CN108860634A - A kind of Novel helicopter carrying detection instrument connecting platform - Google Patents
A kind of Novel helicopter carrying detection instrument connecting platform Download PDFInfo
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- CN108860634A CN108860634A CN201810494935.8A CN201810494935A CN108860634A CN 108860634 A CN108860634 A CN 108860634A CN 201810494935 A CN201810494935 A CN 201810494935A CN 108860634 A CN108860634 A CN 108860634A
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- 238000001514 detection method Methods 0.000 title claims abstract description 133
- 230000008844 regulatory mechanism Effects 0.000 claims abstract description 43
- 239000000523 sample Substances 0.000 claims abstract description 37
- 230000007246 mechanism Effects 0.000 claims abstract description 36
- 230000005484 gravity Effects 0.000 claims abstract description 11
- 238000009827 uniform distribution Methods 0.000 claims abstract description 7
- 238000004804 winding Methods 0.000 claims description 16
- 230000008602 contraction Effects 0.000 claims description 3
- 230000001105 regulatory effect Effects 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 238000005516 engineering process Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
- 239000003643 water by type Substances 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- Aviation & Aerospace Engineering (AREA)
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- Geophysics And Detection Of Objects (AREA)
Abstract
A kind of Novel helicopter carries detection instrument connecting platform and belongs to spacecraft carrying platform technical field, it is therefore intended that solves the problems, such as that structure function of the existing technology is single, occupied space is big and cannot flexibly change.The present invention includes：Attitude regulation mechanism；It is fixed on the preceding probe unit of attitude regulation mechanism lower end, preceding probe unit includes the telescopic preceding detection bar and the front end guiding mechanism that the preceding detection bar other end is arranged in that one end is connected with auxiliary fixing member；Two groups of side probe units of attitude regulation mechanism lower end are connected to, every group of side probe unit includes that a folding side detects bar, and one end of side detection bar is connected with auxiliary fixing member；Two side detection bars and preceding detection bar circumference uniform distribution；It is fixed on the counterweight balancing unit of attitude regulation mechanism lower end；And gravity sensor and master controller in attitude regulation mechanism are set, master controller adjusts attitude regulation mechanism kinematic, main controller controls molar behavior according to the information that gravity sensor acquires.
Description
Technical field
The invention belongs to spacecraft carrying platform technical fields, and in particular to a kind of Novel helicopter carrying detection instrument company
Connect platform.
Background technique
China has a vast territory, and there are bigger differences in different areas for topographic structure, this brings greatly to resource detection
Difficulty.In addition China territorial waters is resourceful, but yield is less, the reason is that exploration difficulty is big, lacks platform, state needs newly still
Type resource detection equipment.And as earth's surface mine, superficial part mine, mine easy to identify gradually decrease, country even proposes deep resource
Exploration planning.And with the fast development of unmanned air vehicle technique, make it possible to solve the airborne geophysical prospecting of large scale, highly difficult operation
Technology has new developing direction --- --- unmanned plane airborne geophysical prospecting.And unmanned plane limited dimension, it is not able to satisfy resource spy
The carrying demand of measurement equipment, currently, unmanned plane and the carrying connection platform construction of resource detection equipment are simple, idle is taken up space
It is larger；It when execution task, in certain special circumstances, cannot flexibly change, bring to detection data and analysis compared with burden.
Summary of the invention
It is an object of the invention to propose that a kind of Novel helicopter carries detection instrument connecting platform, solves the prior art and deposit
The problem of structure function is single, occupied space is big and cannot flexibly change.
To achieve the above object, a kind of Novel helicopter of the invention carrying detection instrument connecting platform includes：
The attitude regulation mechanism that upper end is connected with unmanned helicopter adjusts the posture of attitude regulation mechanism lower end；
The preceding probe unit of attitude regulation mechanism lower end, the preceding probe unit packet are fixed on by auxiliary fixing member
Include the telescopic preceding detection bar and the front end Guiding machine that the preceding detection bar other end is set that one end is connected with auxiliary fixing member
Structure；
Two groups of side probe units of attitude regulation mechanism lower end are connected to, every group of side probe unit, which includes one, to be rolled over
Folded side detects bar, and one end of the side detection bar is connected with the auxiliary fixing member, and the other end is free end；Two side detections
Bar and preceding detection bar circumference uniform distribution；
The counterweight balancing unit of attitude regulation mechanism lower end is fixed on by auxiliary fixing member；
And gravity sensor and master controller in the attitude regulation mechanism are set, the master controller is according to weight
The information of force snesor acquisition adjusts attitude regulation mechanism kinematic, probe unit, side probe unit before the main controller controls
And counterweight balancing unit movement.
The attitude regulation mechanism includes：
The silent flatform being fixedly connected with unmanned helicopter；
With silent flatform moving platform disposed in parallel, the auxiliary fixing member is fixed on the moving platform, described heavy
Force snesor is fixed on the moving platform center；
And six attitude regulation electric cylinders between silent flatform and moving platform are connected to, each attitude regulation electric cylinders two
End is hinged by a universal joint and silent flatform and moving platform respectively.
The side detects bar：
The first detection bar that one end is connected with attitude regulation mechanism lower end；
And one end and the first another end in contact of detection bar and the second detection bar being coaxially disposed.
Side detection bar cross section is drops, is large end face by the side of nearby probe unit.
The side probe unit further includes fold mechanism, and the fold mechanism includes：
With the vertical pivot of the first detection bar other end key connection；
It is connected to the hole set of vertical pivot one end；
It is connected to the terminal pad of the vertical pivot other end；
The hole set is fixedly connected by a connecting rod with the second detection bar with the terminal pad；
Folded spring, the folded spring are placed in the disk of terminal pad, and folded spring both ends are separately connected by T shape
On vertical pivot and terminal pad；
And the first servo motor in the attitude regulation mechanism is set, the first servo motor and a winding
The connection of line one end, the other end for winding line are wrapped on the set excircle of hole.
The fold mechanism further includes side electric cylinders, and the side electric cylinders are fixed on the first detection bar, when the second detection
Through-hole when bar and the first detection bar are fully deployed, in the relatively described terminal pad of side electric cylinders with the side electric cylinders corresponding position
It stretches out or retracts.
Detection bar includes before described：
Female detection bar that one end is fixedly connected with the auxiliary fixing member；
One end and female coaxially connected son of the bar other end that detects detect bar；
And the flexible electric cylinders of female detection bar and son detection bar junction are set.
The front end guiding mechanism includes：
It is fixed on the leading to electric cylinders of the sub- detection bar other end；
Multiple preceding guide links of the circumference uniform distribution on the outside of the sub- detection bar, described preceding guide link one end and it is described before
Guiding electric cylinders output end is hinged, and the other end is free end；
And the multiple guiding wings being separately connected with multiple preceding guide rods, each described guiding wing one end and it is described before
Guide rod is hinged, and the other end and the sub- detection bar are slidably matched.
The preceding probe unit further includes automatic winding wire device, and the automatic winding wire device includes：
The crust of the device being fixed on the sub- detection bar；
The inner ring that on described device shell and opposite sets shell rotates is set；
With the motionless horizontal axis of crust of the device one, the motionless horizontal axis and inner ring coaxial arrangement；
And be arranged between inner ring and motionless horizontal axis around wire spring, the coiling both ends of the spring is T-type, respectively and not
It is connected on the inside of dynamic horizontal axis and inner ring, when current detection bar is completely in contraction, in the raw around wire spring.
The counterweight balancing unit includes：
The counterweight guide rod that one end is fixedly connected with attitude regulation mechanism lower end surface, the counterweight guide rod and described
Preceding detection bar coaxial arrangement；
It is connected to the balance weight mechanism of the counterweight guide rod other end, the balance weight mechanism includes being fixed on the counterweight to lead
The clump weight and and the lead screw cooperated to the counter-balanced carriage, the lead screw that is arranged on counter-balanced carriage and the lead screw of the bar other end
Second servo motor of connection；
And it is connected to guiding mechanism after two groups of balance weight mechanism both ends, rear guiding mechanism described in every group includes being fixed on institute
State the rear guiding electric cylinders on counter-balanced carriage, one end with it is described after guiding electric cylinders the output end push rod, one end and the institute's push rod that connect it is another
Guide links and two tail portion wings after end hinged two is symmetrically arranged, two tail portion wing one end are respectively with two
The other end of a push rod is hinged, and the other end and the counter-balanced carriage of the tail portion wing are hinged.
Beneficial effects of the present invention are：A kind of Novel helicopter of the invention carries detection instrument connecting platform and may be implemented
Detection instrument is carried on helicopter, the connection with unmanned helicopter is realized by the silent flatform of attitude regulation mechanism, by preceding
The preceding detection bar of probe unit and the side detection bar of side probe unit realize the carrying of detection instrument；Keep adopting for detection instrument
Sample is stablized.During non-executing task, the preceding probe unit and side probe unit of connecting platform can realize flexible and folding function respectively
Can, space occupied is saved, the automatic winding wire device of front side feeler lever is mounted on, it can be by the electric wire of connecting power device and electric cylinders
It packs up.
During execution task, the signal that master controller can be passed to by gravity sensor carries out attitude regulation mechanism
Control makes connecting platform keep lateral stability by the lateral position of the adjusting clump weight of main controller controls.Two sides detect bar
Drops shape and front and back end connecting platform guide frame, reduce in-flight suffered resistance, maintain the steady of flight
It is qualitative.
Detailed description of the invention
Fig. 1 is that a kind of Novel helicopter of the invention carries detection instrument connecting platform depression angle overall structure diagram；
Fig. 2 is that a kind of Novel helicopter of the invention carries detection instrument connecting platform upward view angle overall structure diagram；
Fig. 3 is that a kind of Novel helicopter of the invention carries detection instrument connecting platform side view；
Fig. 4 is that a kind of Novel helicopter of the invention carries detection instrument connecting platform left view；
Fig. 5 is that a kind of Novel helicopter of the invention carries detection instrument connecting platform top view；
Fig. 6 is that a kind of Novel helicopter of the invention carries detection instrument connecting platform rearview；
Fig. 7 is that a kind of Novel helicopter of the invention carries attitude regulation mechanism structure signal in detection instrument connecting platform
Figure；
Fig. 8 is that a kind of Novel helicopter of the invention carries preceding probe unit structural representation in detection instrument connecting platform
Figure；
Fig. 9 is that a kind of Novel helicopter of the invention carries automatic winding wire device structure in detection instrument connecting platform
Schematic diagram；
Figure 10 is that a kind of Novel helicopter of the invention carries side probe unit structural representation in detection instrument connecting platform
Figure；
Figure 11 is that a kind of Novel helicopter of the invention carries fold mechanism structural schematic diagram in detection instrument connecting platform；
Figure 12 is that a kind of Novel helicopter of the invention carries balance weight mechanism structural schematic diagram in detection instrument connecting platform；
Figure 13 is guiding mechanism structural representation after a kind of Novel helicopter of the invention carries in detection instrument connecting platform
Figure；
Wherein：1, attitude regulation mechanism, 101, silent flatform, 102, moving platform, 103, attitude regulation electric cylinders, 104, universal
Section, 105, auxiliary fixing member, 2, preceding probe unit, 201, female detection bar, 202, sub- detection bar, 203, flexible electric cylinders, 204, preceding
It is oriented to electric cylinders, 205, preceding guide link, 206, guiding wing, 207, motionless horizontal axis, 208, coiling, 209, around wire spring,
210, inner ring, 3, side probe unit, the 301, first detection bar, the 302, second detection bar, 303, vertical pivot, 304, hole set, 305, company
Connect disk, 306, connecting rod, 307, folded spring, 308, first servo motor, 309, side electric cylinders, 4, counterweight balancing unit, 401,
Counterweight guide rod, 402, counter-balanced carriage, 403, lead screw, 404, clump weight, the 405, second servo motor, 406, be oriented to electric cylinders afterwards,
407, push rod, 408, rear guide link, 409, tail portion wing, 5, gravity sensor, 6, master controller.
Specific embodiment
Embodiments of the present invention are described further with reference to the accompanying drawing.
Referring to attached drawing 1- attached drawing 6, a kind of Novel helicopter of the invention carries detection instrument connecting platform and includes：
The attitude regulation mechanism 1 that upper end is connected with unmanned helicopter adjusts the posture of 1 lower end of attitude regulation mechanism；
It is fixed on the preceding probe unit 2 of 1 lower end of attitude regulation mechanism by auxiliary fixing member 105, is detected before described
Unit 2 include one end and auxiliary fixing member 105 connect it is telescopic before detection bar and the preceding detection bar other end is set
Front end guiding mechanism；
Two groups of side probe units 3 of 1 lower end of attitude regulation mechanism are connected to, every group of side probe unit 3 includes one
Folding side detects bar, and one end of the side detection bar and the auxiliary fixing member 105 connect, and the other end is free end；Two
A side detection bar and preceding detection bar circumference uniform distribution；
The counterweight balancing unit 4 of 1 lower end of attitude regulation mechanism is fixed on by auxiliary fixing member 105；
And gravity sensor 5 and master controller 6 in the attitude regulation mechanism 1, the master controller 6 are set
The information adjustment attitude regulation mechanism 1 acquired according to gravity sensor 5 moves, and the master controller 6 controls preceding probe unit 2, side
Probe unit 3 and counterweight balancing unit 4 act.
Referring to attached drawing 7, the attitude regulation mechanism 1 includes：
The silent flatform 101 being fixedly connected with unmanned helicopter；
With the silent flatform 101 moving platform 102 disposed in parallel, the auxiliary fixing member 105 is fixed on the moving platform
On 102, the gravity sensor 5 is fixed on 102 center of moving platform；
And it is connected to six attitude regulation electric cylinders 103 between silent flatform 101 and moving platform 102, each posture
It adjusts 103 both ends of electric cylinders and passes through a universal joint 104 and silent flatform 101 and moving platform 102 respectively hingedly.Master controller 6 controls
102 balance and stability of moving platform of 103 action drives lower end of attitude regulation electric cylinders.
Referring to attached drawing 10, the side detection bar includes：
The first detection bar 301 that one end is connected with 1 lower end of attitude regulation mechanism；
And one end and it is described first detection another end in contact of bar 301 and be coaxially disposed second detection bar 302.
Side detection bar cross section is drops, is large end face by the side of nearby probe unit 2, reduces platform and executes
Suffered resistance when task.
Referring to attached drawing 11, the side probe unit 3 further includes fold mechanism, and the fold mechanism includes：
With the vertical pivot 303 of the first detection 301 other end of bar key connection；
It is connected to the hole set 304 of 303 one end of vertical pivot；
It is connected to the terminal pad 305 of 303 other end of vertical pivot；
The hole set 304 and the terminal pad 305 pass through a connecting rod 306 and the fixed company of the second detection bar 302
It connects；
Folded spring 307, the folded spring 307 are placed in the disk of terminal pad 305, and 307 both ends of folded spring are logical
T shape is crossed to be connected on vertical pivot 303 and terminal pad 305；
And the first servo motor 308 in the attitude regulation mechanism 1 is set, 308 He of first servo motor
One winding line one end connection, the other end for winding line are wrapped in hole and cover on 304 excircles.
The side detection bar that attitude regulation structure two sides are arranged in is folding structure, and one end of the first detection bar 301 passes through
Bolt and nut is connected to 102 lower section of moving platform of attitude regulation mechanism 1, and for the other end with vertical pivot 303 by being keyed, second detects bar
302 one end connect firmly winding bore set 304 and folded spring 307, and folded spring 307 detects bar with first respectively by T shape piece
301, the second detection bar 302 is connected, and bore portion forms bolt and nut with the first detection bar 301 and is connected, the hole cover 304 with twine
Coiling connection, the other end are connect with first servo motor 308, and first servo motor 308 rotates coiling, and the winding line other end pulls
Hole set 304 is rotated around vertical pivot 303, when reaching designated position, by 309 company of extending through of side electric cylinders being fixed on the first detection bar 301
The through-hole connect on disk 305 is fixed, and is realized that the position of the first detection detection bar 302 of bar 301, second is fixed, is worked as first servo motor
308 rotate backward, and hole set 304 leans on 307 spring return initial position of folded spring, realize the first detection bar 301 and the second detection
The folding of bar 302 reduces space waste with this.
Referring to attached drawing 8, detecting bar before described includes：
Female detection bar 201 that one end is fixedly connected with the auxiliary fixing member 105；
One end and female coaxially connected son of 201 other end of bar that detects detect bar 202；
And the flexible electric cylinders 203 of female detection bar 201 and son detection 202 junction of bar are set.
The front end guiding mechanism includes：
It is fixed on the leading to electric cylinders 204 of sub- 202 other end of detection bar；
Multiple preceding guide links 205 of the circumference uniform distribution in sub- 202 outside of detection bar, the preceding guide link 205 1
It holds and described leading hinged to 204 output end of electric cylinders, the other end is free end；
And the multiple guiding wings 206 being separately connected with multiple preceding guide rods, each described 206 one end of guiding wing and
The preceding guide rod is hinged, and the other end and the sub- detection bar 202 are slidably matched.
Detection bar is retractable structure before described, and sub- detection bar 202 and female detection bar 201 are coaxially connected, realizes that detection is set
Standby required space layout position, on mother's detection bar 201, the guiding mechanism is umbrella shape mechanism for electric cylinders 203 of stretching setting, Gu
The electric cylinders being scheduled on sub- detection bar 202 are leading to push preceding guide link 205 hinged therewith, preceding guide link 205 to horizontal bar
Guiding wing 206 hinged therewith is supportted, guiding wing 206 is hinged on sub- detection bar 202 by front position, realizes the guiding steady of feeler lever
It is fixed.
Referring to attached drawing 9, the preceding probe unit 2 further includes automatic winding wire device, the automatic winding wire device
Including：
The crust of the device 208 being fixed on the sub- detection bar 202；
The inner ring 210 that on described device shell 208 and opposite sets shell 208 rotates is set, and the inner ring 210 passes through
One cover board is arranged in described device shell 208 and relatively rotates, and electric outlet mouth is provided on cover board；
With the motionless horizontal axis 207 of 208 one of crust of the device, the motionless horizontal axis and inner ring coaxial arrangement；
And be arranged between inner ring 210 and motionless horizontal axis 207 around wire spring 209, it is described to be around 209 both ends of wire spring
T-type is connected on the inside of motionless horizontal axis 207 and inner ring 210 respectively, when current detection bar is completely in contraction, at wire spring 209
In nature.
Referring to attached drawing 12 and attached drawing 13, the counterweight balancing unit 4 includes：
The counterweight guide rod 401 that one end is fixedly connected with 1 lower end surface of attitude regulation mechanism, the counterweight guide rod
401 and preceding detection bar coaxial arrangement；
It is connected to the balance weight mechanism of 401 other end of counterweight guide rod, the balance weight mechanism includes being fixed on described match
What the counter-balanced carriage 402 for being redirected 401 other end of bar, the lead screw 403 being arranged on counter-balanced carriage 402 and the lead screw 403 cooperated matches
Pouring weight 404 and the second servo motor 405 connected with the lead screw 403；
And it is connected to guiding mechanism after two groups of balance weight mechanism both ends, rear guiding mechanism described in every group includes being fixed on institute
State the rear guiding electric cylinders 406 on counter-balanced carriage 402, the push rod 407 that one end is connected with rear guiding 406 output end of electric cylinders, one end
With 407 other ends of institute push rod hinged two it is symmetrically arranged after guide links 408 and two tail portion wings 409, two institutes
State that wing 409 one end in tail portion is hinged with the other end of two push rods 407 respectively, the other end of the tail portion wing 409 and described
Counter-balanced carriage 402 is hinged.
The second servo motor 405 that 401 rear end of counterweight guide rod is arranged in is rotated by lead screw 403, and then realization and silk
The clump weight 404 that thick stick 403 cooperates is moved left and right along rear counter-balanced carriage 402, realizes that the left and right of integral platform in some cases is matched
Galassing weighing apparatus；The push rod 407 that is symmetricly set in the guiding mechanism of weight linear meter guide rod rear portion two sides push it is hinged therewith after lead
To connecting rod 408, rear guide link 408 supports tail portion wing 409 hinged therewith, and tail portion wing 409 is hinged on counter-balanced carriage 402
Both ends realize that tail portion guiding is stablized.
Claims (10)
1. a kind of Novel helicopter carries detection instrument connecting platform, which is characterized in that including：
The attitude regulation mechanism (1) that upper end is connected with unmanned helicopter adjusts the posture of attitude regulation mechanism (1) lower end；
It is fixed on the preceding probe unit (2) of attitude regulation mechanism (1) lower end by auxiliary fixing member (105), is visited before described
Survey the telescopic preceding detection bar and be arranged another in preceding detection bar that unit (2) include one end and auxiliary fixing member (105) connection
The front end guiding mechanism of one end；
Two groups of side probe units (3) of attitude regulation mechanism (1) lower end are connected to, every group of side probe unit (3) includes one
A folding side detects bar, and one end of the side detection bar and the auxiliary fixing member (105) connection, the other end are freely
End；Two side detection bars and preceding detection bar circumference uniform distribution；
The counterweight balancing unit (4) of attitude regulation mechanism (1) lower end is fixed on by auxiliary fixing member (105)；
And the gravity sensor (5) and master controller (6) being arranged on the attitude regulation mechanism (1), the master controller
(6) it according to information adjustment attitude regulation mechanism (1) movement of gravity sensor (5) acquisition, is visited before master controller (6) control
Survey unit (2), side probe unit (3) and counterweight balancing unit (4) movement.
2. a kind of Novel helicopter according to claim 1 carries detection instrument connecting platform, which is characterized in that the appearance
State regulating mechanism (1) includes：
The silent flatform (101) being fixedly connected with unmanned helicopter；
With the silent flatform (101) moving platform disposed in parallel (102), the auxiliary fixing member (105) is fixed on described dynamic flat
On platform (102), the gravity sensor (5) is fixed on the moving platform (102) center；
And it is connected to six attitude regulation electric cylinders (103) between silent flatform (101) and moving platform (102), each appearance
State adjusts electric cylinders (103) both ends and passes through a universal joint (104) and silent flatform (101) and moving platform (102) respectively hingedly.
3. a kind of Novel helicopter according to claim 1 carries detection instrument connecting platform, which is characterized in that the side
Detecting bar includes：
The first detection bar (301) that one end is connected with attitude regulation mechanism (1) lower end；
And one end and described first detection bar (301) another end in contact and the second detection bar (302) being coaxially disposed.
4. a kind of Novel helicopter according to claim 3 carries detection instrument connecting platform, which is characterized in that the side
Detection bar cross section is drops, is large end face by the side of nearby probe unit (2).
5. a kind of Novel helicopter according to claim 3 carries detection instrument connecting platform, which is characterized in that the side
Probe unit (3) further includes fold mechanism, and the fold mechanism includes：
With the vertical pivot (303) of the first detection bar (301) other end key connection；
It is connected to the hole set (304) of vertical pivot (303) one end；
It is connected to the terminal pad (305) of vertical pivot (303) other end；
The hole set (304) and the terminal pad (305) are solid by a connecting rod (306) and second detection bar (302)
Fixed connection；
Folded spring (307), the folded spring (307) are placed in the disk of terminal pad (305), folded spring (307) two
End is connected on vertical pivot (303) and terminal pad (305) by T shape；
And the first servo motor (308) being arranged on the attitude regulation mechanism (1), the first servo motor (308)
It is connected with a winding line one end, the other end for winding line is wrapped on set (304) excircle of hole.
6. a kind of Novel helicopter according to claim 5 carries detection instrument connecting platform, which is characterized in that the folding
Folded mechanism further includes side electric cylinders (309), and the side electric cylinders (309) are fixed in first detection bar (301), when the second detection
Bar (302) and the first detection bar (301) be when being fully deployed, on the relatively described terminal pad (305) of the side electric cylinders (309) with it is described
The through-hole of side electric cylinders (309) corresponding position is stretched out or is retracted.
7. a kind of Novel helicopter carrying detection instrument connecting platform described in any one of -6 according to claim 1, special
Sign is that detecting bar before described includes：
Female detection bar (201) that one end is fixedly connected with the auxiliary fixing member (105)；
One end and female coaxially connected son of bar (201) other end that detects detect bar (202)；
And setting is in the flexible electric cylinders (203) of female detection bar (201) and son detection bar (202) junction.
8. a kind of Novel helicopter according to claim 7 carries detection instrument connecting platform, which is characterized in that before described
End guiding mechanism include：
It is fixed on the leading to electric cylinders (204) of sub- detection bar (202) other end；
Multiple preceding guide links (205) of the circumference uniform distribution on the outside of the sub- detection bar (202), the preceding guide link (205)
One end and described leading hinged to electric cylinders (204) output end, the other end is free end；
And the multiple guiding wings (206) being separately connected with multiple preceding guide rods, each guiding wing (206) one end and
The preceding guide rod is hinged, and the other end and the sub- detection bar (202) are slidably matched.
9. a kind of Novel helicopter according to claim 8 carries detection instrument connecting platform, which is characterized in that before described
Probe unit (2) further includes automatic winding wire device, and the automatic winding wire device includes：
The crust of the device (208) being fixed on the sub- detection bar (202)；
The inner ring (210) of simultaneously opposite sets shell (208) rotation is set on described device shell (208)；
With the motionless horizontal axis (207) of crust of the device (208) one, the motionless horizontal axis and inner ring coaxial arrangement；
And be arranged between inner ring (210) and motionless horizontal axis (207) around wire spring (209), it is described around wire spring (209) two
End is T-type, is connected respectively on the inside of motionless horizontal axis (207) and inner ring (210), when current detection bar is completely in contraction, coiling
Spring (209) is in the raw.
10. a kind of Novel helicopter according to claim 1 carries detection instrument connecting platform, which is characterized in that described
Counterweight balancing unit (4) includes：
The counterweight guide rod (401) that one end is fixedly connected with attitude regulation mechanism (1) lower end surface, the counterweight guide rod
(401) it is coaxially disposed with the preceding detection bar；
It is connected to the balance weight mechanism of counterweight guide rod (401) other end, the balance weight mechanism includes being fixed on the counterweight
The counter-balanced carriage (402) of guide rod (401) other end, the lead screw (403) and the lead screw (403) being arranged on counter-balanced carriage (402)
The clump weight (404) of cooperation and the second servo motor (405) connected with the lead screw (403)；
And it is connected to guiding mechanism after two groups of balance weight mechanism both ends, rear guiding mechanism described in every group includes being fixed on described match
Weight frame (402) on rear guiding electric cylinders (406), one end with it is described after guiding electric cylinders (406) output end connect push rod (407),
Two symmetrically arranged guide links (408) and the two tail portion wings afterwards of one end and institute push rod (407) other end hingedly
(409), two described tail portion wing (409) one end are hinged with the other end of two push rods (407) respectively, the tail portion wing
(409) the other end and the counter-balanced carriage (402) is hinged.
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|---|---|---|---|
| CN201810494935.8A CN108860634B (en) | 2018-05-22 | 2018-05-22 | Novel helicopter carries on detecting instrument connection platform |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810494935.8A CN108860634B (en) | 2018-05-22 | 2018-05-22 | Novel helicopter carries on detecting instrument connection platform |
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| CN108860634A true CN108860634A (en) | 2018-11-23 |
| CN108860634B CN108860634B (en) | 2021-07-06 |
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| CN201810494935.8A Active CN108860634B (en) | 2018-05-22 | 2018-05-22 | Novel helicopter carries on detecting instrument connection platform |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112504063A (en) * | 2021-02-04 | 2021-03-16 | 湖南华诺星空电子技术有限公司 | Networking detection device with all-terrain adaptability |
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