CN112700691A - Air refueling simulation mechanism - Google Patents
Air refueling simulation mechanism Download PDFInfo
- Publication number
- CN112700691A CN112700691A CN202011420012.1A CN202011420012A CN112700691A CN 112700691 A CN112700691 A CN 112700691A CN 202011420012 A CN202011420012 A CN 202011420012A CN 112700691 A CN112700691 A CN 112700691A
- Authority
- CN
- China
- Prior art keywords
- scissor
- seat
- mounting
- mount
- transition
- 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.)
- Pending
Links
- 230000007246 mechanism Effects 0.000 title claims abstract description 41
- 238000004088 simulation Methods 0.000 title claims abstract description 27
- 230000007704 transition Effects 0.000 claims abstract description 37
- 238000009434 installation Methods 0.000 claims abstract description 29
- 210000001503 joint Anatomy 0.000 claims abstract description 28
- 238000003032 molecular docking Methods 0.000 claims description 34
- 238000013016 damping Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 8
- 230000008569 process Effects 0.000 description 8
- 230000000694 effects Effects 0.000 description 3
- 238000013459 approach Methods 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 230000003116 impacting effect Effects 0.000 description 2
- 206010023230 Joint stiffness Diseases 0.000 description 1
- 230000008094 contradictory effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/085—Special purpose teaching, e.g. alighting on water, aerial photography
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
The invention discloses an aerial refueling simulation mechanism, which comprises an installation rack, a butt joint device and a position adjusting device, wherein the installation rack is provided with a support; the mounting rack is movably arranged along the left and right directions; the butt joint device comprises a transition seat arranged on the installation rack, an installation seat arranged on the transition seat and a butt joint arranged on the installation seat; the position adjusting device comprises a height adjusting assembly with a vertical height adjusting stroke and a horizontal adjusting assembly with a horizontal adjusting stroke, wherein one of the horizontal adjusting assembly and the height adjusting assembly is arranged between the mounting rack and the transition seat, and the other one of the horizontal adjusting assembly and the height adjusting assembly is arranged between the transition seat and the mounting seat. The installation rack moves in the left-right direction to simulate the motion state of an aerial body, the position adjusting structure controls the transition seat and the installation seat to move in the up-down direction and the horizontal direction, and controls the butt joint to adjust the position in a three-dimensional space so as to simulate the real aerial refueling state.
Description
Technical Field
The invention relates to the field of laboratory simulation equipment, in particular to an aerial refueling simulation mechanism.
Background
In the aircraft air refueling flight test process, the docking stage is the highest risk stage, the docking process is influenced by air flow, engine tail jet vortex and other influence factors, and in the process that a taper sleeve main body of a refueling nacelle approaches an oil receiving head of an oil receiving machine, the relative swinging amount of the taper sleeve is too large, so that a safety accident of impacting a target aircraft can be caused.
Disclosure of Invention
The invention mainly aims to provide an aerial refueling simulation mechanism, aiming at solving the problem of difficult aerial refueling space simulation.
In order to achieve the above object, the present invention provides an aerial refueling simulation mechanism, comprising:
the mounting frame is movably arranged along the left and right direction;
the butt joint device comprises a transition seat arranged on the installation rack, an installation seat arranged on the transition seat and a butt joint arranged on the installation seat; and the number of the first and second groups,
the position adjusting device comprises a height adjusting assembly with a vertical height adjusting stroke and a horizontal adjusting assembly with a horizontal adjusting stroke, wherein one of the horizontal adjusting assembly and the height adjusting assembly is arranged between the mounting rack and the transition seat, and the other one of the horizontal adjusting assembly and the height adjusting assembly is arranged between the transition seat and the mounting seat.
Optionally, the aerial refueling simulation mechanism further comprises a base;
the installation frame is to movable mounting extremely to about along on the up end of base, the installation frame with be provided with sliding fit structure between the relative terminal surface of base, sliding fit structure is including the slide rail and the pulley that mutually support and set up, the slide rail with in the pulley, one of them is located on the base, another is located on the installation frame, wherein, the slide rail is along controlling to extending the setting.
Optionally, the aerial refueling simulation mechanism further comprises a conveyor belt, the conveyor belt is arranged on the base and has a conveying stroke along the left-right direction, and the upper end face of the conveyor belt is used for driving the mounting rack to move.
Optionally, the mount includes:
the bearing plate is arranged on the transition seat; and the number of the first and second groups,
the mounting seat body is mounted on the bearing plate, a movable groove and a mounting block which are matched with each other are arranged between the mounting seat body and the opposite end surfaces of the bearing plate, and the mounting block is movably mounted in the movable groove along the horizontal direction;
wherein the docking head is mounted to the mount body.
Optionally, the docking device further includes a plurality of elastic restoring members disposed between the side wall surface of the mounting seat body and the mounting rack, and the elastic restoring members are disposed at intervals along the circumferential direction of the mounting seat.
Optionally, the docking device further includes a buffer structure, and the buffer structure is disposed between the mounting seat and the docking head, so that the docking head is movably mounted on the mounting seat.
Optionally, a ball groove is concavely arranged on the mounting seat;
the butt joint device further comprises a connecting rod, one end of the connecting rod is provided with a ball head corresponding to the ball groove, and the ball head is movably mounted in the ball groove;
the butt joint is fixedly mounted to the other end of the connecting rod;
the ball groove and the connecting rod form the buffer structure.
Optionally, the buffering structure further comprises a return spring fixedly sleeved on the connecting rod, and one end of the return spring abuts against the mounting seat.
Optionally, the height adjusting assembly is disposed between the mounting rack and the transition seat, and includes a scissor mechanism, the scissor mechanism is disposed in an up-down direction, the scissor mechanism includes a plurality of scissor units connected in the up-down direction, each scissor unit includes a first scissor arm and a second scissor arm, the middle positions of the first scissor arm and the second scissor arm are hinged to each other, the scissor units are located in two adjacent scissor units in the up-down direction, a lower end of the first scissor arm of the upper scissor unit is hinged to an upper end of the second scissor arm of the lower scissor unit, and a lower end of the second scissor arm of the upper scissor unit is hinged to an upper end of the first scissor arm of the lower scissor unit;
the plurality of scissor units comprise adjusting scissor units positioned at the lower ends, and the distance between the lower ends of the first scissor arms and the lower ends of the second scissor arms of the adjusting scissor units is adjustable;
the lower end of the scissor mechanism is mounted on the mounting rack, and the transition seat is mounted at the upper end of the scissor mechanism.
Optionally, the horizontal adjustment assembly is mounted between the transition seat and the mounting seat, and includes a first slide seat movably mounted on the transition seat and a second slide seat movably mounted on the first slide seat, one of the first slide seat and the second slide seat is movably disposed in a front-back direction, and the other is movably disposed in a left-right direction;
wherein the mount is mounted to the second carriage.
In the technical scheme of the invention, the mounting rack moves in the left and right directions to simulate the motion state of an aerial body, the butt joint is used for simulating an oil filling joint, the position adjusting structure controls the transition seat and the mounting seat to move in the up and down directions and the horizontal direction, and controls the butt joint to adjust the position in a three-dimensional space to be butted with an external oil supply part, so that the real aerial oil filling state is simulated, and the program and the oil filling mechanism are conveniently adjusted.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
Fig. 1 is a schematic perspective view of an aerial refueling simulation device according to an embodiment of the present invention;
FIG. 2 is a schematic perspective view of the docking device and the position adjustment device shown in FIG. 1;
FIG. 3 is a schematic perspective view of the docking device shown in FIG. 1;
FIG. 4 is a schematic perspective view of the carrier plate shown in FIG. 1;
FIG. 5 is a front cross-sectional view of the docking device of FIG. 1;
FIG. 6 is a perspective view of the height adjustment assembly of FIG. 1;
fig. 7 is a schematic perspective view of the horizontal adjustment assembly shown in fig. 1.
The reference numbers illustrate:
| reference numerals | Name (R) | Reference numerals | Name (R) |
| 100 | Aerial |
26 | Reset spring |
| 1 | |
3 | Position adjusting |
| 2 | |
31 | |
| 21 | |
311 | |
| 22 | |
312 | |
| 221 | |
32 | |
| 222 | |
321 | |
| 23 | |
322 | |
| 24 | Reset elastic piece | 4 | |
| 25 | Connecting |
5 | Conveyor belt |
The implementation, functional features and advantages of the objects of the present invention will be further explained with reference to the accompanying drawings.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
It should be noted that, if directional indication is involved in the embodiment of the present invention, the directional indication is only used for explaining the relative positional relationship, the motion situation, and the like between the components in a certain posture, and if the certain posture is changed, the directional indication is changed accordingly.
In addition, if there is a description of "first", "second", etc. in an embodiment of the present invention, the description of "first", "second", etc. is for descriptive purposes only and is not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, technical solutions between various embodiments may be combined with each other, but must be realized by a person skilled in the art, and when the technical solutions are contradictory or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.
In the aircraft air refueling flight test process, the docking stage is the highest risk stage, the docking process is influenced by air flow, engine tail jet vortex and other influence factors, and in the process that a taper sleeve main body of a refueling nacelle approaches an oil receiving head of an oil receiving machine, the relative swinging amount of the taper sleeve is too large, so that a safety accident of impacting a target aircraft can be caused.
The invention provides an aerial refueling simulation mechanism, aiming at solving the problem of difficult aerial refueling space simulation.
Referring to fig. 1 to 2, the present invention provides an aerial refueling simulation mechanism 100, which includes an installation frame 1, a docking device 2 and a position adjustment device 3; the mounting rack 1 is movably arranged along the left-right direction; the docking device 2 comprises a transition seat 21 arranged on the installation rack 1, an installation seat 22 arranged on the transition seat 21, and a docking head 23 arranged on the installation seat 22; the position adjusting device 3 comprises a height adjusting assembly 31 with a vertical height adjusting stroke and a horizontal adjusting assembly 32 with a horizontal adjusting stroke, wherein one of the horizontal adjusting assembly 32 and the height adjusting assembly 31 is arranged between the installation rack 1 and the transition seat 21, and the other one is arranged between the transition seat 21 and the installation seat 22.
In the technical scheme of the invention, the mounting frame 1 moves in the left and right directions to simulate the motion state of an aerial body, the butt joint 23 is used for simulating an oil filling joint, the position adjusting structure 3 controls the transition seat 21 and the mounting seat 22 to move in the up-down direction and the horizontal direction, and controls the butt joint 23 to adjust the position in a three-dimensional space to be in butt joint with an external oil supplying part, so that the real aerial oil filling state is simulated, and the program and the oil filling mechanism are conveniently adjusted.
In this embodiment, the airborne fueling simulation mechanism 100 further includes a base 4; installing frame 1 is to movable mounting extremely about along on the up end of base 4, installing frame 1 with be provided with the sliding fit structure between the relative terminal surface of base 4, the sliding fit structure is including the slide rail and the pulley that mutually support and set up, the slide rail with in the pulley, one of them is located on the base 4, another is located on the installing frame 1, wherein, the slide rail is along controlling to extending the setting. Through the slide rail with the cooperation of pulley guarantees the activity of installation frame 1 is steady, and is convenient for control activity route and stroke, is convenient for simulate the active state of organism.
Further, the aerial refueling simulation mechanism 100 further comprises a conveyor belt 5, the conveyor belt is arranged on the base 4, the conveyor belt 5 has a conveying stroke along the left-right direction, and the upper end surface of the conveyor belt 5 is used for driving the mounting rack 1 to move.
Specifically, in this embodiment, two protruding blocks are formed at the upper end surface of the conveyor belt 5 and are arranged at intervals in the left-right direction, the installation frame 1 is installed between the two protruding blocks, the conveyor belt 5 moves, and one of the protruding blocks abuts against the installation frame 1 to drive the installation frame 1 to move.
In addition, referring to fig. 3 to 4, the mounting base 22 includes a carrier 221 and a mounting base body 222; the bearing plate 221 is arranged on the transition seat 21; the mounting seat body 222 is mounted on the bearing plate 221, a movable groove and a mounting block which are matched with each other are arranged between the opposite end surfaces of the mounting seat body 222 and the bearing plate 221, and the mounting block is movably mounted in the movable groove along the horizontal direction; wherein the docking head 23 is mounted to the mount body 222. When the docking head 23 is docked, in order to avoid hard collision between the docking head and the oil feeding device, the mounting seat body 222 is movably mounted on the bearing plate 221 in the horizontal direction, and when the collision occurs, the mounting seat body 222 has a certain buffer space to prevent the docking head 23 from being damaged during docking.
Further, the docking device 2 further includes a plurality of elastic restoring members 24 disposed between the side wall surface of the mounting seat body 222 and the mounting rack 1, and the plurality of elastic restoring members 24 are disposed at intervals along the circumferential direction of the mounting seat 22. After the collision and docking are successful and the docking is completed, the mount body 222 is driven to be restored to the original position by the reset elastic piece 24.
In this embodiment, the return elastic member 24 is a spring.
In this embodiment, the docking device 2 further includes a buffer structure, which is disposed between the mounting seat 22 and the docking head 23, so that the docking head 23 is movably mounted on the mounting seat 22. When in butt joint, the butt joint is stressed and can shake and deflect, and the buffer structure prevents the butt joint 23 from being damaged by impact during butt joint.
Specifically, referring to fig. 5, a ball groove is concavely formed on the mounting seat 22; the butt joint device 2 further comprises a connecting rod 25, one end of the connecting rod 25 is provided with a ball head corresponding to the ball groove, and the ball head is movably mounted in the ball groove; the butt joint 23 is fixedly mounted to the other end of the connecting rod 25; the ball grooves and the connecting rods 25 form the buffer structure. When the butt joint 23 collides, the butt joint 23 drives the connecting rod 25 to move along the ball groove, so that deflection of a certain angle and a certain range is generated, the structure is simple, and the anti-collision effect is good.
Further, the buffering structure further includes a return spring 26 fixedly sleeved on the connecting rod 25, and one end of the return spring 26 abuts against the mounting seat 22. After the butt joint 23 deflects, the connecting rod 25 is driven to reset by the reset spring 26, so that the butt joint tightness is facilitated.
Referring to fig. 6, in the present invention, the height adjusting assembly 31 is disposed between the mounting rack 1 and the transition seat 21, the height adjusting assembly 31 includes a scissor mechanism, the scissor mechanism is disposed along an up-down direction, the scissor mechanism includes a plurality of scissor units connected in the up-down direction, each scissor unit includes a first scissor arm 311 and a second scissor arm 312, which are hinged to each other at middle positions, and are located in two adjacent scissor units in the up-down direction, a lower end of the first scissor arm 311 of the upper scissor unit is hinged to an upper end of the second scissor arm 312 of the lower scissor unit, and a lower end of the second scissor arm 312 of the upper scissor unit is hinged to an upper end of the first scissor arm 311 of the lower scissor unit; the plurality of scissor units comprise adjusting scissor units positioned at the lower ends, and the distance between the lower ends of the first scissor arms 311 and the second scissor arms 312 of the adjusting scissor units is adjustable; the lower end of the scissor mechanism is mounted on the mounting rack 1, and the transition seat 21 is mounted at the upper end of the scissor mechanism. The height of the transition seat 21 is adjusted through the scissors mechanism, and then the height of the butt joint 23 is adjusted, so that the oil feeding part is aligned in the vertical direction.
In addition, referring to fig. 7, the horizontal adjustment assembly 32 is mounted between the transition seat 21 and the mounting seat 22, and includes a first sliding seat 321 movably mounted on the transition seat 21 and a second sliding seat 322 movably mounted on the first sliding seat 321, one of the first sliding seat 321 and the second sliding seat 322 is movably disposed along the front-back direction, and the other is movably disposed along the left-right direction; wherein the mounting seat 22 is mounted to the second slider 322. So that the mounting seat 22 has a moving stroke in the front-back direction and the left-right direction, thereby simulating the docking process of the docking head 23 in the horizontal upward direction.
It should be noted that the horizontal adjustment assembly 32 further includes a driving motor, so as to drive the first sliding base 321 and the second sliding base 322 to slide. In addition, a sliding fit structure is arranged between the first sliding seat 321 and the transition seat 21, and the sliding fit structure comprises a sliding rail and a sliding groove which are matched with each other, so that the horizontal sliding is realized, and the sliding process is stable. The oil sliding fit structure is also arranged between the second sliding seat 322 and the first sliding seat 321.
The above description is only a preferred embodiment of the present invention, and not intended to limit the scope of the present invention, and all modifications and equivalents made by the contents of the present specification and drawings, or directly/indirectly applied to other related technical fields, are included in the scope of the present invention.
Claims (10)
1. An airborne fueling simulation mechanism, comprising:
the mounting frame is movably arranged along the left and right direction;
the butt joint device comprises a transition seat arranged on the installation rack, an installation seat arranged on the transition seat and a butt joint arranged on the installation seat; and the number of the first and second groups,
the position adjusting device comprises a height adjusting assembly with a vertical height adjusting stroke and a horizontal adjusting assembly with a horizontal adjusting stroke, wherein one of the horizontal adjusting assembly and the height adjusting assembly is arranged between the mounting rack and the transition seat, and the other one of the horizontal adjusting assembly and the height adjusting assembly is arranged between the transition seat and the mounting seat.
2. The airborne fueling simulation mechanism of claim 1, further comprising a base;
the installation frame is to movable mounting extremely to about along on the up end of base, the installation frame with be provided with sliding fit structure between the relative terminal surface of base, sliding fit structure is including the slide rail and the pulley that mutually support and set up, the slide rail with in the pulley, one of them is located on the base, another is located on the installation frame, wherein, the slide rail is along controlling to extending the setting.
3. The airborne fueling simulation mechanism of claim 2, further comprising a conveyor belt disposed on the base, the conveyor belt having a left-right direction travel, an upper end of the conveyor belt being configured to drive the mounting frame.
4. The airborne fueling simulation mechanism of claim 1, wherein the mounting base comprises:
the bearing plate is arranged on the transition seat; and the number of the first and second groups,
the mounting seat body is mounted on the bearing plate, a movable groove and a mounting block which are matched with each other are arranged between the mounting seat body and the opposite end surfaces of the bearing plate, and the mounting block is movably mounted in the movable groove along the horizontal direction;
wherein the docking head is mounted to the mount body.
5. The airborne fueling simulation mechanism of claim 4, wherein the docking assembly further comprises a plurality of return springs disposed between the sidewall surface of the mount base body and the mount frame, the plurality of return springs being spaced circumferentially of the mount base.
6. The airborne fueling simulation mechanism of claim 1, wherein the docking assembly further comprises a cushion structure disposed between the mount and the docking head for movably mounting the docking head to the mount.
7. An airborne fueling simulation mechanism as set forth in claim 6, wherein said mounting block is recessed with a ball groove;
the butt joint device further comprises a connecting rod, one end of the connecting rod is provided with a ball head corresponding to the ball groove, and the ball head is movably mounted in the ball groove;
the butt joint is fixedly mounted to the other end of the connecting rod;
the ball groove and the connecting rod form the buffer structure.
8. The airborne fueling simulation mechanism of claim 7, wherein the damping structure further comprises a return spring fixedly sleeved on the connecting rod, and wherein one end of the return spring abuts against the mounting seat.
9. The aerial refueling simulation mechanism as recited in claim 1, wherein the height adjustment assembly is disposed between the mounting frame and the transition seat, the height adjustment assembly includes a scissor mechanism, the scissor mechanism is disposed in an up-down direction, the scissor mechanism includes a plurality of scissor units connected in the up-down direction, each scissor unit includes a first scissor arm and a second scissor arm hinged to each other at a middle position, the scissor arms are disposed in two adjacent scissor units in the up-down direction, a lower end of the first scissor arm of the upper scissor unit is hinged to an upper end of the second scissor arm of the lower scissor unit, and a lower end of the second scissor arm of the upper scissor unit is hinged to an upper end of the first scissor arm of the lower scissor unit;
the plurality of scissor units comprise adjusting scissor units positioned at the lower ends, and the distance between the lower ends of the first scissor arms and the lower ends of the second scissor arms of the adjusting scissor units is adjustable;
the lower end of the scissor mechanism is mounted on the mounting rack, and the transition seat is mounted at the upper end of the scissor mechanism.
10. The airborne fueling simulation mechanism of claim 1, wherein said leveling assembly is mounted between said transition mount and said mounting mount and comprises a first slide movably mounted to said transition mount and a second slide movably mounted to said first slide, one of said first and second slides being movably disposed in a fore-and-aft direction and the other being movably disposed in a left-and-right direction;
wherein the mount is mounted to the second carriage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011420012.1A CN112700691A (en) | 2020-12-07 | 2020-12-07 | Air refueling simulation mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011420012.1A CN112700691A (en) | 2020-12-07 | 2020-12-07 | Air refueling simulation mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112700691A true CN112700691A (en) | 2021-04-23 |
Family
ID=75506259
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011420012.1A Pending CN112700691A (en) | 2020-12-07 | 2020-12-07 | Air refueling simulation mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112700691A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115424496A (en) * | 2022-08-31 | 2022-12-02 | 北京蓝天航空科技股份有限公司 | Air refueling training simulation system |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6059574A (en) * | 1998-06-11 | 2000-05-09 | The United States Of America As Represented By The Secretary Of The Navy | Aircraft fuel trainer with low viscosity/high flashpoint fuel look-alike |
| CN106742055A (en) * | 2016-12-13 | 2017-05-31 | 长春市科泰致达科技有限公司 | A kind of ground simulation aircraft adds by oily umbrella tapered sleeve anti-collision structure |
| CN206327586U (en) * | 2016-12-13 | 2017-07-14 | 长春市科泰致达科技有限公司 | A kind of aircraft adds by oily analogue means |
| CN108372402A (en) * | 2016-12-21 | 2018-08-07 | 中国航空工业集团公司北京航空制造工程研究所 | The adaptive location device and posture adjustment docking system and control method of big component docking |
| CN207895728U (en) * | 2017-10-25 | 2018-09-21 | 江苏屹高鹰视文化传播有限公司 | Aircraft Air oiling pseudo-experience device |
| CN208378320U (en) * | 2018-06-01 | 2019-01-15 | 广东嘉腾机器人自动化有限公司 | Actuator lifting device |
| CN210372749U (en) * | 2019-02-24 | 2020-04-21 | 谢小军 | Safety fixing equipment for access control card reader |
| CN211506813U (en) * | 2020-01-19 | 2020-09-15 | 南京航空航天大学 | Experimental platform for simulating air two-engine refueling and docking |
| CN211649589U (en) * | 2020-01-21 | 2020-10-09 | 东曜药业有限公司 | Butt-joint mechanism of AB valve |
| CN211761304U (en) * | 2020-03-09 | 2020-10-27 | 李建平 | Multipurpose detection platform |
-
2020
- 2020-12-07 CN CN202011420012.1A patent/CN112700691A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6059574A (en) * | 1998-06-11 | 2000-05-09 | The United States Of America As Represented By The Secretary Of The Navy | Aircraft fuel trainer with low viscosity/high flashpoint fuel look-alike |
| CN106742055A (en) * | 2016-12-13 | 2017-05-31 | 长春市科泰致达科技有限公司 | A kind of ground simulation aircraft adds by oily umbrella tapered sleeve anti-collision structure |
| CN206327586U (en) * | 2016-12-13 | 2017-07-14 | 长春市科泰致达科技有限公司 | A kind of aircraft adds by oily analogue means |
| CN108372402A (en) * | 2016-12-21 | 2018-08-07 | 中国航空工业集团公司北京航空制造工程研究所 | The adaptive location device and posture adjustment docking system and control method of big component docking |
| CN207895728U (en) * | 2017-10-25 | 2018-09-21 | 江苏屹高鹰视文化传播有限公司 | Aircraft Air oiling pseudo-experience device |
| CN208378320U (en) * | 2018-06-01 | 2019-01-15 | 广东嘉腾机器人自动化有限公司 | Actuator lifting device |
| CN210372749U (en) * | 2019-02-24 | 2020-04-21 | 谢小军 | Safety fixing equipment for access control card reader |
| CN211506813U (en) * | 2020-01-19 | 2020-09-15 | 南京航空航天大学 | Experimental platform for simulating air two-engine refueling and docking |
| CN211649589U (en) * | 2020-01-21 | 2020-10-09 | 东曜药业有限公司 | Butt-joint mechanism of AB valve |
| CN211761304U (en) * | 2020-03-09 | 2020-10-27 | 李建平 | Multipurpose detection platform |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115424496A (en) * | 2022-08-31 | 2022-12-02 | 北京蓝天航空科技股份有限公司 | Air refueling training simulation system |
| CN115424496B (en) * | 2022-08-31 | 2023-09-26 | 北京蓝天航空科技股份有限公司 | Aerial refueling training simulation system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10654381B2 (en) | Vehicle seat comprising adjustable damper | |
| CA2510581A1 (en) | Movement device | |
| CN112700691A (en) | Air refueling simulation mechanism | |
| CN111741896A (en) | Aircraft with a flight control device | |
| US20150308921A1 (en) | Simulator | |
| CN107328543B (en) | Impact test stand | |
| KR102112475B1 (en) | Apparatus for testing air vehicle on ground | |
| CN213753263U (en) | Automatic docking mechanism and fill electric pile charge that charge | |
| CN111601735B (en) | Device for suspending a lamp in a vehicle | |
| CN111465531A (en) | Device for suspending a lamp in a vehicle | |
| CN105424344A (en) | Debugging device used for airplane calibration test deformation structure loading actuator | |
| EP3278323B1 (en) | Motion arrangement | |
| KR101657176B1 (en) | Pedestal apparatus for satellite tracking antenna | |
| CN104238273A (en) | Safety protection device for workpiece table | |
| US20210178941A1 (en) | Vehicle seat with scissor frame arrangement | |
| WO2019069077A1 (en) | Motion arrangement | |
| CN206327586U (en) | A kind of aircraft adds by oily analogue means | |
| CN112289727B (en) | Chip position adjusting mechanism and chip transmission mechanism | |
| CN106347525B (en) | Adjustable pedal installation device | |
| CN105835990A (en) | Tool and method for positioning H point of total arrangement space verification model of passenger car | |
| CN108908300B (en) | Two-rotation one-translation three-freedom-degree motion platform | |
| KR100785424B1 (en) | Device for transferring heavy load using air bearing | |
| US11014700B2 (en) | Packaging machine with compensation cylinder | |
| CN110745443B (en) | High-speed stacker with buffer guiding device | |
| CN106742055A (en) | A kind of ground simulation aircraft adds by oily umbrella tapered sleeve anti-collision structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20210423 |