CN204710925U - One draws lead aircraft outer cover - Google Patents
One draws lead aircraft outer cover Download PDFInfo
- Publication number
- CN204710925U CN204710925U CN201520373639.4U CN201520373639U CN204710925U CN 204710925 U CN204710925 U CN 204710925U CN 201520373639 U CN201520373639 U CN 201520373639U CN 204710925 U CN204710925 U CN 204710925U
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- China
- Prior art keywords
- housing
- lead aircraft
- outer cover
- maintenance window
- side wall
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- 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.)
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Abstract
The utility model discloses one and draw lead aircraft outer cover, belong to Machining Technology field.Described outer cover mainly comprises base, housing and observation maintenance window; Wherein, base is provided with oil storage tank; The upper surface of housing is provided with warning lamp; The front side wall of housing is processed with and observes maintenance window installing port, and be provided with gas source interface and control panel; The left side wall of housing is provided with heat dissipating grid, charging aperture and discharging opening; The right side wall of housing is processed with and observes maintenance window installing port, and be provided with power interface and scram button; The observation maintenance window frame of window and the part of body contact are provided with sealing strip; Observe maintenance window and housing hinge; Open end and the base of housing are connected; Warning lamp is connected by controlling cable with control panel; Scram button is connected with the main circuit that machine gun cartridge case draws lead aircraft by controlling cable.The open lead aircraft that draws can be closed by described outer cover, effectively reduces the noise drawing lead aircraft.
Description
Technical field
The utility model relates to one and draws lead aircraft outer cover, belongs to Machining Technology field.
Background technology
Drawing lead aircraft is vertical equipment, and what be mainly used in various small bore cartridge shell case draws long stretch process.Because traditional lead aircraft that draws is open equipment, the noise in use produced is comparatively large, and easily causes the security incident of operating personnel; The each functional switch drawn in addition on lead aircraft is dispersed placement, make operation comparatively loaded down with trivial details, not easily it is controlled, cause that error is large, efficiency is low.
Utility model content
In view of this, the purpose of this utility model is to provide one and draws lead aircraft outer cover, and described outer cover can reduce the noise drawing lead aircraft, reduces measure error, the service efficiency of drawing lead aircraft is improved greatly.
The purpose of this utility model is realized by following technical scheme:
One draws lead aircraft outer cover, and described outer cover mainly comprises base, housing and observation maintenance window;
Wherein, described base is provided with oil storage tank, and the cell wall of oil storage tank is provided with circulating pump; Described housing is the rectangular configuration that bottom opens, and the upper surface of housing is provided with warning lamp; The front side wall of housing is processed with and observes maintenance window installing port, and be provided with gas source interface and control panel; The left side wall of housing is provided with heat dissipating grid, charging aperture and discharging opening, described heat dissipating grid is arranged on the position corresponding with the motor drawing lead aircraft; The right side wall of housing is processed with and observes maintenance window installing port, and be provided with power interface and scram button;
Described observation maintenance window comprises window frame and glass; And be provided with sealing strip at the observation maintenance window frame of window and the part of body contact;
Described observation maintenance window is movably connected in be observed on maintenance window installing port; Open end and the base of described housing are connected; The grease-box that described circulating pump draws lead aircraft with machine gun cartridge case is connected; Described warning lamp is connected by controlling cable with control panel; Described scram button is connected with the main circuit that machine gun cartridge case draws lead aircraft by controlling cable.
Further, the profile of described outer cover is with to draw lead aircraft corresponding.
Further, the material of described housing is acoustic damping materials, as sound panel.
Further, the drift angle of described housing is arc transition.
Further, described glass is double layer glass.
The course of work:
Before work, to draw lead aircraft is installed on base, by case cover to draw on lead aircraft and with the recess-mounted of base, and each functional switch drawn on lead aircraft is connected on the control panel on described outer cover by controlling cable, scram button is connected with the main circuit that machine gun cartridge case draws lead aircraft by controlling cable.In the course of work, staff is controlled drawing lead aircraft by the button on control panel, and when there is dangerous or violation operation, the warning lamp of described housing upper surface starts flicker, and staff can press scram button, and equipment is quit work; In addition, staff also detects by observing the service condition of maintenance window to equipment.
Beneficial effect
(1) the open lead aircraft that draws can be closed by the utility model by described outer cover, effectively reduces the noise drawing lead aircraft; And by control panel, each functional switch is carried out integrating control, can effectively reduce measure error, the service efficiency of drawing lead aircraft is improved greatly.
(2) the utility model is by the profile of described outer cover with to draw lead aircraft corresponding, facilitates the operation of staff.
(3) material of described housing case is acoustic damping materials by the utility model, and described material of observing maintenance window is double layer glass, can effectively reduce the noise produced when drawing lead aircraft work.
(4) drift angle of described housing case is arc transition by the utility model, when lead aircraft is drawn in operated by personnel's use, can prevent wedge angle from scratching, improve the safety in utilization of equipment.
Accompanying drawing explanation
Fig. 1 is the front view drawing lead aircraft outer cover described in the utility model;
Fig. 2 is the left view drawing lead aircraft outer cover described in the utility model.
Wherein, 1-base; 2-gas source interface; 3-warning lamp; 4-control panel; 5-observes maintenance window; 6-heat dissipating grid; 7-charging aperture; 8-discharging opening.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments in detail the utility model is described in detail, but is not limited thereto.
Embodiment
One draws lead aircraft outer cover, and as illustrated in fig. 1 and 2, it mainly comprises base 1, housing and observation maintenance window 5 to the structural representation of described outer cover;
Wherein, described base 1 is provided with oil storage tank, and the cell wall of oil storage tank is provided with circulating pump; Described housing is the rectangular configuration that bottom opens, and the upper surface of housing is provided with warning lamp 3; The front side wall of housing is processed with and observes maintenance window installing port, and be provided with gas source interface 2 and control panel 4; The left side wall of housing is provided with heat dissipating grid 6, charging aperture 7 and discharging opening 8, described heat dissipating grid is arranged on the position corresponding with the motor drawing lead aircraft; The right side wall of housing is processed with and observes maintenance window installing port, and be provided with power interface and scram button;
Described observation maintenance window 5 comprises window frame and glass; And be provided with sealing strip at the observation maintenance window frame of window 5 and the part of body contact;
Described observation maintenance window 5 is movably connected in be observed on maintenance window installing port; Open end and the base 1 of described housing are connected; The grease-box that described circulating pump draws lead aircraft with machine gun cartridge case is connected; Described warning lamp 3 is connected by controlling cable with control panel 4; Described scram button is connected with the main circuit that machine gun cartridge case draws lead aircraft by controlling cable.
The profile of described outer cover is with to draw lead aircraft corresponding.
The material of described housing is acoustic damping materials sound panel.
The drift angle of described housing is arc transition.
Described material of observing maintenance window 5 is double layer glass.
The course of work:
Before work, to draw lead aircraft is installed on base 1, by case cover to draw on lead aircraft and with the recess-mounted of base 1, and each functional switch drawn on lead aircraft is connected on the control panel 4 on described outer cover by controlling cable, scram button is connected with the main circuit that machine gun cartridge case draws lead aircraft by controlling cable.In the course of work, staff is controlled drawing lead aircraft by the button on control panel 4, and when there is dangerous or violation operation, the warning lamp 3 of described housing upper surface starts flicker, and staff can press scram button, and equipment is quit work; In addition, the service condition of staff also by observing maintenance window 5 pairs of equipment detects.
The utility model includes but not limited to above embodiment, and every any equivalent replacement of carrying out under the principle of the utility model spirit or local improvement, all will be considered as within protection domain of the present utility model.
Claims (6)
1. draw a lead aircraft outer cover, it is characterized in that: described outer cover mainly comprises base (1), housing and observation maintenance window (5);
Wherein, (1) is provided with oil storage tank to described base, and the cell wall of oil storage tank is provided with circulating pump; Described housing is the rectangular configuration that bottom opens, and the upper surface of housing is provided with warning lamp (3); The front side wall of housing is processed with and observes maintenance window installing port, and be provided with gas source interface (2) and control panel (4); The left side wall of housing is provided with heat dissipating grid (6), charging aperture (7) and discharging opening (8), described heat dissipating grid is arranged on the position corresponding with the motor drawing lead aircraft; The right side wall of housing is processed with and observes maintenance window installing port, and be provided with power interface and scram button (9);
Described observation maintenance window (5) comprises window frame and glass; And be provided with sealing strip in the part of the window frame and body contact of observing maintenance window (5);
Described observation maintenance window (5) is movably connected in observes on maintenance window installing port; The open end of described housing and base (1) are connected; The grease-box that described circulating pump draws lead aircraft with machine gun cartridge case is connected; Described warning lamp (3) is connected by controlling cable with control panel (4); Described scram button (9) is connected with the main circuit that machine gun cartridge case draws lead aircraft by controlling cable.
2. one according to claim 1 draws lead aircraft outer cover, it is characterized in that: the profile of described outer cover is with to draw lead aircraft corresponding.
3. one according to claim 1 draws lead aircraft outer cover, it is characterized in that: the material of described housing is acoustic damping materials.
4. one according to claim 3 draws lead aircraft outer cover, it is characterized in that: described acoustic damping materials are sound panel.
5. one according to claim 1 draws lead aircraft outer cover, it is characterized in that: the drift angle of described housing is arc transition.
6. one according to claim 1 draws lead aircraft outer cover, it is characterized in that: described glass is double layer glass.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520373639.4U CN204710925U (en) | 2015-06-03 | 2015-06-03 | One draws lead aircraft outer cover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520373639.4U CN204710925U (en) | 2015-06-03 | 2015-06-03 | One draws lead aircraft outer cover |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204710925U true CN204710925U (en) | 2015-10-21 |
Family
ID=54309955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520373639.4U Active CN204710925U (en) | 2015-06-03 | 2015-06-03 | One draws lead aircraft outer cover |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204710925U (en) |
-
2015
- 2015-06-03 CN CN201520373639.4U patent/CN204710925U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |