CN110155360A - One kind is based on aircraft aerial survey positioning bracket - Google Patents
One kind is based on aircraft aerial survey positioning bracket Download PDFInfo
- Publication number
- CN110155360A CN110155360A CN201910416035.6A CN201910416035A CN110155360A CN 110155360 A CN110155360 A CN 110155360A CN 201910416035 A CN201910416035 A CN 201910416035A CN 110155360 A CN110155360 A CN 110155360A
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- China
- Prior art keywords
- fixedly connected
- fixed
- plate
- aerial survey
- aircraft
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- 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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Arresting gear; Liquid barriers
-
- 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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Launching or towing gear
Abstract
The invention discloses one kind based on aircraft aerial survey positioning bracket, it is related to aircraft Aerial Surveying Technology field, including support plate, the bottom surface of the support plate is fixedly connected with supporting leg, the upper surface of the support plate is fixedly connected with fixing seat, and the upper surface fixation of the support plate is inlaid with bearing, and the inner ring of the bearing is fixedly connected with column spinner, the outer surface of the column spinner offers the first fixation hole, and the outer surface of the column spinner is equipped with regulating mechanism.It should be based on aircraft aerial survey positioning bracket, pass through the reflective layer and color difference layer on eye-catching pad, aircraft is facilitated to find the target in aerial survey location, make bottom surface that there is control point, improves the precision of aerophotogrammetry data, improve the working efficiency of later stage work personnel, brake block is fixedly connected with by the upper surface of support plate, the upper surface of brake block offers breaker slot, can reach the inside for facilitating staff brake bar to be sticked into breaker slot, and the working efficiency for improving staff is used.
Description
Technical field
It is specially a kind of based on aircraft aerial survey positioning bracket the present invention relates to aircraft Aerial Surveying Technology field.
Background technique
Aircraft aerial survey is the strong supplement of traditional aerophotogrammetry means, have maneuverability, efficiently quickly, it is fine
Accurately, the features such as operating cost is low, applied widely, with short production cycle, in zonule and flight area in hardship high-resolution shadow
As having a clear superiority in terms of quick obtaining, with the development of aircraft and digital camera technology, the number based on aircraft platforms
Word aerial photographing technology has shown that its unique advantage, and aircraft is combined with aerophotogrammetry so that aircraft number low latitude is distant
Sense becomes a brand-new developing direction in air remote sensing field.
Currently, without specific aircraft riding position, often arbitrarily being put in operating area in daily take photo by plane
It puts, and unmanned vehicle is required due to flying, fuselage makes usually using light and soft material, and fuselage is deposited in the placement position of mistake
In serious security risk, an existing simple bracket mostly can only place a frame aircraft, and change its undercarriage
Angle changing rate trouble causes influences to aerial survey work, and the take photo by plane process of the data such as photography acquisition geography of aircraft is to adopt first
Aerotriangulation is carried out with aircraft and photography of taking photo by plane, at the data progress later period for then taking photo by plane acquired to aircraft
Reason, but the precision of post-processing is not high, and one of main cause is to lack terrestrial positioning point, especially desert, farmland and
In meadow, without obvious target, cause the data precision of aerial survey not high, for this purpose, it is proposed that a kind of used based on aircraft aerial survey is determined
Position bracket.
Summary of the invention
It is a kind of based on aircraft aerial survey positioning the object of the invention is in order to make up for the deficiencies of the prior art, provide
Bracket, it has to change undercarriage angle, has terrestrial positioning point, the high advantage of the data precision of aerial survey has solved
Arch high over changes undercarriage angle changing rate trouble, lacks terrestrial positioning point, the not high problem of the data precision of aerial survey.
The present invention is in order to solve the above technical problems, provide the following technical solutions: one kind is based on aircraft aerial survey positioning support
Frame, including support plate, the bottom surface of the support plate are fixedly connected with supporting leg, and the upper surface of the support plate is fixedly connected with
The upper surface fixation of reservation, the support plate is inlaid with bearing, and the inner ring of the bearing is fixedly connected with column spinner, the rotation
The outer surface of column offers the first fixation hole, and the outer surface of the column spinner is equipped with regulating mechanism, the upper surface of the support plate
Equipped with lift, the upper surface of the fixing seat is fixedly connected with positioning mechanism.
The regulating mechanism includes folder cylinder, the second fixation hole, pin, fixed plate, the second pin shaft, mandril, support rod, first
Pin shaft and card slot.
The lift includes fixing pipe, fixed ring, the plate that rises and falls, fixed cone, foam-rubber cushion, snap-gauge, inflator, snap ring, leads to
Tracheae, connector, air pump and connecting tube.
The positioning mechanism includes groove, support frame, fixed disk, fixed case, through-hole, support column, supporting plate, locating slot, wakes up
Mesh pad, color difference layer, reflective layer and rubber pad.
Further, the outer surface of the column spinner is connected with folder cylinder, and it is fixed that the outer surface of the folder cylinder offers second
Hole, the inside of second fixation hole are connected with pin, and the right side of the folder cylinder is fixedly connected with fixed plate, the fixed plate
Top support rod is fixedly hinged with by the first pin shaft.
By using above-mentioned technical proposal, the take-off angle for facilitating and adjusting aircraft can be reached, improved aircraft
Efficiency of taking off.
Further, the right end of the support rod is fixedly connected with fixing pipe, and the bottom surface of the fixing pipe is fixedly connected with
The inside fixation of inflator, the inflator is communicated with snorkel, and the snorkel is fixedly connected with connector far from one end of inflator, institute
The top for stating fixing pipe is fixedly connected with fixed ring, and the top of the fixed ring is fixedly connected with the plate that rises and falls, the plate that rises and falls
Upper surface is fixedly connected with fixed cone, and the left and right ends of the plate that rises and falls are fixedly connected to snap-gauge, the upper table of the support plate
Face is fixedly connected with air pump, and the output end of the air pump is fixedly connected with connecting tube.
By using above-mentioned technical proposal, apply power-assisted when can reach to aircraft takeoff, when being aircraft takeoff
Increase power.
Further, the upper surface of the fixing seat opens up fluted, and the inside of the groove is connected with support frame, described
The upper surface of support frame is fixedly connected with fixed disk, and the upper surface of the fixed disk offers through-hole, the bottom surface of the fixed disk
It is fixedly connected with fixed case, the inner ring of the through-hole is connected with support column, and the support column is through through-hole and extends to fixed case
Inside, the top of the fixed case is fixedly connected with supporting plate, and the upper surface of the supporting plate offers locating slot, the locating slot
Inner bottom wall be fixed with eye-catching pad, the upper surface of the eye-catching pad is fixedly connected with color difference layer, the upper surface of the eye-catching pad
It is fixed with reflective layer.
By using above-mentioned technical proposal, it can reach convenient for discovery aerial survey target, improve the precision of aerial survey.
Further, the bottom surface of the support rod offers card slot, and the outer surface of the fixed plate is solid by the second pin shaft
Surely it is hinged with mandril.
By using above-mentioned technical proposal, the fixation convenient for staff to support rod can be reached, facilitated aircraft
Rise and fall.
Further, the mandril is connected to the inside of card slot, the interior bottom of the fixed case far from one end of the second pin shaft
Wall is fixedly connected with rubber pad.
By using above-mentioned technical proposal, support rod is fixed in the inside that can reach makes mandril stick into card slot, is mentioned
The high convenience of fixed support rod.
Further, the bottom surface of the fixed plate is fixedly connected with snap ring, and the snorkel is wrapped in the outer surface of snap ring.
By using above-mentioned technical proposal, it can reach and snorkel has been wound, prevent snorkel is in disorder from making
The injury of pairs of snorkel, improves the protectiveness to snorkel.
Further, the upper surface of the plate that rises and falls is fixedly connected with foam-rubber cushion, and the thickness of the foam-rubber cushion is at least one
Centimetre.
By using above-mentioned technical proposal, the vibration generated when reducing the mobile device can be reached, aircraft has been made
At influence, improve the protectiveness to aircraft.
Further, the outer surface of the column spinner is fixedly connected with connecting rod, and the connecting rod is solid by third pin shaft
Surely it is hinged with brake bar.
By using above-mentioned technical proposal, it can reach and staff is facilitated to brake column spinner, improve this
The stability of device.
Further, the upper surface of the support plate is fixedly connected with brake block, and the upper surface of the brake block offers
Breaker slot.
By using above-mentioned technical proposal, the inside for facilitating staff brake bar to be sticked into breaker slot can have been reached,
Improve the working efficiency of staff.
Compared with prior art, should be had based on aircraft aerial survey positioning bracket it is following the utility model has the advantages that
1, the present invention then lifts support rod and mandril is allowed to stick into card slot by rotation column spinner adjustment direction and angle
Inside is supported support rod, then aircraft is placed on standby for takeoff on the plate that rises and falls, then by air pump to aircraft
Take off and apply power-assisted, by the reflective layer and color difference layer on eye-catching pad, facilitate aircraft to find the target in aerial survey location, make bottom
Face has control point, improves the precision of aerophotogrammetry data, improves the working efficiency of later stage work personnel, receives after the completion of aerial survey
It plays support rod and facilitates next use, card slot is offered by the bottom surface of support rod, the outer surface of fixed plate is solid by the second pin shaft
Surely it is hinged with mandril, the fixation convenient for staff to support rod can have been reached, facilitates rising and falling for aircraft.
2, the present invention is connected to the inside of card slot by mandril far from one end of the second pin shaft, and the inner bottom wall of fixed case is fixed
It is connected with rubber pad, support rod is fixed in the inside that can reach makes mandril stick into card slot, improves fixed support rod
Convenience is fixedly connected with snap ring by the bottom surface of fixed plate, and snorkel is wrapped in the outer surface of snap ring, can reach to logical
Tracheae is wound, and is prevented the snorkel injury in disorder caused to snorkel, is improved the protectiveness to snorkel, pass through
The rise and fall upper surface of plate is fixedly connected with foam-rubber cushion, and the thickness of foam-rubber cushion is at least one centimetre, and can reach reduces movement
The vibration generated when the device influence caused by aircraft, improves the protectiveness to aircraft, passes through the upper table of support plate
Face is fixedly connected with brake block, and the upper surface of brake block offers breaker slot, can reach and facilitate staff brake bar
The inside for sticking into breaker slot improves the working efficiency of staff.
Detailed description of the invention
Fig. 1 is the cross-sectional view of column spinner front view of the present invention；
Fig. 2 is the top view of the eye-catching pad of the present invention；
Fig. 3 is the cross-sectional view of fixed case front view of the present invention；
Fig. 4 is structure enlargement diagram at A in Fig. 1 of the present invention；
Fig. 5 is structure enlargement diagram at B in Fig. 1 of the present invention.
In figure: 1, regulating mechanism；101, cylinder is pressed from both sides；102, the second fixation hole；103, pin；104, fixed plate；105, second
Pin shaft；106, mandril；107, support rod；108, the first pin shaft；109, card slot；2, lift；201, fixing pipe；202, fixed
Ring；203, rise and fall plate；204, fixed cone；205, foam-rubber cushion；206, snap-gauge；207, inflator；208, snap ring；209, snorkel；
210, connector；211, air pump；212, connecting tube；3, positioning mechanism；301, groove；302, support frame；303, fixed disk；304, solid
Determine case；305, through-hole；306, support column；307, supporting plate；308, locating slot；309, eye-catching pad；310, color difference layer；311, reflective
Layer；312, rubber pad；4, supporting leg；5, support plate；6, bearing；7, fixing seat；8, column spinner；9, the first fixation hole；10, it connects
Bar；11, third pin shaft；12, brake bar；13, brake block；14, breaker slot.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig. 1-5, the present invention provides a kind of technical solution: one kind positioning bracket based on aircraft aerial survey, including
Support plate 5, the bottom surface of support plate 5 are fixedly connected with supporting leg 4, and the upper surface of support plate 5 is fixedly connected with fixing seat 7, support
The upper surface fixation of plate 5 is inlaid with bearing 6, and the inner ring of bearing 6 is fixedly connected with column spinner 8, and the outer surface of column spinner 8 offers
First fixation hole 9, the outer surface of column spinner 8 are equipped with regulating mechanism 1, and the upper surface of support plate 5 is equipped with lift 2, fixing seat 7
Upper surface be fixedly connected with positioning mechanism 3.
Regulating mechanism 1 includes folder cylinder 101, the second fixation hole 102, pin 103, fixed plate 104, the second pin shaft 105, mandril
106, support rod 107, the first pin shaft 108 and card slot 109.
Lift 2 includes fixing pipe 201, fixed ring 202, the plate 203 that rises and falls, fixed cone 204, foam-rubber cushion 205, snap-gauge
206, inflator 207, snap ring 208, snorkel 209, connector 210, air pump 211 and connecting tube 212.
Positioning mechanism 3 include groove 301, support frame 302, fixed disk 303, fixed case 304, through-hole 305, support column 306,
Supporting plate 307, locating slot 308, eye-catching pad 309, color difference layer 310, reflective layer 311 and rubber pad 312.
Further, the outer surface of column spinner 8 is connected with folder cylinder 101, and the outer surface of folder cylinder 101 offers the second fixation hole
102, the inside of the second fixation hole 102 is connected with pin 103, and the right side of folder cylinder 101 is fixedly connected with fixed plate 104, fixed
The top of plate 104 is fixedly hinged with support rod 107 by the first pin shaft 108, can reach and facilitate taking off for adjusting aircraft
Angle improves the efficiency of taking off of aircraft.
Further, the right end of support rod 107 is fixedly connected with fixing pipe 201, and the bottom surface of fixing pipe 201 is fixedly connected with
The inside fixation of inflator 207, inflator 207 is communicated with snorkel 209, and snorkel 209 is fixedly connected with far from one end of inflator 207
Connector 210, the top of fixing pipe 201 are fixedly connected with fixed ring 202, and the top of fixed ring 202 is fixedly connected with the plate that rises and falls
203, the upper surface for the plate 203 that rises and falls is fixedly connected with fixed cone 204, and the left and right ends for the plate 203 that rises and falls are fixedly connected to snap-gauge
206, the upper surface of support plate 5 is fixedly connected with air pump 211, and the output end of air pump 211 is fixedly connected with connecting tube 212, can
Apply power-assisted when having reached to aircraft takeoff, increases power when being aircraft takeoff.
Further, the upper surface of fixing seat 7 opens up fluted 301, and the inside of groove 301 is connected with support frame 302, branch
The upper surface of support 302 is fixedly connected with fixed disk 303, and the upper surface of fixed disk 303 offers through-hole 305, fixed disk 303
Bottom surface is fixedly connected with fixed case 304, and the inner ring of through-hole 305 is connected with support column 306, and support column 306 is through through-hole 305 and prolongs
The inside of fixed case 304 is extended to, the top of fixed case 304 is fixedly connected with supporting plate 307, and the upper surface of supporting plate 307 offers fixed
Position slot 308, the inner bottom wall of locating slot 308 are fixed with eye-catching pad 309, and the upper surface of eye-catching pad 309 is fixedly connected with color difference layer
310, the upper surface of eye-catching pad 309 is fixed with reflective layer 311, can reach convenient for discovery aerial survey target, improve aerial survey
Precision.
Further, the bottom surface of support rod 107 offers card slot 109, and the outer surface of fixed plate 104 passes through the second pin shaft
105 are fixedly hinged with mandril 106, can reach the fixation convenient for staff to support rod 107, facilitate rising for aircraft
It falls.
Further, mandril 106 is connected to the inside of card slot 109 far from one end of the second pin shaft 105, fixed case 304
Inner bottom wall is fixedly connected with rubber pad 312, and support rod 107 is consolidated in the inside that can reach makes mandril 106 stick into card slot 109
It is fixed, improve the convenience of fixed support rod 107.
Further, the bottom surface of fixed plate 104 is fixedly connected with snap ring 208, and snorkel 209 is wrapped in the outer of snap ring 208
Surface can reach and be wound to snorkel 209, prevent the wound in disorder caused to snorkel 209 of snorkel 209
Evil, improves the protectiveness to snorkel 209.
Further, the rise and fall upper surface of plate 203 is fixedly connected with foam-rubber cushion 205, and the thickness of foam-rubber cushion 205 is at least one
Centimetre, the vibration influence caused by aircraft generated when reducing the mobile device can have been reached, improved to aircraft
Protectiveness.
Further, the outer surface of column spinner 8 is fixedly connected with connecting rod 10, and connecting rod 10 is fixed by third pin shaft 11
It is hinged with brake bar 12, can reach and staff is facilitated to brake column spinner 8, improves the stability of the device.
Further, the upper surface of support plate 5 is fixedly connected with brake block 13, and the upper surface of brake block 13 offers braking
Slot 14 can reach the inside for facilitating staff brake bar 12 to be sticked into breaker slot 14, improve the work of staff
Efficiency.
Working principle: being first put into the device position of suitable aerial survey, and then air pump 211 is connected with municipal power supply
It is logical, snorkel 209 is connect again with the connecting tube 212 of 211 output end of air pump then, then passes through rotation 8 side of adjustment of column spinner
To and angle, then support rod 107 is lifted the inside for allowing mandril 106 to stick into card slot 109 and support rod 107 is supported, so
Aircraft is placed on afterwards standby for takeoff on the plate 203 that rises and falls, power-assisted is then applied to taking off for aircraft by air pump 211, led to
The reflective layer 311 and color difference layer 310 on eye-catching pad 309 are crossed, aircraft is facilitated to find the target in aerial survey location, makes bottom surface that there is control
It is processed, the precision of aerophotogrammetry data is improved, the working efficiency of later stage work personnel is improved, support rod is packed up after the completion of aerial survey
107 facilitate next use.
In the description of the present invention, the terms "include", "comprise" or its any other variant are intended to nonexcludability
Include so that include a series of elements process, method, article or equipment not only include those elements, but also
Including other elements that are not explicitly listed, or further include for this process, method, article or equipment intrinsic want
Element.In the absence of more restrictions, the element limited by sentence " including a reference structure ", it is not excluded that including institute
State in the process, method, article or equipment of element that there is also other identical elements.It should be noted that, in this document, all
As the relational terms of " first ", " second " or the like are used merely to an entity or operation and another entity or operating space
It separates, without necessarily requiring or implying between these entities or operation, there are any actual relationship or orders.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (10)
1. one kind is fixedly connected based on aircraft aerial survey with positioning bracket, including support plate (5), the bottom surface of the support plate (5)
Have supporting leg (4), the upper surface of the support plate (5) is fixedly connected with fixing seat (7), and the upper surface of the support plate (5) is solid
Surely it is inlaid with bearing (6), the inner ring of the bearing (6) is fixedly connected with column spinner (8), and the outer surface of the column spinner (8) is opened
Equipped with the first fixation hole (9), it is characterised in that: the outer surface of the column spinner (8) is equipped with regulating mechanism (1), the support plate
(5) upper surface is equipped with lift (2), and the upper surface of the fixing seat (7) is fixedly connected with positioning mechanism (3)；
The regulating mechanism (1) includes folder cylinder (101), the second fixation hole (102), pin (103), fixed plate (104), the second pin
Axis (105), mandril (106), support rod (107), the first pin shaft (108) and card slot (109)；
The lift (2) includes fixing pipe (201), fixed ring (202), the plate that rises and falls (203), fixed cone (204), foam-rubber cushion
(205), snap-gauge (206), inflator (207), snap ring (208), snorkel (209), connector (210), air pump (211) and connecting tube
(212)；
The positioning mechanism (3) includes groove (301), support frame (302), fixed disk (303), fixed case (304), through-hole
(305), support column (306), supporting plate (307), locating slot (308), eye-catching pad (309), color difference layer (310), reflective layer (311) and
Rubber pad (312).
2. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the column spinner
(8) outer surface is connected with folder cylinder (101), and the outer surface of folder cylinder (101) offers the second fixation hole (102), and described the
The inside of two fixation holes (102) is connected with pin (103), and the right side of folder cylinder (101) is fixedly connected with fixed plate
(104), the top of the fixed plate (104) is fixedly hinged with support rod (107) by the first pin shaft (108).
3. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the support rod
(107) right end is fixedly connected with fixing pipe (201), and the bottom surface of the fixing pipe (201) is fixedly connected with inflator (207), institute
The inside fixation for stating inflator (207) is communicated with snorkel (209), and the snorkel (209) is fixed far from the one end of inflator (207)
It is connected with connector (210), the top of the fixing pipe (201) is fixedly connected with fixed ring (202), the fixed ring (202)
Top is fixedly connected with the plate that rises and falls (203), and the upper surface of the plate that rises and falls (203) is fixedly connected with fixed cone (204), and described
The left and right ends for falling plate (203) are fixedly connected to snap-gauge (206), and the upper surface of the support plate (5) is fixedly connected with air pump
(211), the output end of the air pump (211) is fixedly connected with connecting tube (212).
4. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the fixing seat
(7) upper surface opens up fluted (301), and the inside of the groove (301) is connected with support frame (302), support frame as described above
(302) upper surface is fixedly connected with fixed disk (303), and the upper surface of the fixed disk (303) offers through-hole (305), institute
The bottom surface for stating fixed disk (303) is fixedly connected with fixed case (304), and the inner ring of the through-hole (305) is connected with support column
(306), the support column (306) runs through through-hole (305) and extends to the inside of fixed case (304), the fixed case (304)
Top is fixedly connected with supporting plate (307), and the upper surface of the supporting plate (307) offers locating slot (308), the locating slot
(308) inner bottom wall is fixed with eye-catching pad (309), and the upper surface of the eye-catching pad (309) is fixedly connected with color difference layer
(310), the upper surface of the eye-catching pad (309) is fixed with reflective layer (311).
5. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the support rod
(107) bottom surface offers card slot (109), and the outer surface of the fixed plate (104) is fixedly hinged with by the second pin shaft (105)
Mandril (106).
6. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the mandril
(106) one end far from the second pin shaft (105) is connected to the inside of card slot (109), and the inner bottom wall of the fixed case (304) is fixed
It is connected with rubber pad (312).
7. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the fixed plate
(104) bottom surface is fixedly connected with snap ring (208), and the snorkel (209) is wrapped in the outer surface of snap ring (208).
8. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the plate that rises and falls
(203) upper surface is fixedly connected with foam-rubber cushion (205), and the thickness of the foam-rubber cushion (205) is at least one centimetre.
9. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the column spinner
(8) outer surface is fixedly connected with connecting rod (10), and the connecting rod (10) is fixedly hinged with braking by third pin shaft (11)
Bar (12).
10. according to claim 1 a kind of based on aircraft aerial survey positioning bracket, it is characterised in that: the support plate
(5) upper surface is fixedly connected with brake block (13), and the upper surface of the brake block (13) offers breaker slot (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910416035.6A CN110155360A (en) | 2019-05-19 | 2019-05-19 | One kind is based on aircraft aerial survey positioning bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910416035.6A CN110155360A (en) | 2019-05-19 | 2019-05-19 | One kind is based on aircraft aerial survey positioning bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110155360A true CN110155360A (en) | 2019-08-23 |
Family
ID=67631387
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910416035.6A Withdrawn CN110155360A (en) | 2019-05-19 | 2019-05-19 | One kind is based on aircraft aerial survey positioning bracket |
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| Country | Link |
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| CN (1) | CN110155360A (en) |
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| CN107902078A (en) * | 2017-12-19 | 2018-04-13 | 刘杰 | A kind of unmanned plane damping base |
| CN108163185A (en) * | 2018-01-12 | 2018-06-15 | 广东翔龙航空技术有限公司 | A kind of integral type undercarriage of unmanned plane |
| CN208149596U (en) * | 2018-05-07 | 2018-11-27 | 石家庄朗和航空科技有限公司 | A kind of unmanned plane shock bracket |
| CN108860640A (en) * | 2018-05-28 | 2018-11-23 | 芜湖千创智能科技有限公司 | A kind of support platform for parking sizes aircraft |
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Application publication date: 20190823 |