CN105905315B - A kind of depopulated helicopter test monitoring control cabinet - Google Patents
A kind of depopulated helicopter test monitoring control cabinet Download PDFInfo
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- CN105905315B CN105905315B CN201610411972.9A CN201610411972A CN105905315B CN 105905315 B CN105905315 B CN 105905315B CN 201610411972 A CN201610411972 A CN 201610411972A CN 105905315 B CN105905315 B CN 105905315B
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- proof mirror
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Abstract
The invention discloses a kind of depopulated helicopter test monitoring control cabinet, including bottom plate, cockpit head, riser, breakage-proof mirror, table top and seat；Riser is fixed on bottom plate；Cockpit head includes arc and straight panel, and arc is connected with bottom plate, arc it is recessed one facing to riser, straight panel tilts towards riser direction；Seat is located on the bottom plate between cockpit head and riser, and table top one end is slidably connected on riser, and table top corresponds to seat setting, and height adjustment mechanism is provided between table top and riser；Breakage-proof mirror is located on the riser above table top, and the minute surface of breakage-proof mirror is higher than cockpit head towards seat, breakage-proof mirror；Breakage-proof mirror is turnover to be connected with riser, and angle adjusting mechanism is provided between breakage-proof mirror and riser.By the above-mentioned means, the present invention can improve the agility and security of the experiments such as the dangerous experimental enviroment monitoring and controlling such as helicopter, anti-fragment impact, all parts are coordinated reliably, and control cabinet is segmented, foldable assembly.
Description
Technical field
The present invention relates to test monitoring control cabinet field, more particularly to a kind of depopulated helicopter test monitoring control cabinet.
Background technology
Depopulated helicopter experiment is the main subject of depopulated helicopter development, production and factory inspection and acceptance.Depopulated helicopter is
Recent 10 Years in China enters a new industry in the stage that develops rapidly, and its test monitoring, control method, installations and facilities are continuous
Improve in improving.Flight test, ground engine test of the depopulated helicopter before user is delivered all are critically important experiments,
And the technical security of these experiments is also critically important.At present, the monitoring and controlling facility of domestic depopulated helicopter test site does not have
There is unified standard, using the method for temporal organization, though being completed task, organization work process is cumbersome, potential safety hazard
Can not thoroughly solve.Torn open in helicopter, depopulated helicopter, the ground run of general aircraft, conventional blasting method experiment, danger
Remove, the dangerous experimental enviroment occasion such as anti-fragment impact ensures the safety of tester frequently with security protection screen, but monitor,
Control device, plant facility are set, debug time is longer, influence bulk testing；Scene is participated in the experiment more than the people of technical staff 3, people with
Material object distance is big, and work coordination is complicated, and information conversion, transmission accuracy are poor；Site safety protecting screen arranges difficult, it is difficult to takes precautions against
Generation security incident.
The content of the invention
The present invention solves the technical problem of provide a kind of depopulated helicopter test monitoring control cabinet, it is possible to increase straight
The agility and security of the experiments such as the dangerous experimental enviroment monitoring and controllings such as the machine of liter, anti-fragment impact, all parts are coordinated reliably,
Detection control cabinet is segmented, foldable assembly.
In order to solve the above technical problems, one aspect of the present invention is：A kind of depopulated helicopter experiment is provided
Monitoring and controlling cabin, including：Bottom plate, cockpit head, riser, breakage-proof mirror, table top and seat；The riser is vertically fixed on bottom plate
On；The cockpit head includes the arc to link together and straight panel, arc are connected with bottom plate, and the one of arc fovea superior
Facing to riser, straight panel tilts towards riser direction；The seat is located on the bottom plate between cockpit head and riser, the table top
One end is slidably connected on riser, and table top corresponds to the seat and set, and height adjustment mechanism is provided between table top and riser；
The breakage-proof mirror is located on the riser above table top, and the minute surface of breakage-proof mirror is higher than cockpit head towards seat, breakage-proof mirror；Institute
State that breakage-proof mirror is turnover to be connected with riser, and angle adjusting mechanism is provided between breakage-proof mirror and riser.
Preferably, the riser is provided with the slide rail of vertical direction, and slide rail is provided with sliding block, and the table top is fixed on sliding block
On；The height adjustment mechanism includes regulation fixed block and regulating bolt, and regulation fixed block is fixed on the riser below slide rail,
Screw is provided with regulation fixed block, regulating bolt is against the lower surface of the table top through screw and regulating bolt.
Preferably, the side of the table top is fixed with communication antenna.
Preferably, the table top and seat are below the straight panel.
Preferably, one layer of breakage-proof pad pasting is posted on the breakage-proof mirror.
Preferably, the cockpit head is carbon fibre composite.
The beneficial effects of the invention are as follows：The present invention can improve the dangerous experimental enviroment monitoring such as helicopter, anti-fragment impact
The agility and security of the experiments such as control, all parts are coordinated reliable, and detection control cabinet is segmented, foldable assembly.
Brief description of the drawings
Fig. 1 is a kind of main structure diagram of the preferred embodiment of depopulated helicopter test monitoring control cabinet one of the present invention；
Structural representation when Fig. 2 is a kind of shown depopulated helicopter test monitoring control cabinet use state.
The mark of each part is as follows in accompanying drawing：1st, cockpit head；2nd, seat；3rd, breakage-proof mirror；4th, angle adjusting mechanism；5th, stand
Plate；6th, table top；7th, height adjustment mechanism；8th, bottom plate.
Embodiment
Presently preferred embodiments of the present invention is described in detail below in conjunction with the accompanying drawings, so that advantages and features of the invention energy
It is easier to be readily appreciated by one skilled in the art, apparent is clearly defined so as to be made to protection scope of the present invention.
Fig. 1 and Fig. 2 are referred to, the embodiment of the present invention includes：
A kind of depopulated helicopter test monitoring control cabinet, including：Bottom plate 8, cockpit are first 1, riser 5, breakage-proof mirror 3, table top 6
With seat 2, cockpit first 1 is carbon fibre composite, and one layer of breakage-proof pad pasting is posted on breakage-proof mirror 3.The riser 5 is vertically fixed
On bottom plate 8；The cockpit first 1 includes the arc to link together and straight panel, arc are connected with bottom plate, arc
The one of fovea superior tilts facing to riser, straight panel towards riser direction, and the inside of cockpit first 1 can place monitoring, control device, instrument
Device；The seat 2 is located on the bottom plate between cockpit first 1 and riser 5, and described one end of table top 6 is slidably connected to riser 5
On, the corresponding seat 2 of table top 6 is set, and height adjustment mechanism 7 is provided between table top 6 and riser 5, table top and seat are below
The straight panel；The breakage-proof mirror 3 is located on the riser above table top, and the minute surface of breakage-proof mirror 3 is towards seat, breakage-proof mirror 3
First higher than cockpit 1；The breakage-proof mirror 3 is turnover to be connected with riser 5, and angle is provided between breakage-proof mirror and riser
Governor motion 4, for adjusting the angle of breakage-proof mirror so that for depopulated helicopter ground debugging, take off and sighting distance in
Effective observation of flight.The riser is provided with the slide rail of vertical direction, and slide rail is provided with sliding block, and the table top is fixed on sliding block
On；The height adjustment mechanism includes regulation fixed block and regulating bolt, and regulation fixed block is fixed on the riser below slide rail,
Screw is provided with regulation fixed block, regulating bolt is against the lower surface of the table top through screw and regulating bolt, and table top is used for
Ground control station, flight monitoring instrument etc. are placed, the side of table top is fixed with communication antenna.
The present invention is closely monitored, controlled in experiment overall process, the technical staff that participates in the experiment, and the monitoring and controlling cabin is protected really
Hinder the personal safety of staff；Ensure field test data accurate delivery, coordinate with command system outside the venue, coordinate, according to finger
The accurate processing site problems of portion's instruction are waved, complete task.The present invention can improve the dangerous proving rings such as helicopter, anti-fragment impact
The agility and security of the experiments such as border monitoring and controlling, all parts are coordinated reliable, and detection control cabinet is segmented, foldable spelling
Dress.
Embodiments of the invention are the foregoing is only, are not intended to limit the scope of the invention, it is every to utilize this hair
The equivalent structure that bright specification and accompanying drawing content are made, or other related technical areas are directly or indirectly used in, similarly
It is included within the scope of the present invention.
Claims (4)
- A kind of 1. depopulated helicopter test monitoring control cabinet, it is characterised in that including：Bottom plate, cockpit head, riser, breakage-proof mirror, Table top and seat；The riser is vertically fixed on bottom plate；The cockpit head includes arc and the straight panel to link together, arc Shape plate is connected with bottom plate, and the one of arc fovea superior tilts facing to riser, straight panel towards riser direction；The seat is located at On bottom plate between cockpit head and riser, described table top one end is slidably connected on riser, and table top corresponds to the seat and set Put, height adjustment mechanism is provided between table top and riser；The breakage-proof mirror is located on the riser above table top, breakage-proof mirror Minute surface is higher than cockpit head towards seat, breakage-proof mirror；The breakage-proof mirror is turnover to be connected with riser, and breakage-proof mirror Angle adjusting mechanism is provided between riser；The riser is provided with the slide rail of vertical direction, and slide rail is provided with sliding block, described Face is fixed on sliding block；The height adjustment mechanism includes regulation fixed block and regulating bolt, and regulation fixed block is fixed on slide rail On the riser of lower section, adjust and screw is provided with fixed block, regulating bolt is against under the table top through screw and regulating bolt Surface；The table top and seat are below the straight panel.
- A kind of 2. depopulated helicopter test monitoring control cabinet according to claim 1, it is characterised in that：The side of the table top Face is fixed with communication antenna.
- A kind of 3. depopulated helicopter test monitoring control cabinet according to claim 1, it is characterised in that：The breakage-proof mirror On post one layer of breakage-proof pad pasting.
- A kind of 4. depopulated helicopter test monitoring control cabinet according to claim 1, it is characterised in that：The cockpit head is Carbon fibre composite.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610411972.9A CN105905315B (en) | 2016-06-14 | 2016-06-14 | A kind of depopulated helicopter test monitoring control cabinet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610411972.9A CN105905315B (en) | 2016-06-14 | 2016-06-14 | A kind of depopulated helicopter test monitoring control cabinet |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105905315A CN105905315A (en) | 2016-08-31 |
| CN105905315B true CN105905315B (en) | 2017-12-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610411972.9A Active CN105905315B (en) | 2016-06-14 | 2016-06-14 | A kind of depopulated helicopter test monitoring control cabinet |
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| Country | Link |
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Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109573096B (en) * | 2018-11-07 | 2021-12-24 | 中国航空救生研究所 | System-level ground comprehensive test facility for aviation protection and lifesaving equipment |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6195609B1 (en) * | 1993-09-07 | 2001-02-27 | Harold Robert Pilley | Method and system for the control and management of an airport |
| CN105314128A (en) * | 2015-11-04 | 2016-02-10 | 中国直升机设计研究所 | Hydraulic control system for helicopter ground integrated test bench |
| CN105644775A (en) * | 2016-03-16 | 2016-06-08 | 中国直升机设计研究所 | Flight test command and control system for unmanned helicopters |
| CN205891276U (en) * | 2016-06-14 | 2017-01-18 | 苏州环球集团飞行机器人有限公司 | Experimental monitor control cabin of unmanned helicopter |
-
2016
- 2016-06-14 CN CN201610411972.9A patent/CN105905315B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6195609B1 (en) * | 1993-09-07 | 2001-02-27 | Harold Robert Pilley | Method and system for the control and management of an airport |
| CN105314128A (en) * | 2015-11-04 | 2016-02-10 | 中国直升机设计研究所 | Hydraulic control system for helicopter ground integrated test bench |
| CN105644775A (en) * | 2016-03-16 | 2016-06-08 | 中国直升机设计研究所 | Flight test command and control system for unmanned helicopters |
| CN205891276U (en) * | 2016-06-14 | 2017-01-18 | 苏州环球集团飞行机器人有限公司 | Experimental monitor control cabin of unmanned helicopter |
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| Publication number | Publication date |
|---|---|
| CN105905315A (en) | 2016-08-31 |
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Address after: 215156 Jiangsu province Suzhou city Wuzhong District Town Village Road No. 6 light collection agency Applicant after: Suzhou Huanqiu elevator mechanical transmission Co.,Ltd. Address before: 215156 Jiangsu province Suzhou city Wuzhong District Town Stone Road No. 188 Applicant before: SUZHOU UNIVERSAL GROUP FLYING ROBOT Co.,Ltd. |
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Address after: Building 6, No. 188, Shizhong Road, Xukou Town, Wuzhong District, Suzhou City, Jiangsu Province, 215000 Patentee after: Suzhou Universal Intelligent System Co.,Ltd. Address before: No. 6 Guangcun Village Front Road, Cangshu Society, Mudu Town, Wuzhong District, Suzhou City, Jiangsu Province, 215156 Patentee before: Suzhou Huanqiu elevator mechanical transmission Co.,Ltd. |
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| TR01 | Transfer of patent right |
Effective date of registration: 20230627 Address after: 215000 No. 188 Shizhong Road, Xukou Town, Wuzhong District, Suzhou City, Jiangsu Province Patentee after: SUZHOU UNIVERSAL GROUP TECHNOLOGY CO.,LTD. Address before: Building 6, No. 188, Shizhong Road, Xukou Town, Wuzhong District, Suzhou City, Jiangsu Province, 215000 Patentee before: Suzhou Universal Intelligent System Co.,Ltd. |