CN212333007U - Rotor unmanned aerial vehicle accredited testing organization - Google Patents
Rotor unmanned aerial vehicle accredited testing organization Download PDFInfo
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- CN212333007U CN212333007U CN201922240105.5U CN201922240105U CN212333007U CN 212333007 U CN212333007 U CN 212333007U CN 201922240105 U CN201922240105 U CN 201922240105U CN 212333007 U CN212333007 U CN 212333007U
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Abstract
The utility model discloses a rotor unmanned aerial vehicle testing mechanism, including gallows mechanism and accredited testing organization, be equipped with crossbeam lift coaster on the truss strut, be equipped with the truss crossbeam between the crossbeam lift coaster, the truss strut top is equipped with hand block, the truss crossbeam below is equipped with rope guide pulley, rope and pull up gauge, the ground below the truss crossbeam is equipped with rope guide pulley down, rope and pull down gauge down, truss strut one side ground is equipped with rope spud pile and pull up and down display; the utility model discloses a pull force display can show the current weight of the unmanned aerial vehicle of being hoisted, can also survey pull force under the current rotational speed of unmanned aerial vehicle through the difference of upper and lower pull force simultaneously after the unmanned aerial vehicle engine starts, and this accredited testing organization has improved security, the convenience of test moreover, not only can ensure tester's life safety, and unmanned aerial vehicle explodes the machine in the time of can preventing to test in addition, various flight test work when can accomplishing rotor unmanned aerial vehicle development.
Description
Technical Field
The utility model relates to a rotor unmanned aerial vehicle security test technical field especially relates to a rotor unmanned aerial vehicle accredited testing organization.
Background
In recent years, the unmanned aerial vehicle technology in China is fully developed, and the rotor unmanned aerial vehicle is simple and convenient to operate, convenient to carry, high in environmental adaptability and widely applied to various fields such as military investigation, resource exploration, environmental monitoring, earthquake resistance and disaster relief;
some big load unmanned aerial vehicle, unmanned aerial vehicle weight is great, and the screw size number of using is great, and danger coefficient is higher when the test is driven on ground, when debugging unmanned aerial vehicle flight control system parameter, needs a large amount of flight test to rotor unmanned aerial vehicle simultaneously, consequently, the utility model provides a rotor unmanned aerial vehicle accredited testing organization is in order to solve the problem that exists among the prior art.
SUMMERY OF THE UTILITY MODEL
To the above problem, the utility model aims to provide a rotor unmanned aerial vehicle accredited testing organization, this rotor unmanned aerial vehicle accredited testing organization can show the current weight of the unmanned aerial vehicle of being hoisted through last lower tension display, can also survey the pulling force under the current rotational speed of unmanned aerial vehicle through last lower tension difference simultaneously after the unmanned aerial vehicle engine starts, and this accredited testing organization has improved the security of test moreover, the convenience, not only can ensure tester's life safety, and unmanned aerial vehicle explodes the machine when can preventing to be experimental, various flight test work when can accomplishing rotor unmanned aerial vehicle development.
For realizing the purpose of the utility model, the utility model discloses a following technical scheme realizes: a rotor unmanned aerial vehicle testing mechanism comprises a hanger mechanism and a testing mechanism, wherein the hanger mechanism comprises a traveling frame pillar, fixed supporting legs, a beam lifting pulley, a traveling frame beam, a hand-operated hoist, a beam sling and a hand-operated cable, the traveling frame pillar is fixed on the ground through the fixed supporting legs, the beam lifting pulley is arranged on the traveling frame pillar, the traveling frame beam is arranged between the beam lifting pulleys, the hand-operated hoist is arranged at the top end of the traveling frame pillar, the beam sling and the hand-operated cable are arranged on the hand-operated hoist, the testing mechanism comprises an upper cable guide pulley, an upper cable, an upper tension meter, a lower cable guide pulley, a lower cable, a lower tension meter, a cable fixing pile and upper and lower tension displays, the upper cable guide pulley is arranged below the traveling frame beam, the upper cable is arranged in the upper cable guide pulley, and one end of the upper cable is provided with the upper tension meter, the lower rope guide pulley is arranged on the ground below the travelling crane cross beam, a lower rope is arranged in the lower rope guide pulley, a lower tension meter is arranged at one end of the lower rope, a rope fixing pile is arranged on the ground on one side of the travelling crane strut, and an upper and lower tension display is arranged on the rope fixing pile.
The further improvement lies in that: the beam lifting tackle is sleeved on the truss strut, the hand-operated hoists are provided with two groups, the hand-operated hoists are controlled through the hand-operated inhaul cables, and the beam slings are fixedly connected with the upper portion of the truss beam.
The further improvement lies in that: the upper rope guide pulleys are provided with three groups, one group is arranged in the middle of the lower part of the travelling frame beam, and the lower rope guide pulleys are arranged on the ground right below the middle of the travelling frame beam.
The further improvement lies in that: and the other ends of the upper rope and the lower rope respectively penetrate through the upper rope guide pulley and the lower rope guide pulley and are fixed on the rope fixing piles.
The further improvement lies in that: go up the tensiometer below and be equipped with the connection cable of connecting unmanned aerial vehicle below the tensiometer.
The utility model has the advantages that: the utility model discloses a pull force display can show the current weight of the unmanned aerial vehicle of being hoisted, can also survey pull force under the current rotational speed of unmanned aerial vehicle through the difference of upper and lower pull force simultaneously after the unmanned aerial vehicle engine starts, and this accredited testing organization has improved security, the convenience of test moreover, not only can ensure tester's life safety, and unmanned aerial vehicle explodes the machine in the time of can preventing to test in addition, various flight test work when can accomplishing rotor unmanned aerial vehicle development.
Drawings
Fig. 1 is a perspective front view of the present invention.
Fig. 2 is a schematic view of the fixing support leg of the present invention.
Wherein: 1. a truss strut; 2. fixing the supporting legs; 3. a beam lifting pulley; 4. a truss cross beam; 5. a chain block; 6. a cross-beam sling; 7. a manual cable; 8. a rope guiding pulley is arranged; 9. rope feeding; 10. an upper tension meter; 11. a lower rope guide pulley; 12. rope descending; 13. a lower tension meter; 14. rope fixing piles; 15. an up-down tension display; 16. and connecting a pull rope.
Detailed Description
In order to deepen the understanding of the present invention, the following embodiments will be combined to make the present invention do further details, and the present embodiment is only used for explaining the present invention, and does not constitute the limitation of the protection scope of the present invention.
According to fig. 1 and 2, the embodiment provides a testing mechanism for a rotor unmanned aerial vehicle, which comprises a hanger mechanism and a testing mechanism, wherein the hanger mechanism comprises a traveling frame pillar 1, fixed supporting legs 2, a beam lifting pulley 3, a traveling frame beam 4, a manual hoist 5, a beam sling 6 and a manual cable 7, the traveling frame pillar 1 is fixed on the ground through the fixed supporting legs 2, the beam lifting pulley 3 is arranged on the traveling frame pillar 1, the traveling frame beam 4 is arranged between the beam lifting pulleys 3, the manual hoist 5 is arranged at the top end of the traveling frame pillar 1, the beam sling 6 and the manual cable 7 are arranged on the manual hoist 5, the testing mechanism comprises an upper cable guide pulley 8, an upper cable 9, an upper tension meter 10, a lower cable guide pulley 11, a lower cable 12, a lower tension meter 13, a cable fixing pile 14 and an upper and lower tension display 15, the upper cable guide pulley 8 is arranged below the traveling frame beam 4, an upper rope 9 is arranged in the upper rope guide pulley 8, an upper tension meter 10 is arranged at one end of the upper rope 9, a lower rope guide pulley 11 is arranged on the ground below the truss cross beam 4, a lower rope 12 is arranged in the lower rope guide pulley 11, a lower tension meter 13 is arranged at one end of the lower rope 12, a rope fixing pile 14 is arranged on the ground on one side of the truss strut 1, and an upper tension display 15 and a lower tension display 15 are arranged on the rope fixing pile 14.
Go up rope guide pulley 8 and be equipped with three groups and wherein a set of setting is in the middle part of the below of walking frame crossbeam 4, rope guide pulley 11 sets up subaerially under the middle part of walking frame crossbeam 4 down, go up rope 9 and rope 12 other end down and pass rope guide pulley 8 and rope guide pulley 11 down respectively and be fixed in on rope spud pile 14, it is equipped with the connection cable 16 of connecting unmanned aerial vehicle to go up the tensiometer 10 below and 13 tops of lower tensiometer.
The utility model discloses at first stimulate manual cable 7 simultaneously by two people during the use, improve the take up crossbeam 4 to the take up crossbeam through manual cable 7 control hand block 5, the rotor unmanned aerial vehicle with the test hoists through connecting cable 16 and fixes between last tensiometer 10 and lower tensiometer 13, fix the back with rotor unmanned aerial vehicle, stimulate manual cable 7 control hand block 5 simultaneously by two people again and improve the experimental height that requires with take up crossbeam 4, will go up rope 9 and the 12 other ends of lower rope after highly reacing and fix and can begin the test on rope spud pile 14.
This rotor unmanned aerial vehicle accredited testing organization can show the current weight of unmanned aerial vehicle that is hoisted through last lower tension display 15, can also survey the current rotational speed pull down of unmanned aerial vehicle through last lower tension difference simultaneously after the unmanned aerial vehicle engine starts, this accredited testing organization has improved the security, the convenience of test moreover, not only can ensure tester's life safety, unmanned aerial vehicle explodes the machine when can preventing to test in addition, various flight test work when can accomplishing rotor unmanned aerial vehicle development.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides a rotor unmanned aerial vehicle accredited testing organization which characterized in that: including gallows mechanism and accredited testing organization, gallows mechanism includes framed strut (1), fixed legs (2), crossbeam lifting tackle (3), framed crossbeam (4), hand block (5), crossbeam hoist cable (6) and manual cable (7), framed strut (1) is fixed in ground through fixed legs (2), be equipped with crossbeam lifting tackle (3) on framed strut (1), be equipped with framed crossbeam (4) between crossbeam lifting tackle (3), framed strut (1) top is equipped with hand block (5), be equipped with crossbeam hoist cable (6) and manual cable (7) on hand block (5), accredited testing organization includes cable guide pulley (8), goes up cable (9), goes up tensiometer (10), lower cable guide pulley (11), lower cable (12), lower tensiometer (13), Rope spud pile (14) and upper and lower pulling force display (15), the bank crossbeam (4) below is equipped with rope guide pulley (8), upward be equipped with rope (9) in rope guide pulley (8), it is equipped with tensiometer (10) to go up rope (9) one end, bank crossbeam (4) below ground is equipped with down rope guide pulley (11), be equipped with down rope (12) down in rope guide pulley (11), rope (12) one end is equipped with down tensiometer (13) down, bank pillar (1) one side ground is equipped with rope spud pile (14), pulling force display (15) about being equipped with on rope spud pile (14).
2. The rotary wing drone test mechanism of claim 1, wherein: crossbeam lifting pulley (3) suit is on truss pillar (1), hand hoist (5) are equipped with two sets ofly, hand hoist (5) are controlled through manual cable (7), crossbeam hoist cable (6) and truss crossbeam (4) top fixed connection.
3. The rotary wing drone test mechanism of claim 1, wherein: the upper rope guide pulleys (8) are provided with three groups, one group is arranged in the middle of the lower part of the travelling frame cross beam (4), and the lower rope guide pulleys (11) are arranged on the ground right below the middle part of the travelling frame cross beam (4).
4. The rotary wing drone test mechanism of claim 1, wherein: the other ends of the upper rope (9) and the lower rope (12) respectively penetrate through the upper rope guide pulley (8) and the lower rope guide pulley (11) and are fixed on the rope fixing pile (14).
5. The rotary wing drone test mechanism of claim 1, wherein: go up tensiometer (10) below and pull down tensiometer (13) top and be equipped with connection cable (16) of connecting unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922240105.5U CN212333007U (en) | 2019-12-14 | 2019-12-14 | Rotor unmanned aerial vehicle accredited testing organization |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922240105.5U CN212333007U (en) | 2019-12-14 | 2019-12-14 | Rotor unmanned aerial vehicle accredited testing organization |
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| Publication Number | Publication Date |
|---|---|
| CN212333007U true CN212333007U (en) | 2021-01-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201922240105.5U Active CN212333007U (en) | 2019-12-14 | 2019-12-14 | Rotor unmanned aerial vehicle accredited testing organization |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113311806A (en) * | 2021-05-26 | 2021-08-27 | 南京航天国器智能装备有限公司 | Unmanned aerial vehicle intelligent test protection system |
-
2019
- 2019-12-14 CN CN201922240105.5U patent/CN212333007U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113311806A (en) * | 2021-05-26 | 2021-08-27 | 南京航天国器智能装备有限公司 | Unmanned aerial vehicle intelligent test protection system |
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