CN215868237U - Aviation cabin cover dismouting trainer - Google Patents
Aviation cabin cover dismouting trainer Download PDFInfo
- Publication number
- CN215868237U CN215868237U CN202121941650.8U CN202121941650U CN215868237U CN 215868237 U CN215868237 U CN 215868237U CN 202121941650 U CN202121941650 U CN 202121941650U CN 215868237 U CN215868237 U CN 215868237U
- Authority
- CN
- China
- Prior art keywords
- skin
- flip
- covering section
- fixed
- section
- 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.)
- Active
Links
Images
Landscapes
- Instructional Devices (AREA)
Abstract
Aviation cabin cover dismouting trainer, including the board base, board base side is equipped with the support lateral wall, support lateral wall and fixed covering section fixed connection, and fixed covering section inboard upper end rotates with the inboard lower extreme of flip covering section to be connected, realizes expandeing and folding through the rotation of flip covering section, and the appearance of fixed covering section and flip covering section is the arc for simulate real aircraft fuselage appearance, is equipped with multiple training cabin cover in the flip covering section, is used for carrying out the cabin cover dismouting training. Through rotating flip covering section and fixed covering section and being connected, when flip covering section overturns the top extremely spacing, the simulation section of fuselage is constituteed with fixed covering section to flip covering section, and training personnel can carry out the dismouting training of various hatches through the multiple training hatches of flip covering section, when need not train, puts down flip covering section and accomodates, reduces the space and occupies, and simple and practical is put in the repacking, can carry out the live action simulation to the dismouting of various hatches in the engineering work effectively.
Description
Technical Field
The utility model relates to the technical field of aviation aircraft work training, in particular to an aviation cabin cover dismounting training device.
Background
At present, the common training contents of basic maintenance skills of aviation crew mainly comprise training subjects such as tool use training, part disassembly and assembly training, fastening and safety training, binding and arrangement training, electric connector training, electric welding training, circuit measurement training, tightness inspection training, equipment use guarantee, part cleaning and lubrication, marking and the like. Different training subjects require different hardware facilities.
In the engineering management, a large amount of training equipment is often required to be configured for training the skills of each module so as to meet the training requirements of each specialty. However, in the existing aircraft cabin cover dismounting training, the cabin cover dismounting and mounting is simulated on a table, the cabin cover is often positioned in a machine body in real maintenance or operation and inspection, the actual dismounting and mounting is greatly different from the training on the ground table due to the structural characteristics of the machine body, the actual working environment cannot be simulated well, and the dismounting and mounting space cost and the equipment cost of a real machine on the ground are not allowed due to the fact that the machine body is too large, so that the cabin cover dismounting and mounting device capable of simulating the real machine is very difficult to obtain.
Disclosure of Invention
The technical problem to be solved by the utility model is to provide an aviation hatch cover dismounting and mounting training device, which can simulate the hatch cover arrangement characteristics of a real machine and does not occupy too much space due to the structural arrangement of the device.
In order to solve the technical problems, the technical scheme adopted by the utility model is as follows:
aviation cabin cover dismouting trainer, characterized by: including the board base, board base side is equipped with the support lateral wall, supports lateral wall and fixed covering section fixed connection, and the inboard upper end of fixed covering section rotates with the inboard lower extreme of flip covering section to be connected, and the appearance of fixed covering section and flip covering section is the arc for simulate real aircraft fuselage appearance, be equipped with multiple training hatch cover in the flip covering section, be used for carrying out the hatch cover dismouting training.
The training hatch cover comprises a quick-release screw hatch cover, a cross bayonet hatch cover and a screw hatch cover, and the three hatch covers are detachably connected with the flip cover skin section.
The support side wall is provided with a side wall plate on one side of the machine platform base, two ends of the side wall plate are provided with convex skin connecting frames, the skin connecting frames are fixedly connected with the outer sides of two ends of the fixed skin section, and the shape of the skin connecting frames is matched with that of the fixed skin section.
The inner sides of the fixed skin sections are provided with support columns arranged at intervals, and the support columns are fixedly connected through transverse connecting rods.
The flip cover skin section comprises a fuselage skin with an arc-shaped appearance, two ends of the fuselage skin are provided with convex skin side plates, the skin side plates are fixedly connected through supporting connecting plates, and the training hatch cover is positioned between the upper supporting connecting plate and the lower supporting connecting plate.
The upper end of the inner side of the fixed skin section is provided with a fixed skin connecting lug which is fixedly connected, the lower parts of the inner sides of the two ends of the flip skin section are provided with a flip skin connecting lug which is fixedly connected, and the end part of the fixed skin connecting lug is rotatably connected with the end part of the flip skin connecting lug.
According to the aviation cabin cover dismounting training device provided by the utility model, the flip cover skin section is rotatably connected with the fixed skin section, when the flip cover skin section is turned to the upper limit, the flip cover skin section and the fixed skin section form the simulation section of the aircraft body, a trainer can carry out dismounting training on various cabin covers through various training cabin covers of the flip cover skin section, when training is not needed, the flip cover skin section is put down and stored, the space occupation is reduced, the device is simple and practical to modify, and the device can effectively carry out live-scene simulation on dismounting of various cabin covers in the engineering work.
Drawings
The utility model is further illustrated by the following examples in conjunction with the accompanying drawings:
FIG. 1 is a first general structural diagram of the present invention;
FIG. 2 is an enlarged view of a portion of FIG. 1 at A;
FIG. 3 is a second overall view of the present invention;
FIG. 4 is a schematic view of the folded state of the flip cover skin segment of the present invention;
FIG. 5 is a block diagram of the base and supporting sidewalls of the machine;
FIG. 6 is a schematic structural view of a stationary skin segment;
FIG. 7 is a schematic structural view of a section of a cover skin of the flip;
FIG. 8 is a schematic structural view of a quick release screw deck lid;
FIG. 9 is a schematic view of the structure of the cross bayonet hatch;
fig. 10 is a structural schematic view of the screw hatch.
In the figure: the device comprises a machine base 1, a support column 2, a fixed skin section 3, a support side wall 4, a side wall plate 41, a skin connecting frame 42, a flip cover skin section 5, a fuselage skin 51, a skin side plate 52, a support connecting plate 53, a flip cover connecting lug 6, a fixed skin connecting lug 7, a training hatch cover 8, a quick-release screw hatch cover 81, a cross bayonet hatch cover 82 and a screw hatch cover 83.
Detailed Description
As shown in fig. 1-10, the aviation hatch cover dismounting training device is characterized in that: including board base 1, board base 1 side is equipped with support lateral wall 4, supports lateral wall 4 and fixed covering section 3 fixed connection, and fixed covering section 3 inboard upper end is rotated with the inboard lower extreme of flip covering section 5 and is connected, and fixed covering section 3 and flip covering section 5's appearance is the arc for simulation real aircraft fuselage appearance, be equipped with multiple training cabin cover 8 on the flip covering section 5, be used for carrying out the cabin cover dismouting training.
When a cabin cover dismounting test needs to be carried out, the flip cover skin section is turned upwards and unfolded, the fixed cover skin section 3 and the flip cover skin section 5 form the appearance simulation of the fuselage together, and training personnel dismount and mount the training cabin cover 8 on the flip cover skin section 5 to simulate the dismounting and mounting scene under the real aircraft environment.
The training hatch cover 8 comprises a quick-release screw hatch cover 81, a cross bayonet hatch cover 82 and a screw hatch cover 83, the three hatch covers are detachably connected with the flip cover skin section 5, and the connection condition of the hatch covers with different connection structures and the fuselage can be trained through different hatch covers.
The supporting side wall 4 is provided with a side wall plate 41 on one side of the machine base 1, two ends of the side wall plate 41 are provided with convex skin connecting frames 42, the skin connecting frames 42 are fixedly connected with the outer sides of two ends of the fixed skin section 3, the shape of the skin connecting frames 42 is matched with that of the fixed skin section 3, and the skin connecting frames 42 are better connected with the outer sides of the fixed skin section in a matched mode.
The inner sides of the fixed skin sections 3 are provided with support columns 2 arranged at intervals, the support columns 2 are fixedly connected through transverse connecting rods, and the rigidity of the fixed skin sections 3 can be enhanced through the support columns 2 and cross rods between the support columns.
The flip cover skin section 5 comprises a fuselage skin 51 with an arc-shaped appearance, two ends of the fuselage skin 51 are provided with convex skin side plates 52, the skin side plates 52 are fixedly connected through supporting connecting plates 53, the training hatch cover 8 is positioned between the upper supporting connecting plate 53 and the lower supporting connecting plate 53, the rigidity of the whole structure of the flip cover skin section 5 is enhanced through the skin side plates 52 and the supporting connecting plates 53, and the flip cover skin section can bear larger dismounting stress.
The fixed skin engaging lug 7 of fixed connection is arranged at the upper end of the inner side of the fixed skin section 3, the turning skin engaging lug 6 of fixed connection is arranged at the lower part of the inner side of the two ends of the turning cover skin section 5, the end part of the fixed skin engaging lug 7 is rotationally connected with the end part of the turning skin engaging lug 6, the turning cover skin section 5 is combined with the fixed skin section 3 when being unfolded through the turning skin engaging lug 6 and the fixed skin engaging lug 7, and the actual dismounting environment of the real machine can be simulated in height and appearance as much as possible.
Claims (6)
1. Aviation cabin cover dismouting trainer, characterized by: including board base (1), board base (1) side is equipped with supports lateral wall (4), support lateral wall (4) and fixed covering section (3) fixed connection, the inboard upper end of fixed covering section (3) rotates with the inboard lower extreme of flip covering section (5) to be connected, rotation through flip covering section (5) realizes expandeing and folding, the appearance of fixed covering section (3) and flip covering section (5) is the arc, be used for simulating real aircraft fuselage appearance, be equipped with multiple training cabin cover (8) on flip covering section (5), be used for carrying out cabin cover dismouting training.
2. An aviation hatch cover assembly and disassembly training device as in claim 1, wherein the training hatch cover (8) comprises a quick-release screw hatch cover (81), a cross-pin hatch cover (82) and a screw hatch cover (83), and the three hatch covers are detachably connected with the flip cover skin section (5).
3. The aircraft hatch cover assembly and disassembly training device as claimed in claim 1, wherein the supporting side wall (4) is provided with a side wall plate (41) at one side of the machine base (1), two ends of the side wall plate (41) are provided with protruding skin connecting frames (42), the skin connecting frames (42) are fixedly connected with the outer sides of two ends of the fixed skin section (3), and the shape of the skin connecting frames (42) is matched with that of the fixed skin section (3).
4. The aviation hatch cover dismounting training device according to claim 3, characterized in that the inner side of the fixed skin section (3) is provided with support columns (2) arranged at intervals, and the support columns (2) are fixedly connected through transverse connecting rods.
5. The aircraft hatch cover assembly and disassembly training device as claimed in claim 3, wherein the flip cover skin section (5) comprises a fuselage skin (51) with an arc-shaped appearance, two ends of the fuselage skin (51) are provided with protruding skin side plates (52), the skin side plates (52) are fixedly connected through supporting connecting plates (53), and the training hatch cover (8) is positioned between the upper supporting connecting plate and the lower supporting connecting plate (53).
6. The aircraft hatch cover assembly and disassembly training device as claimed in claim 1, wherein the fixed skin section (3) is provided with a fixed skin engaging lug (7) at the upper end of the inner side thereof, the flip skin section (5) is provided with a flip skin engaging lug (6) at the lower part of the inner side thereof, the end part of the fixed skin engaging lug (7) is rotatably connected with the end part of the flip skin engaging lug (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121941650.8U CN215868237U (en) | 2021-08-18 | 2021-08-18 | Aviation cabin cover dismouting trainer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121941650.8U CN215868237U (en) | 2021-08-18 | 2021-08-18 | Aviation cabin cover dismouting trainer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215868237U true CN215868237U (en) | 2022-02-18 |
Family
ID=80240227
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121941650.8U Active CN215868237U (en) | 2021-08-18 | 2021-08-18 | Aviation cabin cover dismouting trainer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215868237U (en) |
-
2021
- 2021-08-18 CN CN202121941650.8U patent/CN215868237U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE10013442C1 (en) | Offshore wind turbine power plant has container housing electrical operating component positioned at side of machine housing provided with helicopter landing platform | |
| CN201544017U (en) | Maintenance cart dedicated for disassembling and assembling multifunctional automobile gearbox | |
| CN215868237U (en) | Aviation cabin cover dismouting trainer | |
| CN207694173U (en) | A kind of limbs strength test device | |
| CN216562157U (en) | Suspension type aircraft cabin simulation system | |
| EP2432953B1 (en) | Rescue training equipment | |
| CN212084423U (en) | Airborne pod simulation system | |
| CN101685124A (en) | Electromagnetic compatibility quick detecting platform for wire cable layout of helicopter | |
| CN109573100B (en) | Iron bird test stand | |
| CN112109890B (en) | A folding oar presss from both sides drive assembly for unmanned aerial vehicle | |
| CN202795790U (en) | Multimedia teaching equipment | |
| GB2281269A (en) | Transportable aircraft safety training device. | |
| CN210574408U (en) | Boarding bridge docking simulator | |
| CN212500990U (en) | Folding unmanned aerial vehicle of easy dismouting | |
| CN114429722A (en) | Desktop training ware is maintained to aircraft | |
| CN218273723U (en) | Integrative frame of implementation training | |
| CN114882757B (en) | Parachute landing simulator capable of truly sensing wind pressure | |
| CN219778370U (en) | Vehicle-mounted helicopter medical rescue simulation device | |
| CN210574434U (en) | Training device for debugging and troubleshooting of motor train unit | |
| CN215182694U (en) | Ship subsection internal structure model for teaching | |
| CN216133574U (en) | Simulation system device convenient for demonstration of main landing gear of airplane | |
| CN220155034U (en) | Emergency drilling training device for driving of high-speed railway train | |
| CN216596670U (en) | Aircraft maintenance skill teaching ladder frame | |
| CN221632117U (en) | Two-station electromechanical integrated training device | |
| CN204979149U (en) | Square fretwork pin -connected panel instrument carries on platform |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |