CN217955329U - Be used for teaching aviation electric pump dismouting device - Google Patents
Be used for teaching aviation electric pump dismouting device Download PDFInfo
- Publication number
- CN217955329U CN217955329U CN202123419248.6U CN202123419248U CN217955329U CN 217955329 U CN217955329 U CN 217955329U CN 202123419248 U CN202123419248 U CN 202123419248U CN 217955329 U CN217955329 U CN 217955329U
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- oil tank
- simulation oil
- electric pump
- desktop frame
- panel
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Abstract
The utility model provides a be used for teaching aviation electric pump dismouting device which characterized in that: including support (5), can overturn spacing desktop frame (8) of damage in support (5), fix panel (4) on desktop frame (8), install simulation oil tank (2) on panel (4), simulation oil tank cap (1) of setting on simulation oil tank (2), electric pump (6) of setting in simulation oil tank cap (1), set up drain valve (3) with simulation oil tank (2) intercommunication on panel (4), desktop frame (8) both sides of linking department with support (5) are equipped with round pin axle (7) that are located the center and are located the location double-screw bolt (9) in the center outside, desktop frame (8) and location double-screw bolt (9) are locked through round pin axle nut (10) respectively. It has the advantages of simple and compact structure, convenient and fast use and the like.
Description
Technical Field
The utility model relates to a teaching presentation device, a be used for teaching aviation electric pump dismouting device specifically says so, it mainly is applicable to aviation electric pump dismouting teaching.
Background
The present dismounting platform, such as the 'generator dismounting platform' disclosed in the invention patent application with application publication number CN103495854a, adopts the following technical scheme that an ultrahigh pressure hydraulic device provides power to a first hydraulic cylinder and a second hydraulic cylinder in a flange fixing device, the flange fixing device comprises a first hydraulic cylinder, a second hydraulic cylinder and a first dismounting plate, the first hydraulic cylinder enables the flange fixing device to move in the vertical direction through the extension and retraction of a hydraulic rod of the first hydraulic cylinder, the hydraulic rod of the second hydraulic cylinder penetrates through a Kong Dingzhu generator rotor shaft on the first dismounting plate, the first dismounting plate and a generator flange are connected together through a third screw rod to dismount the generator flange, a generator supporting device supports a generator, and the generator can freely move in a plane parallel to the ground, and the ultrahigh pressure hydraulic device, the flange fixing device and the generator supporting device are all fixed on the base. The structure is complex, and is not beneficial to the field teaching of the disassembly and assembly of the aviation electric pump.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an aviation electric pump dismouting teaching device, the position that simulation aviation electric pump is located on the aircraft is installed the aviation electric pump, carries out aviation electric pump dismouting teaching to the student, reaches the teaching purpose, and it has advantages such as simple structure is understandable, area is little, convenient to use.
In order to realize the purpose, the aviation electric pump dismounting device adopts the following technical scheme: this aviation electric pump dismouting device, its technical essential is: including the support, can overturn spacing desktop frame at the support damage, fix the panel on the desktop frame, install the simulation oil tank on the panel, the simulation oil tank cap of setting on the simulation oil tank, the electric pump of setting in the simulation oil tank cap, the fuel outlet valve with simulation oil tank intercommunication of setting on the panel, desktop frame both sides of linking department with the support are equipped with the round pin axle that is located the center and are located the positioning stud in the center outside, desktop frame and positioning stud are respectively through round pin axle nut locking.
The utility model discloses beneficial effect: through frame construction, make the student can come to simulation oil tank below and carry out the dismouting exercise of aviation electric pump, reach the purpose that simulation aviation electric pump was practiced in the dismouting of aircraft actual position. Thereby providing convenience for aviation electric pump dismounting teaching. The turnover desktop structure is arranged on the support, so that the application range is effectively enlarged, and the unfolding of teaching courses is facilitated.
Drawings
Fig. 1 is an isometric side view schematic structure of the present invention.
Fig. 2 is a schematic sectional structure diagram of the present invention.
Detailed Description
The present invention will be described in detail with reference to fig. 1~2 by way of specific embodiments. This be used for teaching aviation electric pump dismouting device includes support 5, can overturn spacing desktop frame 8 at 5 damages of support, fix panel 4 on desktop frame 8, install simulation oil tank 2 on panel 4, the simulation oil tank cap 1 of setting on simulation oil tank 2, the electric pump 6 of setting in simulation oil tank cap 1, set up on panel 4 and the fuel outlet valve 3 of simulation oil tank 2 intercommunication, the desktop frame 8 both sides of linking department with support 5 are equipped with the round pin axle 7 that is located the center and are located the locating stud 9 in the center outside, desktop frame 8 and locating stud 9 are locked through round pin axle nut 10 respectively.
The aviation electric pump dismounting device is adjusted to the state shown in figure 2, and then the aviation electric pump dismounting teaching can be carried out.
Erect the take the altitude with simulation oil tank 2, make the student can come to 2 below simulation oil tanks and carry out the dismouting exercise of aviation electric pump 6, simulate aviation electric pump 6 and operate at the aircraft actual position. The simulation oil tank 2 can be rotated to the lower part by turning over the desktop frame 8 and the panel 4, so that the simulation oil tank 2 is convenient to install and overhaul. After 6 installations of aviation electric pump finish, can refuel 2 insides of simulation oil tank through simulation oil tank cap 1, carry out the oil drain operation through fuel outlet valve 3. The simulation oil tank 2 is made of transparent acrylic materials, so that the situation that the aviation electric pump 6 is installed inside the oil tank can be observed.
Description of the reference numerals: the oil tank comprises a simulated oil tank cover 1, a simulated oil tank 2, an oil drain valve 3, a panel 4, a bracket 5, an electric pump 6, a pin shaft 7, a desktop frame 8, a positioning stud 9 and a pin shaft nut 10.
Claims (1)
1. The utility model provides a be used for teaching aviation electric pump dismouting device which characterized in that: including support (5), can overturn spacing desktop frame (8) of damage in support (5), fix panel (4) on desktop frame (8), install simulation oil tank (2) on panel (4), simulation oil tank cap (1) of setting on simulation oil tank (2), electric pump (6) of setting in simulation oil tank cap (1), set up drain valve (3) with simulation oil tank (2) intercommunication on panel (4), desktop frame (8) both sides of linking department with support (5) are equipped with round pin axle (7) that are located the center and are located the location double-screw bolt (9) in the center outside, desktop frame (8) and location double-screw bolt (9) are locked through round pin axle nut (10) respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123419248.6U CN217955329U (en) | 2021-12-31 | 2021-12-31 | Be used for teaching aviation electric pump dismouting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123419248.6U CN217955329U (en) | 2021-12-31 | 2021-12-31 | Be used for teaching aviation electric pump dismouting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217955329U true CN217955329U (en) | 2022-12-02 |
Family
ID=84209023
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123419248.6U Active CN217955329U (en) | 2021-12-31 | 2021-12-31 | Be used for teaching aviation electric pump dismouting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217955329U (en) |
-
2021
- 2021-12-31 CN CN202123419248.6U patent/CN217955329U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |