CN203461122U - Chemical liquid shaking prevention structure of chemical tank of four-shaft agricultural aircraft - Google Patents

Chemical liquid shaking prevention structure of chemical tank of four-shaft agricultural aircraft Download PDF

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Publication number
CN203461122U
CN203461122U CN201320520173.7U CN201320520173U CN203461122U CN 203461122 U CN203461122 U CN 203461122U CN 201320520173 U CN201320520173 U CN 201320520173U CN 203461122 U CN203461122 U CN 203461122U
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CN
China
Prior art keywords
liquid
chest
casing
agricultural aircraft
chemical
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Expired - Fee Related
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CN201320520173.7U
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Chinese (zh)
Inventor
戴相超
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CHONGQING JINTAI AVIATION INDUSTRIAL Co Ltd
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CHONGQING JINTAI AVIATION INDUSTRIAL Co Ltd
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Priority to CN201320520173.7U priority Critical patent/CN203461122U/en
Application granted granted Critical
Publication of CN203461122U publication Critical patent/CN203461122U/en
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Abstract

The utility model discloses a chemical liquid shaking prevention structure of a chemical tank of a four-shaft agricultural aircraft. The chemical liquid shaking prevention structure comprises a tank body (1), wherein the tank body (1) is of a hemispheric hollow structure of which the small end faces downward; the upper part of the peripheral side wall of the tank body (1) is provided with a round chemical charging port; the chemical charging port is sealed with a seal cap (2); two crisscross clapboards (3) are fixedly arranged on the lower part of the internal cavity of the tank body (1); the crisscross clapboards (3) divide the lower part of the internal cavity of the tank body (1) into four cavities; each two adjacent cavities are communicated by through holes (4) formed in the bottoms of the clapboards (3). The chemical liquid shaking prevention structure is not only simple and attractive in shape and easy to manufacture, but also lower in weight, small in size and good in structural strength, can effectively prevent chemical liquid from shaking, and is applicable for various types of agricultural aircrafts.

Description

The anti-liquid of the agricultural aircraft medicine-chest of four axles rocks structure
Technical field
The utility model belongs to agricultural vehicle technology field, and specifically, particularly the anti-liquid of the agricultural carry-on medicine-chest of four axles rocks structure.
Background technology
Along with social development, the progress of science and technology, the work such as spray insecticide on a large scale in farmland, fertilising are progressively completed by unmanned vehicle.Existing agricultural unmanned vehicle complex structure, bulky, weight is heavier, seriously restricted it and applied on a large scale.Take medicine-chest as example, and medicine-chest is agricultural carry-on vitals, is mainly used in splendid attire liquid.But existing medicine-chest moulding is complicated, processing and fabricating difficulty, productive costs is higher, and Heavy Weight, volume are large, can increase the height of whole aircraft.In addition, when liquid in medicine-chest is less, be subject to the impact of aircraft operational vibration, liquid can agitate and rock, thereby affects the balance of aircraft, reduces the effect of spray liquid.
Utility model content
Technical problem to be solved in the utility model be to provide a kind of processing and fabricating easily, can effectively prevent the agricultural aircraft medicine-chest of four axles that liquid rocks.
The technical solution of the utility model is as follows: the anti-liquid of the agricultural aircraft medicine-chest of a kind of four axle rocks structure, there is casing (1), its key is: described casing (1) is small end semisphere hollow structure down, top at all sidewalls of casing (1) is provided with circular dosing mouth, this dosing mouth is sealed by capping (2), in the bottom of described casing (1) inner chamber, be fixedly installed the dividing plate (3) of two right-angled crossings, these two dividing plates (3) are separated into four chambers by the bottom of casing (1) inner chamber, the through hole (4) of offering by dividing plate (3) bottom between two adjacent chamber is communicated with.
The utility model is semisphere by cabinet design, and not only simply but also attractive in appearance, and processing and fabricating is easy in moulding.Dosing mouth for adding injecting medical liquid in casing, and dosing mouth is sealed by capping, and good airproof performance can prevent that liquid from spattering or revealing outward.The bottom of cabinets cavity is become four chambers of uniform size by baffle for separating, and be interconnected between chamber, can not affect normally pumping of liquid so on the one hand, on the other hand, when liquid is less by uniform distribution in each chamber, not affected by FLIGHT VEHICLE VIBRATION and produce to rock, thereby guarantee the balance of aircraft, effectively improve the effect of spray liquid.
Described casing (1) is made by glass-felt plastic, is easy to like this moulding, and production efficiency is high, can effectively reduce the cost of batch manufacturing, and the structural strength of casing is good simultaneously, is difficult for deforming or damaging; The thickness of casing is 1mm, can when guaranteeing structural strength, save as far as possible material, reduce costs.
In order to beautify outward appearance, and strengthen resistance to abrasion and the anti-corrosive properties of casing, at the outside face of described casing (1), be coated with epoxy enamelled coating.
As preferably, the thickness of described epoxy enamelled coating is 0.05mm.
In order to make dismounting more convenient, quick, described capping (2) snapping or be threaded on dosing mouth.
Described dividing plate (3) is made by cellular composite material, and thickness is 3-5mm, and the intensity of dividing plate is reliable like this, can not deform or damage; Meanwhile, dividing plate lightweight, limited to the increase of medicine-chest weight.
As preferably, the thickness of described dividing plate (3) is 4mm.
Beneficial effect: the utility model not only moulding is simple, attractive in appearance, and processing and fabricating is easy, and weight is light, volume is small and exquisite, and structural strength is good, can effectively prevent that liquid from shaking, all applicable on various types of agricultural aircraft.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the birds-eye view of Fig. 1.
The specific embodiment
Below in conjunction with drawings and Examples, the utility model is described in further detail:
As shown in Figure 1 and Figure 2, the medicine-chest of the agricultural aircraft of four axles has casing 1, and this casing 1 is small end semisphere hollow structure down.Described casing 1 is made by glass-felt plastic, and thickness is preferably 1mm.At the outside face of casing 1, be coated with the epoxy enamelled coating of attractive in appearance and wear-resisting effect, the thickness of epoxy enamelled coating is 0.05mm.The middle part of described casing 1 end face, to lower recess, forms deep gouge, and this deep gouge is rectangle, for Teat pipette is installed, to avoid Teat pipette to increase the height of aircraft.The degree of depth of described deep gouge is 60-75mm, and the present embodiment is preferably 70mm, between all tops of sidewall of deep gouge and the end face of casing 1, passes through arc transition.Top at 1 week sidewall of described casing is provided with a circular dosing mouth, and this dosing mouth is sealed by capping 2, described capping 2 snappings or be threaded on dosing mouth.
As shown in Figure 1 and Figure 2, be provided with the dividing plate 3 of two right-angled crossings in the bottom of described casing 1 inner chamber, this dividing plate 3 is made by cellular composite material, and thickness is 3-5mm, and the present embodiment is preferably 4mm, and the inwall of the bottom of dividing plate 3 and casing 1 fits fixing.Two dividing plates 3 are separated into four chambers by the bottom of casing 1 inner chamber, and the through hole 4 of offering by dividing plate 3 bottoms between two adjacent chamber is communicated with.

Claims (7)

1. the anti-liquid of the agricultural aircraft medicine-chest of axle rocks structure, there is casing (1), it is characterized in that: described casing (1) is small end semisphere hollow structure down, top at all sidewalls of casing (1) is provided with circular dosing mouth, this dosing mouth is sealed by capping (2), in the bottom of described casing (1) inner chamber, be fixedly installed the dividing plate (3) of two right-angled crossings, these two dividing plates (3) are separated into four chambers by the bottom of casing (1) inner chamber, and the through hole (4) of offering by dividing plate (3) bottom between two adjacent chamber is communicated with.
2. the anti-liquid of the agricultural aircraft medicine-chest of four axle according to claim 1 rocks structure, it is characterized in that: described casing (1) is made by glass-felt plastic, and thickness is 1mm.
3. the anti-liquid of the agricultural aircraft medicine-chest of four axle according to claim 1 and 2 rocks structure, it is characterized in that: the outside face at described casing (1) is coated with epoxy enamelled coating.
4. the anti-liquid of the agricultural aircraft medicine-chest of four axle according to claim 3 rocks structure, it is characterized in that: the thickness of described epoxy enamelled coating is 0.05mm.
5. the anti-liquid of the agricultural aircraft medicine-chest of four axle according to claim 1 rocks structure, it is characterized in that: described capping (2) snapping or be threaded on dosing mouth.
6. the anti-liquid of the agricultural aircraft medicine-chest of four axle according to claim 1 rocks structure, it is characterized in that: described dividing plate (3) is made by cellular composite material, and thickness is 3-5mm.
7. the anti-liquid of the agricultural aircraft medicine-chest of four axle according to claim 6 rocks structure, it is characterized in that: the thickness of described dividing plate (3) is 4mm.
CN201320520173.7U 2013-08-23 2013-08-23 Chemical liquid shaking prevention structure of chemical tank of four-shaft agricultural aircraft Expired - Fee Related CN203461122U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320520173.7U CN203461122U (en) 2013-08-23 2013-08-23 Chemical liquid shaking prevention structure of chemical tank of four-shaft agricultural aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320520173.7U CN203461122U (en) 2013-08-23 2013-08-23 Chemical liquid shaking prevention structure of chemical tank of four-shaft agricultural aircraft

Publications (1)

Publication Number Publication Date
CN203461122U true CN203461122U (en) 2014-03-05

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CN201320520173.7U Expired - Fee Related CN203461122U (en) 2013-08-23 2013-08-23 Chemical liquid shaking prevention structure of chemical tank of four-shaft agricultural aircraft

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104285933A (en) * 2014-09-16 2015-01-21 河北雷肯农业机械有限公司 Small-volume drug pot assembled on agricultural unmanned drug spraying machine
WO2016070684A1 (en) * 2014-11-03 2016-05-12 深圳高科新农技术有限公司 U-shaped kit for unmanned farm helicopters
WO2018019150A1 (en) * 2016-07-27 2018-02-01 深圳亿天航科技有限公司 Chemical-tank anti-vibration mechanism and crop-protection unmanned aerial vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104285933A (en) * 2014-09-16 2015-01-21 河北雷肯农业机械有限公司 Small-volume drug pot assembled on agricultural unmanned drug spraying machine
WO2016070684A1 (en) * 2014-11-03 2016-05-12 深圳高科新农技术有限公司 U-shaped kit for unmanned farm helicopters
WO2018019150A1 (en) * 2016-07-27 2018-02-01 深圳亿天航科技有限公司 Chemical-tank anti-vibration mechanism and crop-protection unmanned aerial vehicle

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140305

Termination date: 20170823

CF01 Termination of patent right due to non-payment of annual fee