CN109760850A - A kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted - Google Patents
A kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted Download PDFInfo
- Publication number
- CN109760850A CN109760850A CN201711095502.7A CN201711095502A CN109760850A CN 109760850 A CN109760850 A CN 109760850A CN 201711095502 A CN201711095502 A CN 201711095502A CN 109760850 A CN109760850 A CN 109760850A
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- CN
- China
- Prior art keywords
- transverse
- positioning sleeve
- active block
- unmanned plane
- assembly
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- 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
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Abstract
The invention discloses the ratchet lifting unmanned plane EO that a kind of transverse and longitudinal is adjusted to install vehicle, including pallet component (1), Quick-release pin (2) and lifting assembly (3).The ratchet lifting EO installation vehicle that transverse and longitudinal provided by the present invention is adjusted can be realized quick, the reliable installation of EO, convenient disassembly, not only convenient transportation but also can save cost of labor.
Description
Technical field
The present invention relates to unmanned plane cradle technology fields, and in particular to a kind of ratchet lifting EO installation that transverse and longitudinal is adjusted
Vehicle.
Background technique
EO is the probe assembly of unmanned plane, and the installation site of EO is located at the lower end of unmanned plane head, is higher than fuselage cover bottom
Face.By own form, the constraint of mounting height, fuselage cover, a kind of ratchet that the transverse and longitudinal for facilitating installation EO is adjusted is devised
It goes up and down EO and vehicle is installed.The mounting means of the EO is pushed into installation site using from unmanned plane head toward fuselage direction, adjusts spine
Wheel mechanism runner assembly (7), active block (14), driven nut (15) make EO rise to mounting height, adjust transverse and longitudinal adjustment disk (13)
It is directed at installation point, installation vehicle is lowered after being installed, back pushing block (12) is slided, goes back to support claw (9), then toward head side
Installation is completed to EO installation vehicle is exited.
Summary of the invention
The technical problems to be solved by the present invention are: providing a kind of ratchet lifting unmanned plane EO installation that transverse and longitudinal is adjusted
Vehicle.
The technical scheme adopted by the invention is that: a kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted, it is special
Sign is: EO installs the sliding groove structure of pallet component (1) using three groups of circumference uniform distributions of vehicle and the support with rotation function
Pawl (9), support claw (9) goes to horizontal position just will not be lower turn, and transverse and longitudinal is adjusted using two layers of sliding groove structure, passes through adjusting
Transverse and longitudinal adjustment disk (13) realizes that up-down mode using Quick-release pin (2) connecting trays component (1) and rises using ratchet mechanism
It comes down to a lower group part (3), that is, is readily disassembled and convenient transportation.
In conclusion the ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal provided by the present invention is adjusted can be realized EO's
Quickly, it reliably installs, has saved cost of labor.
Detailed description of the invention
Fig. 1 is that the ratchet lifting unmanned plane EO installation vehicle that a kind of transverse and longitudinal is adjusted installs the schematic diagram after EO.
Fig. 2 is that the ratchet that a kind of transverse and longitudinal is adjusted goes up and down the installation condition schematic diagram that unmanned plane EO installs vehicle.
Fig. 3 is the contraction state schematic diagram that EO installs vehicle.
Fig. 4 is the elevating mechanism cross-sectional view of lifting assembly (3).
Fig. 5 is active block (14) schematic diagram.
Fig. 6 is active block (14) and driven nut (15) cooperates schematic diagram.
Fig. 7 is Quick-release pin (2) schematic diagram.
Fig. 8 is the package assembly detail drawing of pushing block (12), support claw (9) on pallet component (1).
Fig. 9 is support claw (9) schematic diagram.
Figure 10 is pushing block (12) schematic diagram；
Figure 11 is to push slot (24) schematic diagram；
Wherein: pallet component (1), Quick-release pin (2), lifting assembly (3), universal wheel (4), frame assembly (5), positioning sleeve (6) turn
Dynamic component (7), screw rod (8), support claw (9), rotary shaft (10), slide assembly (11), pushing block (12), transverse and longitudinal adjustment disk
(13), active block (14), driven nut (15), pin shaft (16), holding screw (17), plane bearing (18), rocking bar (19), baffle
(20), pull ring (21), shank (22), scotch (23) push slot (24), push button Quick-release pin (25).
Specific embodiment
Specific embodiments of the present invention will be described in detail with reference to the accompanying drawing.
As shown in Fig. 2, the present invention is made of three components altogether: pallet component (1), Quick-release pin (2), lifting assembly (3).
As shown in Fig. 3,4,7,8, pallet component (1) includes: support claw (9), rotary shaft (10), and slide assembly (11) pushes away
Motion block (12), transverse and longitudinal adjustment disk (13) push slot (24), push button Quick-release pin (25)；Quick-release pin (2) includes: pull ring (21), pin
Body (22)；Scotch (23)；Lifting assembly (3) includes: universal wheel (4), frame assembly (5), positioning sleeve (6), runner assembly
(7), screw rod (8), active block (14), driven nut (15), pin shaft (16), holding screw (17), plane bearing (18), rocking bar
(19), baffle (20).
As shown in figure 4, being mounted with positioning sleeve (6) on frame assembly (5), a plane bearing is provided in positioning sleeve (6)
(18), for mitigating the friction between driven nut (15) and positioning sleeve (6) inner face.Driven nut (15) is by circle distribution in fixed
What three holding screws (17) on position set (6) limited, being allowed to be fixed on positioning sleeve (6) can only move in a circle.Active block
(14) it is fixed on runner assembly (7) using split pin, active block (14) is rotatable, and rocking bar (19) is connected to by pin shaft (16)
On runner assembly (7), it can be rotated upwardly and downwardly around pin shaft (16).The working principle of elevating mechanism is: circular-rotation rocking bar (19) drives
Runner assembly (7), active block (14) are mobile to fall into active block (14) sliding in driven nut (15) trough (such as Fig. 5,6 institutes
Show), push driven nut (15) rotation that screw rod (8) is driven to rise, rising to limiting value position rear baffle (20) will limit.It will
Active block (14) rotates to another direction, and rotary screw (8) will decline according to the above method again.
As shown in figure 8, being connect between support claw (9) and pushing block (12) by rotary shaft (10), wherein at support claw (9)
It will not fall after scheming upper position and holding up EO.It is fixed by push button Quick-release pin (25) between pushing block (12) and promotion slot (24)
Position.
Claims (3)
1. unmanned plane EO installation vehicle is made of pallet component (1), Quick-release pin (2), lifting assembly (3).
2. it includes: support claw (9), rotary shaft (10), slide assembly (11), pushing block that unmanned plane EO, which installs vehicle pallet component (1),
(12), transverse and longitudinal adjustment disk (13) push slot (24), push button Quick-release pin (25)；EO install vehicle pallet component (1) using
The sliding groove structure of three groups of circumference uniform distributions and support claw (9) with rotation function, support claw (9) go to horizontal position and stop lower turn,
Transverse and longitudinal is adjusted using two layers of sliding groove structure, is realized by adjusting transverse and longitudinal adjustment disk (13).
3. the lifting assembly (3) that unmanned plane EO installs vehicle includes: universal wheel (4), frame assembly (5), positioning sleeve (6), rotating group
Part (7), screw rod (8), active block (14), driven nut (15), pin shaft (16), holding screw (14), plane bearing (18), rocking bar
(19), baffle (20)；Runner assembly (7), active block (14) movement are driven to make active block (14) by circular-rotation rocking bar (19)
Sliding is fallen into driven nut (15) trough, pushes driven nut (15) rotation that screw rod (8) is driven to rise, after rising to limiting value
Baffle (20) will limit；Active block (14) is rotated to another direction, and rotary screw (8) will decline according to the above method again；
Wherein, it is mounted with positioning sleeve (6) on frame assembly (5), a plane bearing (18) is provided in positioning sleeve (6), for mitigating
Friction between driven nut (15) and positioning sleeve (6) inner face；Driven nut (15) is by circle distribution in three on positioning sleeve (6)
A holding screw (17) limit, it is fixed on driven nut (15) on positioning sleeve (6) and can only move in a circle；Active block
(14) it is fixed on runner assembly (7) using split pin, active block (14) is rotatable, and rocking bar (19) is connected to by pin shaft (16)
On runner assembly (7), it can be rotated upwardly and downwardly around pin shaft (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711095502.7A CN109760850A (en) | 2017-11-09 | 2017-11-09 | A kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711095502.7A CN109760850A (en) | 2017-11-09 | 2017-11-09 | A kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109760850A true CN109760850A (en) | 2019-05-17 |
Family
ID=66449402
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711095502.7A Pending CN109760850A (en) | 2017-11-09 | 2017-11-09 | A kind of ratchet lifting unmanned plane EO installation vehicle that transverse and longitudinal is adjusted |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109760850A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020253621A1 (en) * | 2019-06-18 | 2020-12-24 | 深圳高度创新技术有限公司 | Support frame fitting structure |
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| CN104148914A (en) * | 2014-08-07 | 2014-11-19 | 天津航天长征火箭制造有限公司 | Posture adjustment assembly system used for butt joint of components of rocket and posture adjustment method |
| CN104229158A (en) * | 2014-09-03 | 2014-12-24 | 上海交通大学 | Six-degree-of-freedom positioning gesture adjusting equipment used for automatic assembling of large barrel-shaped thin-wall construction member |
| CN204279979U (en) * | 2014-11-28 | 2015-04-22 | 中国航天空气动力技术研究院 | A kind of multi-purpose portable unmanned plane posture adjustment motorcycle |
| CN205022922U (en) * | 2015-09-15 | 2016-02-10 | 沈阳飞机工业（集团）有限公司 | Propulsion system of engine mounting pulley sheave group |
| CN206407165U (en) * | 2017-01-19 | 2017-08-15 | 陕西理工学院 | A kind of undercarriage erecting device |
| CN107054687A (en) * | 2017-06-19 | 2017-08-18 | 沈阳飞机工业（集团）有限公司 | A kind of big stroke aircraft bracket of low clearance |
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2017
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| RU2028970C1 (en) * | 1992-08-24 | 1995-02-20 | Авиационный научно-технический комплекс им.А.Н.Туполева | Method of mounting aircraft engine on side pylon of flying vehicle |
| CN102009340A (en) * | 2010-09-07 | 2011-04-13 | 成都立航科技有限公司 | Aircraft engine mounting vehicle |
| CN102001451A (en) * | 2010-11-12 | 2011-04-06 | 浙江大学 | Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method |
| CN103303491A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业（集团）有限公司 | Abutting technological equipment of airplane large components and abutting method thereof |
| CN103935528A (en) * | 2014-05-05 | 2014-07-23 | 沈阳飞研航空设备有限公司 | Engine demounting and mounting trailer |
| CN203889998U (en) * | 2014-05-28 | 2014-10-22 | 郑州飞机装备有限责任公司 | Suspended object lifting installation trolley |
| CN104118576A (en) * | 2014-08-07 | 2014-10-29 | 天津航天长征火箭制造有限公司 | Integrated large-angle rolling and posture adjusting rack car |
| CN104148914A (en) * | 2014-08-07 | 2014-11-19 | 天津航天长征火箭制造有限公司 | Posture adjustment assembly system used for butt joint of components of rocket and posture adjustment method |
| CN104229158A (en) * | 2014-09-03 | 2014-12-24 | 上海交通大学 | Six-degree-of-freedom positioning gesture adjusting equipment used for automatic assembling of large barrel-shaped thin-wall construction member |
| CN204279979U (en) * | 2014-11-28 | 2015-04-22 | 中国航天空气动力技术研究院 | A kind of multi-purpose portable unmanned plane posture adjustment motorcycle |
| CN205022922U (en) * | 2015-09-15 | 2016-02-10 | 沈阳飞机工业（集团）有限公司 | Propulsion system of engine mounting pulley sheave group |
| CN206407165U (en) * | 2017-01-19 | 2017-08-15 | 陕西理工学院 | A kind of undercarriage erecting device |
| CN107054687A (en) * | 2017-06-19 | 2017-08-18 | 沈阳飞机工业（集团）有限公司 | A kind of big stroke aircraft bracket of low clearance |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2020253621A1 (en) * | 2019-06-18 | 2020-12-24 | 深圳高度创新技术有限公司 | Support frame fitting structure |
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Application publication date: 20190517 |