CN205040409U - Novel manger - Google Patents

Novel manger Download PDF

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Publication number
CN205040409U
CN205040409U CN201520824579.3U CN201520824579U CN205040409U CN 205040409 U CN205040409 U CN 205040409U CN 201520824579 U CN201520824579 U CN 201520824579U CN 205040409 U CN205040409 U CN 205040409U
Authority
CN
China
Prior art keywords
fuselage
division board
connecting rod
handle
control device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201520824579.3U
Other languages
Chinese (zh)
Inventor
祝大进
薛家行
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JIAXING DAMING INDUSTRIAL Co Ltd
Original Assignee
JIAXING DAMING INDUSTRIAL Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JIAXING DAMING INDUSTRIAL Co Ltd filed Critical JIAXING DAMING INDUSTRIAL Co Ltd
Priority to CN201520824579.3U priority Critical patent/CN205040409U/en
Application granted granted Critical
Publication of CN205040409U publication Critical patent/CN205040409U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model discloses a novel manger, including fuselage (1), defeated silo (2), trough (9) and separation frame (16) of setting in fuselage (1), separation frame (16) will fail silo (2) and keep apart with trough (9), be provided with accuse material device in defeated silo (2), accuse material device includes handle (12), stay tube (10), connecting rod (3), division board (7) and baffle (5), division board (7) adopt elastic material to make, baffle (5) are connected with division board (7), handle (12) are connected with connecting rod (3), handle (12) but the lift of control connection pole (3), the mutual symmetry in the left and right sides of fuselage (1), be provided with trough (9) of controlling two mutual symmetries in fuselage (1). The utility model discloses compact structure, the practicality is good, can freely control unloading speed.

Description

A kind of novel fodder groove
Technical field
The utility model relates to livestock breeding field, is specifically related to a kind of novel fodder groove.
Background technology
Livestock breeding, as the Two Mainstays of agricultural production, for expanding economy provides powerful backing, emphasis as in livestock breeding: pig industry, pig industry is the important industry in China's agricultural, no matter be large-scale farming or cultivation on a small scale, all very common, pig industry is supplied with important function to ensuring food safety, in former pig industry, cultivate lack of standardization, for trough, be generally one side trough, waste for material is comparatively serious, time on the feed simultaneously, hog snout constantly contacts division board, if division board is really up to the mark, can cause damage to hog snout, if division board is excessively soft, then can be bent, ineffective.
Therefore; in order to ensure the quality of pork; protection cultivation pig preserves from; China's pig industry needs to be changed to Pig Industry industry by traditional pig industry; be aquaculture model, Regional Distribution or the mode of production, production capacity all needs to change; trough also needs to increase operation rate, and reduces production cost, reduces the damage of cultivation pig.
Utility model content
The utility model provides a kind of novel fodder groove, and availability is high, and practicality is good, and in order to solve technique scheme, the utility model adopts following technical scheme:
A kind of novel fodder groove, the isolating frame comprising fuselage, feeding groove, crib and be arranged in fuselage, described fuselage upper end is provided with opening, feeding groove and crib are isolated by described isolating frame, are provided with material control device in described delivery chute, and described material control device comprises handle, stay pipe, connecting rod, division board and baffle plate, described division board adopts elastomeric material to make, described baffle plate is connected with division board, and described handle is connected with connecting rod, and described handle can control the lifting of connecting rod; The left and right sides of described fuselage is symmetrical, is provided with the crib that two, left and right is symmetrical in described fuselage.
The utility model provides a kind of novel fodder groove, and preferably, described material control device has two, and described material control device one end is fixing on the supporting plate, and described gripper shoe is arranged on the opening part of fuselage.
The utility model provides a kind of novel fodder groove, preferably, described handle is provided with flap, be connected with sleeve pipe below described flap, described sleeve pipe is arranged on the supporting plate, is connected with stay pipe below described sleeve pipe, be provided with connecting rod in described stay pipe, described connecting rod is connected with handle.
The utility model provides a kind of novel fodder groove, and preferably, described connecting rod afterbody is provided with fixed block, described fixed block lower end is provided with division board, described division board laminating isolating frame is arranged, and described division board adopts spring steel plate to make, and the back side of described division board is provided with baffle plate.
The utility model provides a kind of novel fodder groove, and preferably, the bottom of described fuselage is provided with triangular hill, and described triangular hill is corresponding with delivery chute.
Advantage of the present utility model and beneficial effect are: the novel fodder groove that the utility model provides, and compact conformation is provided with two cribs in a fuselage, and two cribs share a feeding groove, improve availability;
Utilize material control device, can adjust the distance of division board and fuselage bottom, regulate the discharging speed of feed with this, this material control device is controlled by handle, only needs turning handle and Adjustable Range, convenient, efficiently;
Utilize the baffle plate at the division board back side simultaneously, division board can be prevented to be bent, increase the service life.
Accompanying drawing explanation
Carry out describing in detail or preferably to preferred embodiment of the present utility model below in conjunction with accompanying drawing, wherein,
Fig. 1 is the overall schematic of a kind of novel fodder groove of the utility model;
Fig. 2 is the schematic cross-section of a kind of novel fodder groove of the utility model.
Embodiment
With reference to accompanying drawing 1-2, the utility model provides a kind of novel fodder groove, comprise fuselage 1, feeding groove 2, crib 9 and the isolating frame 16 be arranged in fuselage 1, described fuselage 1 upper end is provided with opening, feeding groove 2 and crib 9 are isolated by described isolating frame 16, it is characterized in that, material control device is provided with in described feeding groove 2, described material control device comprises handle 12, stay pipe 10, connecting rod 3, division board 7 and baffle plate 5, described division board 7 adopts elastomeric material to make, described baffle plate 5 is connected with division board 7, described handle 12 is connected with connecting rod 3, described handle 12 can control the lifting of connecting rod 3, the left and right sides of described fuselage 1 is symmetrical, is provided with the crib 9 that two, left and right is symmetrical in described fuselage 1.
Meanwhile, described material control device has two, and described material control device one end is fixed in gripper shoe 13, and described gripper shoe 13 is arranged on the opening part of fuselage 1.
Described handle 12 is provided with flap 14, be connected with sleeve pipe 15 below described flap 14, described sleeve pipe 15 is arranged in gripper shoe 14, is connected with stay pipe 10 below described sleeve pipe 15, be provided with connecting rod 3 in described stay pipe 10, described connecting rod 3 is connected with handle 12.
Further, described connecting rod 3 afterbody is provided with fixed block 4, and described fixed block 4 lower end is provided with division board 7, and described division board 7 isolating frame 16 of fitting is arranged, and described division board 7 adopts spring steel plate to make, and the back side of described division board 7 is provided with baffle plate 5.
The bottom of fuselage 1 is provided with triangular hill, and described triangular hill is corresponding with feeding groove 2, to slow down the pressure of blanking.
Above-described is only preferred embodiment of the present utility model.It should be pointed out that for the person of ordinary skill of the art, under the prerequisite not departing from the utility model principle, can also make some distortion and improvement, these also should be considered as belonging to protection domain of the present utility model.

Claims (5)

1. a novel fodder groove, comprise fuselage (1), feeding groove (2), crib (9) and the isolating frame (16) be arranged in fuselage (1), described fuselage (1) upper end is provided with opening, feeding groove (2) and crib (9) are isolated by described isolating frame (16), it is characterized in that, described feeding groove is provided with material control device in (2), described material control device comprises handle (12), stay pipe (10), connecting rod (3), division board (7) and baffle plate (5), described division board (7) adopts elastomeric material to make, described baffle plate (5) is connected with division board (7), described handle (12) is connected with connecting rod (3), described handle (12) can control the lifting of connecting rod (3), the left and right sides of described fuselage (1) is symmetrical, is provided with the crib (9) that two, left and right is symmetrical in described fuselage (1).
2. a kind of novel fodder groove according to claim 1, it is characterized in that, described material control device has two, and described material control device one end is fixed in gripper shoe (13), and described gripper shoe (13) is arranged on the opening part of fuselage (1).
3. a kind of novel fodder groove according to claim 1, it is characterized in that, described handle (12) is provided with flap (14), described flap (14) below is connected with sleeve pipe (15), described sleeve pipe (15) is arranged in gripper shoe (13), described sleeve pipe (15) below is connected with stay pipe (10), and be provided with connecting rod (3) in described stay pipe (10), described connecting rod (3) is connected with handle (12).
4. a kind of novel fodder groove according to claim 1 or 3, it is characterized in that, described connecting rod (3) afterbody is provided with fixed block (4), described fixed block (4) lower end is provided with division board (7), described division board (7) laminating isolating frame (16) is arranged, described division board (7) adopts spring steel plate to make, and the back side of described division board (7) is provided with baffle plate (5).
5. a kind of novel fodder groove according to claim 1, it is characterized in that, the bottom of described fuselage (1) is provided with triangular hill, and described triangular hill is corresponding with feeding groove (2).
CN201520824579.3U 2015-10-21 2015-10-21 Novel manger Expired - Fee Related CN205040409U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520824579.3U CN205040409U (en) 2015-10-21 2015-10-21 Novel manger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520824579.3U CN205040409U (en) 2015-10-21 2015-10-21 Novel manger

Publications (1)

Publication Number Publication Date
CN205040409U true CN205040409U (en) 2016-02-24

Family

ID=55334042

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520824579.3U Expired - Fee Related CN205040409U (en) 2015-10-21 2015-10-21 Novel manger

Country Status (1)

Country Link
CN (1) CN205040409U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117243147A (en) * 2023-11-13 2023-12-19 诸城市大牧源机械有限公司 Fecal emission reduction three-dimensional egg and duck cage

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117243147A (en) * 2023-11-13 2023-12-19 诸城市大牧源机械有限公司 Fecal emission reduction three-dimensional egg and duck cage

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CB03 Change of inventor or designer information

Inventor after: Zhu Dajin

Inventor after: Xue Jiaqi

Inventor before: Zhu Dajin

Inventor before: Xue Jiaxing

COR Change of bibliographic data
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160224

Termination date: 20171021

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