, lengthwise position,
It height and is adjusted, to improve the installation effectiveness of aircraft wing, while can facilitate to various sizes and respectively in parallel
The wing of kind shape is fixed, and has stronger practicability.
In order to realize the purpose of this utility model, the following technology of proposed adoption:
A kind of aircraft wing installation leveling unit, mass movement mechanism and the levelling machines at different levels on movement mechanism
Structure,
Leveling mechanisms at different levels include level(l)ing mechanism, the leveling mechanism on level(l)ing mechanism and are set to levelling
Wing fixed mechanism in mechanism；
Level(l)ing mechanism includes lateral adjustment on the movement mechanism and in lateral adjustment
Longitudinal adjusting mechanism；
Level(l)ing mechanism, for adjusting the horizontal position for being installed on wing fixed mechanism top wing；
Leveling mechanism, for being installed on the levelling of wing fixed mechanism top wing；
Wing fixed mechanism, for being fixed according to the shape and size of wing to wing.
Preferably, lateral adjustment includes before being set to the first bottom plate on movement mechanism, being set to the first plate upper surface
The cross slide way of two sides, the lateral bearing block set on the first plate upper surface both ends, the transverse direction that is assemblied on lateral bearing block afterwards
Screw rod and cross motor set on transverse screw one end, lateral bearing block and transverse screw are between cross slide way, laterally
Motor is fixed on the first bottom plate.
Preferably, longitudinal adjusting mechanism includes before being set to the second bottom plate on cross slide way, being set to the second lower surface of base plate
Afterwards the transverse slider of two sides it is several, set on the transverse movement block of the second lower surface of base plate middle position, in being longitudinally set to the
The longitudinal rail of two plate upper surface two sides, set on the second plate upper surface middle position longitudinal bearing block, be assemblied in it is vertical
Longitudinal screw on bearing block and the longitudinal motor set on longitudinal screw one end, transverse slider are assemblied on cross slide way,
Transverse movement is packaged assigned on transverse screw, and between longitudinal rail, longitudinal motor is fixed for longitudinal bearing block and longitudinal screw
In the second bottom plate.
Preferably, leveling mechanism includes being set to the third bottom plate on longitudinal rail, being set on third lower surface of base plate two sides
Longitudinal sliding block it is several, set on third lower surface of base plate middle position longitudinal movement block, be set to third plate upper surface four
Flexible module four at angle, the flake bar equipped with connector upper end, is through at flake bar at the connector set on flexible module upper end
The pin shaft of upper end, the support set on flake bar upper end and two pieces of the fixed plate set on support upper end, longitudinal sliding block is assemblied in
On longitudinal rail, longitudinal movement is packaged assigned on longitudinal screw, and fixed plate is parallel to cross slide way, and the lower end of every piece of fixed plate is equal
It is equipped with there are two flexible module, the middle position front and rear sides of third bottom plate are equipped with U-lag.
Preferably, wing fixed mechanism include the fixed frame being installed in fixed plate, it is outer on fixed frame two sidewalls
Prolong frame, the universal base set on the extension frame upper surface other end and fixed frame upper surface front end it is several and be set to extension frame upper surface
On auxiliary installation piece it is several.
Preferably, fixed frame inner wall middle position is equipped with pull rod, and universal base is set to the turning of fixed frame and extension frame
Place.
Preferably, universal base includes being set to fixed frame and the support rod of extension frame corner, the end set on post upper
Ball, the assembling stand for being assemblied in end ball upper end and the disk set on assembling stand upper end.
Preferably, auxiliary installation piece includes the rotating cylinder being set on extension frame upper surface and the installation being assemblied on rotating cylinder
Seat.
Preferably, disk is made of rubber.
Preferably, movement mechanism includes that bottom plate, the moving wheel set on bottom plate lower end be several, push-and-pull set on base plate rear end
Frame is set on the bottom plate sweptback first strut of front end surface, is set on the bottom plate the second strut that front end surface turns forward
And the 4th bottom plate set on the first strut and the second strut upper end, the first strut and the second strut intersect, the first bottom plate
On the 4th bottom plate.
This programme the utility model has the advantages that
It 1, can be right when movement mechanism is relatively fixed by the mutual cooperation of lateral adjustment and longitudinal adjusting mechanism
Wing implements small horizontal adjustment forward, backward, to the left and to the right, so that wing is facilitated to be mounted in aircraft body,
Wherein, lateral adjustment is responsible for the left and right adjustment of wing, and adjustment process drives transverse screw rotation by cross motor, finally
The movement of transverse movement block is driven, and the movement of transverse movement block is able to drive longitudinal adjusting mechanism generation to the left or to the right
Movement；Longitudinal adjusting mechanism is responsible for the front-rear position adjustment of wing, and adjustment process drives longitudinal screw to turn by longitudinal motor
Dynamic, the final movement for driving longitudinal movement block is the front and back that the movement of longitudinal movement block is able to drive the movement of leveling mechanism again
Movement；
2, by leveling mechanism, wing is enabled to carry out short-range lifting and can be realized each of aircraft wing
Wing, is mounted in aircraft body by the balance in a direction to facilitate, and improves the installation effectiveness of wing, wherein flexible mould
Block is the core component in leveling mechanism, first by flexible module distribution the characteristics of, conveniently obtain each position of wing
Balance, secondly, flexible module uses selection lighter weight, facilitates control and reaction is fast in order to reduce the quality of whole device
The miniature electromotive handspike device of speed；
3, the wing fixed mechanism of this programme design, is mainly used for fixing and supporting in wing installation process, wherein
Universal base can adapt to very well the shape of wing, so that wing fixed mechanism is improved to the fixed function of wing, while in order to
The wing feature unstable due to universal seat supports during the installation process is prevented, and falls wing, therefore devise auxiliary peace
Piece installing improves the fixed function to wing, while in order to prevent during universal base generates support to wing to wing
Surface generates scratch, therefore disk is made of rubber；
4, the utility model facilitates the transport of aircraft wing, can be to flight during aircraft wing installation
It the lateral position of device, lengthwise position, height and is adjusted in parallel, to improve the installation effectiveness of aircraft wing, simultaneously
It can facilitate and various sizes and wing of various shapes are fixed, there is stronger practicability.
Detailed description of the invention
Fig. 1 shows the utility model overall three-dimensional structure.
Fig. 2 shows the three-dimensional structure diagrams for not including wing.
Fig. 3 show do not include wing and wing fixed mechanism three-dimensional structure diagram.
Fig. 4 show do not include wing, wing fixed mechanism and leveling mechanism three-dimensional structure diagram.
Fig. 5 show do not include wing, wing fixed mechanism, leveling mechanism and longitudinal adjusting mechanism stereochemical structure
Figure.
Fig. 6 shows the three-dimensional structure diagram of universal base 53.
Specific embodiment
It is practical to this below in conjunction with attached drawing in order to keep the purpose of this utility model, technical solution and advantage clearer
It is novel to be described in further detail.
As shown in figs 1 to 6, a kind of aircraft wing installs leveling unit, mass movement mechanism 1 and is set to fitness machine
Leveling mechanisms at different levels on structure 1, leveling mechanisms at different levels include level(l)ing mechanism, the leveling mechanism on level(l)ing mechanism
4 and the wing fixed mechanism 5 on leveling mechanism 4；Level(l)ing mechanism includes the lateral adjustments on movement mechanism 1
Mechanism 2 and the longitudinal adjusting mechanism 3 in lateral adjustment 2.Wherein, level(l)ing mechanism is installed on for adjusting
The horizontal position of 5 top wing 6 of wing fixed mechanism, leveling mechanism 4, for being installed on looking for for 5 top wing 6 of wing fixed mechanism
Flat, wing fixed mechanism 5 is fixed to wing 6 for the shape and size according to wing 6.
Lateral adjustment 2 includes the first bottom plate 20 being mounted on movement mechanism 1, is mounted on 20 upper surface of the first bottom plate
The cross slide way 21 of front and rear sides is mounted on the lateral bearing block 22 at 20 upper surface both ends of the first bottom plate, is mounted on lateral bearing
Transverse screw 23 on seat 22 and it is mounted on the cross motor 24 of 23 one end of transverse screw, lateral bearing block 22 and transverse screw
23 are between cross slide way 21, and cross motor 24 is fixed on the first bottom plate 20.
Longitudinal adjusting mechanism 3 includes the second bottom plate 30 being mounted on cross slide way 21, is mounted on 30 following table of the second bottom plate
The transverse slider 35 of face front and rear sides is several, is mounted on the transverse movement block 36 of 30 lower surface middle position of the second bottom plate, is in
It is longitudinally mounted on the longitudinal rail 31 of 30 upper surface two sides of the second bottom plate, is mounted on 30 upper surface middle position of the second bottom plate
Longitudinal bearing block 32, the longitudinal screw 33 being mounted on longitudinal bearing block 32 and longitudinal electricity set on 33 one end of longitudinal screw
Machine 34, transverse slider 35 are mounted on cross slide way 21, and transverse movement block 36 is mounted on transverse screw 23, longitudinal bearing block 32
With longitudinal screw 33 between longitudinal rail 31, longitudinal motor 34 is mounted on the second bottom plate 30.
Leveling mechanism 4 includes the third bottom plate 40 being mounted on longitudinal rail 31, is mounted on 40 lower surface two of third bottom plate
Longitudinal sliding block 48 on side is several, is mounted on the longitudinal movement block 47 set on 40 lower surface middle position of third bottom plate, installation
In the flexible module 41 4 of 40 upper surface four corners of third bottom plate, it is mounted on the connector 42 of flexible 41 upper end of module, is mounted on
The flake bar 43 of 42 upper end of connector is mounted on the pin shaft 44 of 43 upper end of flake bar, is mounted on the support 45 of 43 upper end of flake bar
Support 45 and flake bar 43 are assemblied together by pin shaft 44, and are mounted on 46 two pieces of fixed plate of 45 upper end of support, longitudinal
Sliding block 48 is assemblied on longitudinal rail 31, and longitudinal movement block 47 is assemblied on longitudinal screw 33, and fixed plate 46 is parallel to transverse direction
Guide rail 21, the lower end of every piece of fixed plate 46 are equipped with there are two flexible module 41, two before and after the middle position of third bottom plate 40
Side is equipped with U-lag 400, wherein flexible module 41 selects lighter weight, facilitates control and willing miniature electromotive handspike
Device.
Wing fixed mechanism 5 includes the fixed frame 50 being mounted in fixed plate 46, is mounted on 50 two sidewalls of fixed frame
Extension frame 51, the universal base 53 for being mounted on 50 upper surface front end of the 51 upper surface other end of extension frame and fixed frame are several and be set to
Auxiliary installation piece 54 on 51 upper surface of extension frame is several, and 50 inner wall middle position of fixed frame is equipped with pull rod 52, universal base 53
It is set to the corner of fixed frame 50 and extension frame 51.Wherein, universal base 53 includes being mounted on fixed frame 50 and extension frame 51 turns
Support rod 530 at angle, the end ball 5300 for being mounted on 530 upper end of support rod, be assemblied in the assembling stand 531 of end 5300 upper end of ball with
And the disk 532 set on 531 upper end of assembling stand, disk 532 are made of rubber.Auxiliary installation piece 54 includes being set on extension frame 51
Rotating cylinder 540 on surface and the mounting base 541 being assemblied on rotating cylinder 540.
The moving wheel 11 that movement mechanism 1 includes bottom plate 10, is mounted on 10 lower end of bottom plate is several, is mounted on 10 rear end of bottom plate
Pushing-pulling-rack 12, be mounted on sweptback first strut 13 in 10 upper surface front end of bottom plate, be mounted on 10 upper surface front end of bottom plate to
Second strut 14 of top rake and the 4th bottom plate 15 set on 14 upper end of the first strut 13 and the second strut, 13 He of the first strut
Second strut 14 intersects, and the first bottom plate 20 is mounted on the 4th bottom plate 15.
Specific embodiment is as described below:
One, wing 6 is placed on the disk 532 of universal base 53 on wing fixed mechanism 5, each disk 532 will be according to machine
The length and shape of the wing carry out adaptive adjustment；
Two, the height for adjusting mounting base 541, further fixes wing 6；
Three, wing 6 is transferred at the position that aircraft body wing 6 is installed by pushing-pulling-rack 12；
Four, moving wheel 11 is fixed, and comes into effect the assembling of wing 6；
Five, to the adjustment of " left and right " lateral position of wing 6, it is as follows to adjust process: starting cross motor 24 makes cross
Transverse screw 23 is driven to rotate to motor 24, and the rotation of transverse screw 23 further makes the on transverse movement block 36
Two bottom plates 30 to the left or move right, and the cross slide way 21 of two sides plays a part of support and guiding to the second bottom plate 30,
Finally complete the adjustment of the lateral position of wing 6；
Six, to the adjustment of " front and back " lengthwise position of wing 6, it is as follows to adjust process: starting longitudinal motor 34 to indulge
Longitudinal screw 33 is driven to rotate to motor 34, and the rotation of longitudinal screw 33 further makes the on longitudinal movement block 47
Movement forward or backward occurs for three bottom plates 40, finally completes the adjustment of the lengthwise position of wing 6；
Seven, to the adjustment of the height and the degree of balance of wing 6, it is as follows to adjust process: starting 40 4 angles of third bottom plate
On flexible module 41, flexible module 41 can be such that wing 6 goes up and down, after wing 6 is gone up and down to enough height, to wing
6 degree of balance is adjusted, and during adjustment, flexible module 41 carries out scaling operation as the case may be, until entire
Until wing is in a horizontal state；
Eight, wing 6 is mounted in the main body of aircraft.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, it is clear that this field
Technical staff various modification and variations can be carried out to the utility model without departing from the spirit and scope of the utility model.This
Sample, if these modifications and variations of the present invention belong to the claims of the present invention and its equivalent technology range it
Interior, then the utility model is also intended to include these modifications and variations.
Claims (10)
1. a kind of aircraft wing installs leveling unit, mass movement mechanism (1) and be set on movement mechanism (1) at different levels look for
Flattening mechanism, which is characterized in that
Leveling mechanisms at different levels include level(l)ing mechanism, the leveling mechanism (4) on level(l)ing mechanism and are set to levelling
Wing fixed mechanism (5) in mechanism (4)；
Level(l)ing mechanism includes the lateral adjustment (2) on movement mechanism (1) and is set to lateral adjustment (2)
On longitudinal adjusting mechanism (3)；
Level(l)ing mechanism, for adjusting the horizontal position for being installed on wing fixed mechanism (5) top wing (6)；
Leveling mechanism (4), for being installed on the levelling of wing fixed mechanism (5) top wing (6)；
Wing fixed mechanism (5), it is fixed to wing (6) for the shape and size according to wing (6).
2. aircraft wing according to claim 1 installs leveling unit, which is characterized in that lateral adjustment (2) packet
The cross slide way for including the first bottom plate (20) being set on movement mechanism (1), being set to the first bottom plate (20) upper surface front and rear sides
(21), the lateral bearing block (22) at the first bottom plate (20) upper surface both ends, the transverse direction being assemblied on lateral bearing block (22) are set to
Screw rod (23) and the cross motor (24) for being set to transverse screw (23) one end, lateral bearing block (22) and transverse screw (23) position
Between cross slide way (21), cross motor (24) is fixed on the first bottom plate (20).
3. aircraft wing according to claim 2 installs leveling unit, which is characterized in that longitudinal adjusting mechanism (3) packet
The transverse slider for including the second bottom plate (30) being set on cross slide way (21), being set to the second bottom plate (30) lower surface front and rear sides
(35) transverse movement block (36) that is several, being set to the second bottom plate (30) lower surface middle position is in longitudinally to be set to the second bottom
The longitudinal rail (31) of plate (30) upper surface two sides, the longitudinal bearing block for being set to the second bottom plate (30) upper surface middle position
(32), the longitudinal screw (33) being assemblied on longitudinal bearing block (32) and the longitudinal motor set on longitudinal screw (33) one end
(34), transverse slider (35) is assemblied on cross slide way (21), and transverse movement block (36) is assemblied on transverse screw (23), longitudinal
Bearing block (32) and longitudinal screw (33) are located between longitudinal rail (31), and longitudinal motor (34) is fixed on the second bottom plate (30).
4. aircraft wing according to claim 3 installs leveling unit, which is characterized in that leveling mechanism (4) includes setting
In on longitudinal rail (31) third bottom plate (40), be set to third bottom plate (40) lower surface two sides on longitudinal sliding block (48) if
Longitudinal movement block (47) that is dry, being set to third bottom plate (40) lower surface middle position is set to third bottom plate (40) upper surface four
Flexible module (41) four at angle, is set to connector (42) upper end at the connector (42) for being set to flexible module (41) upper end
Flake bar (43), the pin shaft (44) for being through at flake bar (43) upper end, be set to flake bar (43) upper end support (45) and be set to
(46) two pieces of the fixed plate of support (45) upper end, longitudinal sliding block (48) is assemblied on longitudinal rail (31), longitudinal movement block
(47) it is assemblied on longitudinal screw (33), fixed plate (46) is parallel to cross slide way (21), and the lower end of every piece of fixed plate (46) is equal
It is equipped with there are two flexible module (41), the middle position front and rear sides of third bottom plate (40) are equipped with U-lag (400).
5. aircraft wing according to claim 4 installs leveling unit, which is characterized in that wing fixed mechanism (5) packet
It includes the fixed frame (50) being installed on fixed plate (46), the extension frame (51) being set on fixed frame (50) two sidewalls, be set to extension
Frame (51) the upper surface other end and the universal base (53) of fixed frame (50) upper surface front end it is several and be set to extension frame (51) on
Auxiliary installation piece (54) on surface is several.
6. aircraft wing according to claim 5 installs leveling unit, which is characterized in that among fixed frame (50) inner wall
Pull rod (52) are equipped at position, universal base (53) is set to the corner of fixed frame (50) and extension frame (51).
7. aircraft wing according to claim 6 installs leveling unit, which is characterized in that universal base (53) includes being set to
Fixed frame (50) and the support rod (530) of extension frame (51) corner, the end ball (5300) for being set to support rod (530) upper end, dress
Assigned in the assembling stand (531) for holding ball (5300) upper end and set on the disk (532) of assembling stand (531) upper end.
8. aircraft wing according to claim 7 installs leveling unit, which is characterized in that auxiliary installation piece (54) includes
Rotating cylinder (540) on extension frame (51) upper surface and the mounting base (541) being assemblied on rotating cylinder (540).
9. aircraft wing according to claim 7 installs leveling unit, which is characterized in that disk (532) is by rubber system
At.
10. aircraft wing according to claim 2 installs leveling unit, which is characterized in that movement mechanism (1) includes bottom
Plate (10), the moving wheel (11) for being set to bottom plate (10) lower end are several, are set to the pushing-pulling-rack (12) of bottom plate (10) rear end, are set to bottom plate
(10) sweptback first strut (13) in upper surface front end, the second strut to turn forward set on bottom plate (10) upper surface front end
(14) the 4th bottom plate (15) of the first strut (13) and the second strut (14) upper end, the first strut (13) and second are set to and
Bar (14) intersects, and the first bottom plate (20) is set on the 4th bottom plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920064545.7U CN209521884U (en) | 2019-01-15 | 2019-01-15 | A kind of aircraft wing installation leveling unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920064545.7U CN209521884U (en) | 2019-01-15 | 2019-01-15 | A kind of aircraft wing installation leveling unit |
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| Publication Number | Publication Date |
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| CN209521884U true CN209521884U (en) | 2019-10-22 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201920064545.7U Active CN209521884U (en) | 2019-01-15 | 2019-01-15 | A kind of aircraft wing installation leveling unit |
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| CN (1) | CN209521884U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455717A (en) * | 2020-12-12 | 2021-03-09 | 江西洪都航空工业集团有限责任公司 | Wing body assembling and folding platform with transportation function |
| CN112504608A (en) * | 2020-12-17 | 2021-03-16 | 中国航天空气动力技术研究院 | Tail retreating separation test model initial position measuring device |
-
2019
- 2019-01-15 CN CN201920064545.7U patent/CN209521884U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112455717A (en) * | 2020-12-12 | 2021-03-09 | 江西洪都航空工业集团有限责任公司 | Wing body assembling and folding platform with transportation function |
| CN112504608A (en) * | 2020-12-17 | 2021-03-16 | 中国航天空气动力技术研究院 | Tail retreating separation test model initial position measuring device |
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