CN109533388A - A kind of helicopter cockpit ergonomic Universal Assessment platform - Google Patents
A kind of helicopter cockpit ergonomic Universal Assessment platform Download PDFInfo
- Publication number
- CN109533388A CN109533388A CN201811361729.6A CN201811361729A CN109533388A CN 109533388 A CN109533388 A CN 109533388A CN 201811361729 A CN201811361729 A CN 201811361729A CN 109533388 A CN109533388 A CN 109533388A
- Authority
- CN
- China
- Prior art keywords
- cockpit
- helicopter
- floor
- platform
- console
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
Abstract
The present invention provides a kind of helicopter cockpit ergonomic Universal Assessment platforms, belong to helicopter man-machine efficacy design field.Described device includes cockpit floor, is equipped with seat, center console, instrument board and the top console of helicopter cockpit thereon；The instrument board, center console, top console and seat pass through supporting element and are mounted on the cockpit floor, and supporting element height is adjustable；The seat along cockpit central axes it is symmetrical there are two, bottom is mounted on the cockpit floor by horizontal slide rail, and the chair top is connected by rotating mechanism with leaning against.The invention can be used for assessing the cockpit visual field of different helicopters, accessibility, comfort, according to the assessment result of helicopter cockpit manufacture claim and practical flight person, provides input for helicopter type design, reduces iteration time, promotes assessment efficiency.
Description
Technical field
The invention belongs to helicopter man-machine efficacy design fields, and in particular to a kind of helicopter cockpit ergonomic is general
Evaluation Platform.
Background technique
Helicopter cockpit Universal Assessment is a very important link in helicopter cockpit development process, in order to mention
It rises the development efficiency of cockpit and reduces and spend, a cockpit engineering prototype platform need to be constructed in the cockpit development stage, used
In verifying helicopter ergonomic design, the comfort of visuality, accessibility and manipulation comprising driver.Existing helicopter
Cockpit engineering simulator usually with helicopter cockpit design is developed according to the true size of 1:1, is developing rank
Section verifying design rationality, needs to redesign, then proceedes to iterative estimation for unreasonable place, until assessment satisfaction is
Only, the disadvantage is that the period is too long, the result of assessment can not provide effective input to design, usually for each different helicopter types
Number it is both needed to develop a cockpit engineering prototype, somewhat expensive, the period is too long.
Summary of the invention
The present invention provides a kind of helicopter cockpit ergonomic Universal Assessment platforms, to solve, assess existing go straight up to
Subproblem present in machine type design.
Helicopter cockpit ergonomic Universal Assessment platform of the present invention, comprising:
Cockpit floor, for installing seat, center console, instrument board and the top manipulation of helicopter cockpit
Platform；
Bottom support, is used to support the cockpit floor, and the bottom support is height-adjustable structure；
Instrument board is mounted on the cockpit floor by fascia supports frame, and the fascia supports frame height can
It adjusts；
Center console is mounted on the cockpit floor, the center console by center console supporting element
Supporting element height is adjustable；
Top console is mounted on the cockpit floor by top console supporting element, the top console
Supporting element height is adjustable；
Seat, along cockpit central axes it is symmetrical there are two, bottom by horizontal slide rail with being mounted on the cockpit
On plate, the chair top of the seat is connected by rotating mechanism with leaning against.
Preferably, the bottom support includes bottom platform, the support rod upwardly extended by bottom platform, the branch
Cylinder is made in the other side connection of strut, and the other side for making cylinder is connected to the bottom on the cockpit floor.
Preferably, the bottom support rod includes at least 3, is distributed in isosceles triangle.
Preferably, further include left-hand drive bar and right control stick, be arranged symmetrically in two drivers along cockpit central axes
It on the center line of seat, is mounted on floor by horizontal slide rail, control stick bottom is connect with force-feedback control box respectively.
Preferably, further include left collective-pitch lever and right collective-pitch lever, be installed in the left side of driver and copilot seat, pass through cross
It is mounted on floor to sliding rail, collective-pitch lever bottom is connect with force-feedback control box respectively.
Preferably, further include left side staircase and right side staircase, connect ground and cockpit floor.
Preferably, further include left side pedal and right side pedal, be symmetrical arranged along cockpit central axes, pass through transverse direction respectively
Sliding rail is mounted on cockpit floor.
Helicopter cockpit Universal Assessment platform of the invention, can be used for assessing different helicopters the cockpit visual field, can
It is mentioned up to property, comfort according to the assessment result of helicopter cockpit manufacture claim and practical flight person for helicopter type design
For input, iteration time is reduced, promotes assessment efficiency, each helicopter Project R&D of effective solution needs manufacture one
The problem of cockpit platform, reduces cost allowance.
Detailed description of the invention
Fig. 1 is to show according to the structure of a preferred embodiment of helicopter cockpit man-machine efficacy Universal Assessment platform of the present invention
It is intended to.
Fig. 2 is the platform rearview of embodiment illustrated in fig. 1 of the present invention.
Wherein, 1- fascia supports frame, the mounting plate of 2- instrument board, 3- center console supporting element, 4- Left-Hand Side Console
Supporting element, 5- Right-Hand Side Console supporting element, the top 6- console supporting element, 7- left-side seat, 8- right-side seat, 9- left handle drive
Bar, 10- right hand drive bar, the left side 11- collective-pitch lever, the right side 12- collective-pitch lever, the left side 13- pedal, the right side 14- pedal, 15- drive
Cabin floor, 16- bottom support, the left side 17- staircase, the right side 18- staircase, 19- platform base, the top 20- console mounting plate.
Specific embodiment
A kind of helicopter cockpit ergonomic Universal Assessment platform, can be used for different helicopter cockpit type designs
It is assessed, comprising:
Cockpit floor: for installing the seat of helicopter cockpit, left, center, right console, instrument board, top manipulation
Platform supporting element；
Bottom support, all mechanism weight being used to support on helicopter floor, 3 bottom support bottoms and platform
Pedestal is fixedly connected, and 3 bottom support pillar upper ends couple with 3 actuator lower ends respectively, 3 actuator upper ends and driving
Cabin floor bottoms are fixedly connected, and by adjusting the height of 3 actuator respectively, helicopter simulating cockpit is in different flight planing surfaces
The terrain clearance of level inclination and different helicopter floors under state；
The mounting plate of instrument board, the mounting plate bottom of instrument board are fixedly connected with 3 actuator tops, the installation of instrument board
Plate is for installing instrument and display equipment；
Fascia supports frame, fascia supports frame lower section are fixedly mounted on floor, fascia supports frame upper end and 3 works
Dynamic device connection, 3 actuator upper ends are fixedly connected with instrument board mounting plate；Instrument can be carried out by adjusting actuator height respectively
The pitch angle and height adjustment of dash board, simulate different helicopter instrumentation plates terrain clearance size and different flight attitudes；
Center console installs case, as the mounting structure pattern of bottom support, center console installs case is used for
The commanding apparatus of helicopter basic configuration is installed.Center console installs case lower end is fixedly connected with 3 actuator upper ends, and 3
Actuator lower end is fixedly connected with cockpit floor mounting plate, can be by adjusting the height of 3 actuator respectively, to be simulated
Adjust the height and pitch angle of center console；
Left and right console installs case, left and right side console installs case is just the same, for installing the optional behaviour of helicopter
It is longitudinally set with standby.Left and right console installs case is prolonged cockpit central axes and is arranged symmetrically, installs case lower end respectively with 3 actuator upper ends
It is fixedly connected, 3 actuator lower ends and cockpit floor mounting plate are fixedly connected, and adjust behaviour by adjusting the height of actuator
Vertical platform terrain clearance, pitch orientation tilt angle；
Top console installs case is mounted on the console supporting element of top by a rotary shaft, is installed by rotation
Case come simulate top console pitching tilt angle；
Top console supporting element, is fixedly mounted on floor, top console supporting element and top console installs case
Connection, supporting element middle part are the pressurized struts of a customization, and top console can be adjusted to the height adjustment of pressurized strut by passing through
Height.
Pilot set, right side are positive pilot set, and left side is co pilot's seat, and driver and copilot seat prolongs driving
Cabin central axes are symmetrically installed, and bottom is mounted on floor by horizontal slide rail, pass through whirler between chair top and backrest
The rotation that structure carries out backrest is adjusted；The position of the horizontal slide rail of seat can be adjusted, simulate the seat of different tonnage helicopters
Spacing fixes seat after size determines；Due to current true helicopter is in view of anti-crash etc., backrest is equal
It is unadjustable, therefore the rotation angle of backrest need to be adjusted to assess the tilt angle that determining seat optimum is taken, it is mentioned for design
For reference.
Left and right control stick prolongs cockpit central axes and is arranged symmetrically on the center line of two pilot sets, installation approach
It as seat, is mounted on floor by horizontal slide rail, is simulated not by adjusting the position of horizontal slide rail of left and right control stick
With the spacing of tonnage helicopter control stick, control stick bottom is connect with force-feedback control box respectively, and there is no need to leverage connections to be
True force feedback effect can be experienced.
Left and right collective-pitch lever is installed in the left side of driver and copilot seat, is mounted on floor by horizontal slide rail, can
Prolong the spacing that sliding rail carries out left and right directions adjusting, the different tonnage helicopter collective-pitch levers of simulation, force feedback control is distinguished in collective-pitch lever bottom
Box connection processed, there is no need to leverage connections can experience true force feedback effect.
Left and right staircase, boarding staircase is for simulating true helicopter cockpit terrain clearance requirement, if going straight up to compared with large-tonnage
Machine generally uses rear to enter cockpit, can put together 2 groups of staircases, be placed in cockpit platform rear portion；Simulate small tonnage
Helicopter enters cockpit from left and right directions, and two groups of staircases can be moved to respectively to cockpit Evaluation Platform two sides, simulates from two sides
Into the boarding methods of cockpit.
Left and right pedal, 2 groups of pedals prolong cockpit central axes symmetrical placement on floor, are installed respectively by horizontal slide rail
On floor, the spacing of 2 groups of pedals is adjusted by the adjusting to position on sliding rail, can carry out simulating different helicopter pedals it
Between spacing.
With reference to Fig. 1-Fig. 2, the present invention relates to a kind of helicopter cockpit Universal Assessment platforms, and bottom mounting plate 16 is placed in
In ground grading, connect by 3 bottom supports 16 with cockpit floor 15, each bottom support 16 with corresponding actuation
Device lower end is connected, and actuator upper end couples with cockpit floor bottoms, by adjusting the height-adjustable of 3 actuator respectively
The terrain clearance of entire cockpit platform, tilt angle.
Cockpit floor 15 is hollow structure, is equipped with mounting plate 2, the center console of fascia supports frame 1, instrument board
Supporting element 3, Left-Hand Side Console supports support part 4, Right-Hand Side Console supporting element 5, top console supporting element 6, left-side seat
7, right-side seat 8, left handle drive bar 9, right hand drive bar 10, left side collective-pitch lever 11, right side collective-pitch lever 12, left side pedal 13, the right side
Batter pedals 14, bottom support 16, left side staircase 17, right side staircase 18, platform base 19, top console mounting plate 20.
Fascia supports frame 1 is fixedly mounted on floor, is fixedly connected by 3 actuator with the mounting plate 2 of instrument board, often
The adjustable height of a actuator is, it can be achieved that adjust the height of the mounting plate of instrument board, pitch angle.
3 bottom of center console supporting element is fixed on cockpit floor 15, is connected by 3 actuator, in 3 actuator
End and center console installs case are fixedly connected, the adjustable height of each actuator, it can be achieved that the height of center console,
Pitch angle is adjusted.
Left-Hand Side Console supporting element 4 and Right-Hand Side Console supporting element 5 are arranged symmetrically, and are separately fixed on floor, are made by 3
Dynamic device bottom is fixedly connected with transverse direction, height, tilt adjustment, it can be achieved that console by 2 horizontal slide rails with floor mounting plate.
Top console supporting element 6 is mounted on cockpit floor 15, can be made by adjusting in top console supporting element 6
The adjusting to top console height can be achieved in the height of dynamic cylinder, and top console mounting plate 20 can be realized by rotary shaft to top
The pitch angle of portion's console is adjusted.
Left-side seat 7 as 8 mounting means of right-side seat, prolong cockpit central axes and be symmetrically mounted on floor by the two,
Lateral adjustments are realized by bottom horizontal slide rail, backrest realizes angle tune by the rotary shaft between backrest and seat cushion
Section；
Left handle drive bar 9 as 10 mounting means of right hand drive bar, prolong cockpit central axes and be arranged symmetrically in ground by the two
On plate, left handle drive bar 9 and right hand drive bar 10 can realize lateral adjustments by bottom horizontal slide rail, below floor with force feedback
The connection of mechanism controls box is designed, it can be achieved that true force feedback effect according to true force feedback size.
Left side collective-pitch lever 11 is installed on the left of seat side as 12 mounting means of right side collective-pitch lever, sliding by bottom
Rail can realize lateral adjustments, connect below floor with force feedback mechanism control box, be designed according to true force feedback size,
True force feedback effect can be achieved.
Left side pedal 13 prolongs cockpit central axes and is symmetrically mounted on floor, pass through bottom transverse as right side pedal 14
Lateral adjustments can be realized to sliding rail, are connect below floor with force feedback mechanism control box, are carried out according to true force feedback size
Design is, it can be achieved that true force feedback effect.
Left side staircase 17 and right side staircase 18 are placed in cockpit Universal Assessment platform rear end, can meet cockpit rear portion into
Enter the requirement of cockpit, staircase 17 and staircase 18 can also be respectively placed in cockpit platform two sides, simulates left and right sides boarding side
Formula.
The 15 periphery spare interface of cockpit floor of cockpit Universal Assessment platform can add money to expand cooperation peace by platform
Fill the driving hatch cover of different helicopters.
The present invention greatly reduces the lead time of helicopter by using helicopter cockpit Universal Assessment platform, can be with
In design scheme, the general layout for developing simplation verification early period helicopter cockpit, and avoids each helicopter and develop
A case where cockpit platform need to be manufactured, largely save research fund.
Claims (7)
1. a kind of helicopter cockpit ergonomic Universal Assessment platform characterized by comprising
Cockpit floor (15), for installing seat, center console, instrument board and the top manipulation of helicopter cockpit
Platform；
Bottom support (16), is used to support the cockpit floor (15), and the bottom support (16) is height-adjustable
Structure；
Instrument board, by fascia supports frame (1) with being mounted on the cockpit (15) plate, the fascia supports frame (1)
It is highly adjustable；
Center console is mounted on the cockpit floor (15), the central control by center console supporting element (3)
Platform supporting element (3) height is adjustable；
Top console is mounted on the cockpit floor (15) by top console supporting element (6), the top manipulation
Platform supporting element (6) height is adjustable；
Seat, along cockpit central axes it is symmetrical there are two, bottom is mounted on the cockpit floor by horizontal slide rail
(15) on, the chair top of the seat is connected by rotating mechanism with leaning against.
2. helicopter cockpit ergonomic Universal Assessment platform as described in claim 1, which is characterized in that the bottom branch
Support member (16) includes bottom platform, the support rod upwardly extended by bottom platform, and cylinder is made in the other side connection of the support rod,
The other side for making cylinder is connected to the bottom on the cockpit floor.
3. helicopter cockpit ergonomic Universal Assessment platform as claimed in claim 2, which is characterized in that the bottom branch
Strut includes at least 3, is distributed in isosceles triangle.
4. helicopter cockpit ergonomic Universal Assessment platform as described in claim 1, which is characterized in that further include that a left side is driven
It sails bar and right control stick passes through horizontal slide rail along the center line that cockpit central axes are arranged symmetrically in two pilot sets
It is mounted on floor, control stick bottom is connect with force-feedback control box respectively.
5. helicopter cockpit ergonomic Universal Assessment platform as described in claim 1, which is characterized in that further include left total
Away from bar and right collective-pitch lever, it is installed in the left side of driver and copilot seat, is mounted on floor by horizontal slide rail, collective-pitch lever bottom
Portion is connect with force-feedback control box respectively.
6. helicopter cockpit ergonomic Universal Assessment platform as described in claim 1, which is characterized in that further include left side
Staircase (17) and right side staircase (18), connection ground and cockpit floor.
7. helicopter cockpit ergonomic Universal Assessment platform as described in claim 1, which is characterized in that further include left side
Pedal (13) and right side pedal (14) are symmetrical arranged, respectively with being mounted on cockpit by horizontal slide rail along cockpit central axes
On plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811361729.6A CN109533388B (en) | 2018-11-15 | 2018-11-15 | General evaluation platform for man-machine work efficiency of helicopter cockpit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811361729.6A CN109533388B (en) | 2018-11-15 | 2018-11-15 | General evaluation platform for man-machine work efficiency of helicopter cockpit |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109533388A true CN109533388A (en) | 2019-03-29 |
| CN109533388B CN109533388B (en) | 2020-10-02 |
Family
ID=65847844
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811361729.6A Active CN109533388B (en) | 2018-11-15 | 2018-11-15 | General evaluation platform for man-machine work efficiency of helicopter cockpit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109533388B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111932979A (en) * | 2019-05-13 | 2020-11-13 | 拉季埃-菲雅克有限责任公司 | Cockpit control part simulator |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1356675A (en) * | 2001-12-21 | 2002-07-03 | 北京航空航天大学 | Analog flight training equipment for manipulator of robot helicopter |
| CN102390544A (en) * | 2011-09-15 | 2012-03-28 | 北京航空航天大学 | Motion-linked cabin layout converting device for airplane simulator |
| CN102855410A (en) * | 2012-09-20 | 2013-01-02 | 上海品铭机械工程有限公司 | Method and system for evaluation of man-machine work efficiency of cabin simulation test bed |
| CN203910062U (en) * | 2014-02-27 | 2014-10-29 | 中国人民解放军空军第一航空学院 | Helicopter cabin base plate dynamic simulation platform |
| FR2991295B1 (en) * | 2012-06-04 | 2015-02-27 | Eurocopter France | AIRCRAFT WITH GREAT VISIBILITY |
| CN204759813U (en) * | 2015-06-15 | 2015-11-11 | 天津飞联科技有限公司 | Novel semi -closed emulation cockpit |
| CN105539854A (en) * | 2016-01-21 | 2016-05-04 | 南京航空航天大学 | Cockpit driving work efficiency designing and evaluating system platform |
| FR3005032B1 (en) * | 2013-04-26 | 2016-06-10 | Eurocopter France | SYMMETRICAL PILOTAGE STATION OF A GIRAVION HAVING SEATS POSSIBLE SIDE BY SIDE AND SIDE ACCESS DOORS |
| CN106126786A (en) * | 2016-06-17 | 2016-11-16 | 中国航空无线电电子研究所 | Cockpit display Human Machine Interface ergonomic's quantitative evaluating method |
| CN106599416A (en) * | 2016-11-30 | 2017-04-26 | 中国直升机设计研究所 | Man-machine work efficiency evaluation and optimization design method |
| CN107274747A (en) * | 2017-08-01 | 2017-10-20 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft cockpit ergonomic assessment system |
-
2018
- 2018-11-15 CN CN201811361729.6A patent/CN109533388B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1356675A (en) * | 2001-12-21 | 2002-07-03 | 北京航空航天大学 | Analog flight training equipment for manipulator of robot helicopter |
| CN102390544A (en) * | 2011-09-15 | 2012-03-28 | 北京航空航天大学 | Motion-linked cabin layout converting device for airplane simulator |
| FR2991295B1 (en) * | 2012-06-04 | 2015-02-27 | Eurocopter France | AIRCRAFT WITH GREAT VISIBILITY |
| CN102855410A (en) * | 2012-09-20 | 2013-01-02 | 上海品铭机械工程有限公司 | Method and system for evaluation of man-machine work efficiency of cabin simulation test bed |
| FR3005032B1 (en) * | 2013-04-26 | 2016-06-10 | Eurocopter France | SYMMETRICAL PILOTAGE STATION OF A GIRAVION HAVING SEATS POSSIBLE SIDE BY SIDE AND SIDE ACCESS DOORS |
| CN203910062U (en) * | 2014-02-27 | 2014-10-29 | 中国人民解放军空军第一航空学院 | Helicopter cabin base plate dynamic simulation platform |
| CN204759813U (en) * | 2015-06-15 | 2015-11-11 | 天津飞联科技有限公司 | Novel semi -closed emulation cockpit |
| CN105539854A (en) * | 2016-01-21 | 2016-05-04 | 南京航空航天大学 | Cockpit driving work efficiency designing and evaluating system platform |
| CN106126786A (en) * | 2016-06-17 | 2016-11-16 | 中国航空无线电电子研究所 | Cockpit display Human Machine Interface ergonomic's quantitative evaluating method |
| CN106599416A (en) * | 2016-11-30 | 2017-04-26 | 中国直升机设计研究所 | Man-machine work efficiency evaluation and optimization design method |
| CN107274747A (en) * | 2017-08-01 | 2017-10-20 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircraft cockpit ergonomic assessment system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111932979A (en) * | 2019-05-13 | 2020-11-13 | 拉季埃-菲雅克有限责任公司 | Cockpit control part simulator |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109533388B (en) | 2020-10-02 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5431569A (en) | Computer interactive motion simulator | |
| CA2960554C (en) | Motion and vibration cuing system | |
| US5669773A (en) | Realistic motion ride simulator | |
| US8364435B2 (en) | Device and a method for testing the design of a seat comprising a seat area, a backrest, and a headrest | |
| KR102042307B1 (en) | Simulator | |
| EP2541531B1 (en) | Motion seat for aircraft simulator | |
| EP1305785A2 (en) | Apparatus for producing or enhancing a perceived sensation of motion | |
| EP0784839B1 (en) | Method of manufacturing a motion simulator, and a motion simulator | |
| CN105403410A (en) | Vehicle man-machine subjective evaluation universal platform | |
| CN106043439A (en) | Carriage structure for vehicle test | |
| CN205300935U (en) | Man -machine subjective assessment common platform of vehicle | |
| CN109545063A (en) | A kind of verifying device of automobile human engineering | |
| CN109533388A (en) | A kind of helicopter cockpit ergonomic Universal Assessment platform | |
| US5513990A (en) | Realistic motion ride simulator | |
| CN111932979A (en) | Cockpit control part simulator | |
| KR101350267B1 (en) | Aircraft simulation system having arrangeable cockpit by length and breadth direction | |
| CN108152054A (en) | A kind of manipulation device analogue test platform of Agricultural Machinery Equipment driver's cabin | |
| CN105784391A (en) | Brake beam fatigue test stand | |
| CN210464892U (en) | Multifunctional driving seat display rack for simulating driving environment | |
| EP3693965B1 (en) | Compact movement simulator | |
| KR20080046719A (en) | Integrated aircraft scale and leveling apparatus and methods for use | |
| CN110782740B (en) | Miniature portable motion platform for simulating flight movement | |
| US1910655A (en) | Training apparatus for flying machine pilots | |
| KR100863070B1 (en) | Electronic control suspension system for car simulation education equipment | |
| CN215182564U (en) | Self-loading and unloading vehicle simulation training simulator |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |