CN107416225A - A kind of vehicle-mounted landing platform of aircraft - Google Patents
A kind of vehicle-mounted landing platform of aircraft Download PDFInfo
- Publication number
- CN107416225A CN107416225A CN201710667728.3A CN201710667728A CN107416225A CN 107416225 A CN107416225 A CN 107416225A CN 201710667728 A CN201710667728 A CN 201710667728A CN 107416225 A CN107416225 A CN 107416225A
- Authority
- CN
- China
- Prior art keywords
- supporting plate
- platform
- vehicle
- aircraft
- landing platform
- 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 claims description 41
- 238000010521 absorption reaction Methods 0.000 claims description 3
- 230000035515 penetration Effects 0.000 claims description 3
- 230000001105 regulatory effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000004073 vulcanization Methods 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000003490 calendering Methods 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
- B64F1/025—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using decelerating or arresting beds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R11/00—Arrangements for holding or mounting articles, not otherwise provided for
- B60R11/02—Arrangements for holding or mounting articles, not otherwise provided for for radio sets, television sets, telephones, or the like; Arrangement of controls thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R11/00—Arrangements for holding or mounting articles, not otherwise provided for
- B60R2011/0001—Arrangements for holding or mounting articles, not otherwise provided for characterised by position
- B60R2011/004—Arrangements for holding or mounting articles, not otherwise provided for characterised by position outside the vehicle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R11/00—Arrangements for holding or mounting articles, not otherwise provided for
- B60R2011/0042—Arrangements for holding or mounting articles, not otherwise provided for characterised by mounting means
- B60R2011/0049—Arrangements for holding or mounting articles, not otherwise provided for characterised by mounting means for non integrated articles
- B60R2011/005—Connection with the vehicle part
- B60R2011/0056—Connection with the vehicle part using suction cups
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R11/00—Arrangements for holding or mounting articles, not otherwise provided for
- B60R2011/0042—Arrangements for holding or mounting articles, not otherwise provided for characterised by mounting means
- B60R2011/008—Adjustable or movable supports
- B60R2011/0085—Adjustable or movable supports with adjustment by rotation in their operational position
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Transportation (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Abstract
The present invention relates to a kind of vehicle-mounted landing platform of aircraft, it is used for the platform of aircraft landing above roof including being arranged on, the levelling device for leveling platform is provided between platform and roof, described platform includes magnetic rubber board and nonmagnetic supporting plate, magnetic rubber board is removably arranged on supporting plate upper surface, and supporting plate is arranged on levelling device upper end.The upper end of expansion link of the present invention and the floating type connection of supporting plate, the length by adjusting multiple expansion links make supporting plate upper surface keep level；The upper surface of supporting plate sets magnetic rubber board, and aircraft landing gear is adsorbed when aircraft is dropped on platform for the first time, it is no longer departed from platform, so as to ensure that aircraft security lands.
Description
Technical field
The present invention relates to the landing platform of aircraft, the vehicle-mounted landing platform of particularly a kind of aircraft.
Background technology
Multi-axis aircraft is to have certain requirements to place in the landing stage, general to require more smooth, because in gradient
In the case of larger, sensor is difficult to the terrain clearance of accuracy of judgement on fuselage, and error is larger, easily damages aircraft, especially
It is the control of speed when influenceing landing, makes aircraft stall or at a high speed landing and damage, while requires there are enough safe areas,
In personnel or the intensive place of wagon flow, as station or rally place, flow of the people are big, it is difficult to control, it is difficult to find suitable place, rise
Risk is larger during drop.
In addition, when Multi-axis aircraft lands, one can be typically upspring after contacting to earth first to twice, then final landing, but this
Pick-up point is not consistent twice, and is at this moment than relatively hazardous not by remote control control.
The magnetic rubber board used in the present invention（Prior art, it can be commercially available）Also known as soft rubber, it is by rubber
In plus magnetic iron powder and various compounding ingredients by banburying, calendering vulcanization, withdraw from vulcanization and manufactured, one side can be made and cover magnetic or double
Cover magnetic in face.
The content of the invention
It is an object of the invention to provide a kind of vehicle-mounted landing platform of aircraft, to solve aircraft in densely populated place
Or wagon flow is intensive or takeoff and landing problem when gradient is larger.
In order to solve the above technical problems, the technical solution adopted in the present invention is：A kind of vehicle-mounted landing platform of aircraft,
It is used for the platform of aircraft landing above roof including being arranged on, the leveling for leveling platform is provided between platform and roof
Device, described platform includes magnetic rubber board and nonmagnetic supporting plate, magnetic rubber board are removably arranged on supporting plate
Upper surface, supporting plate are arranged on levelling device upper end.
Further, described levelling device is arranged on roof including at least three groups of telescoping mechanisms, the lower end of telescoping mechanism
On, upper end and the supporting plate floating connection of telescoping mechanism.
Further, described levelling device includes four groups of telescoping mechanisms.
Further, the telescoping mechanism includes coarse adjustment mechanism and micro-adjusting mechanism.
Further, the coarse adjustment mechanism of telescoping mechanism includes loop bar, portable stanchion and coarse adjustment bolt, and loop bar lower end is arranged on
On roof, portable stanchion is set in loop bar and coordinated with loop bar gap, and coarse adjustment bolt is along inside and outside loop bar radial penetration loop bar two
Side is simultaneously threadedly coupled with loop bar；Or/and；The micro-adjusting mechanism of telescoping mechanism includes portable stanchion and the fine setting being threadedly coupled vertically
Pillar, finely tune upper end and the supporting plate floating connection of pillar.
Further, the spherical shape in the upper end of telescoping mechanism and pass through floating support saddle and supporting plate floating connection, float branch
Seat lower end is provided with sleeve, and sleeve is set in outside the sphere of telescoping mechanism upper end and sleeve top surface and the sphere are tangent, branch of floating
Seat upper end is detachably connected with supporting plate, is also associated with being used for preventing floating support saddle and telescoping mechanism disengaging and steady on floating support saddle
The bracing means of the fixed landing platform.
Further, described bracing means includes bracing wire and vacuum cup, and bracing wire one end is detachably connected on floating branch
On seat, the bracing wire other end is adsorbed on roof by vacuum cup.
Further, described supporting plate is connected by the angle support frame for two bar shapeds be arrangeding in parallel with floating support saddle,
The both ends of angle support frame are respectively detachably connected with a floating support saddle.
Further, the rectangular shape in cross section of the angle support frame, described supporting plate are the one of rectangle and supporting plate
Parallel edges is connected on two angle support frames.
Further, angle support frame and floating support saddle grafting.
Beneficial effect：The upper end of telescoping mechanism of the present invention and the floating type connection of supporting plate, by adjusting multiple expansion links
Length makes supporting plate upper surface keep level；The upper surface of supporting plate sets magnetic rubber board, is dropped to for the first time in aircraft
Aircraft landing gear is adsorbed when on platform, it is no longer departed from platform, so as to ensure that aircraft security lands.
Brief description of the drawings
Fig. 1 is the dimensional structure diagram of the specific embodiment of the invention；
Fig. 2 is magnetic rubber board, supporting plate and angle support frame connection relationship diagram, where the dotted line signifies that bolt connection position；
Fig. 3 be expansion link and its with floating support saddle, the connection relationship diagram of supporting plate；
Fig. 4 is the dimensional structure diagram for the elastic force pin folder for coordinating the specific embodiment of the invention to use；
Marked in figure：1st, roof, 2, platform, 201, magnetic rubber board, 202, supporting plate, 3, telescoping mechanism, 301, loop bar, 302,
Portable stanchion, 303, coarse adjustment bolt, 304, fine setting pillar, 4, floating support saddle, 401, sleeve, 5, bracing means, 501, bracing wire,
502nd, vacuum cup, 6, angle support frame.
Embodiment
The present invention will be further described in detail with specific embodiment below in conjunction with the accompanying drawings.
As Figure 1-3, the portable car-mounted landing platform of a kind of Multi-axis aircraft, including be arranged on the top of roof 1 and use
In the platform 2 of aircraft landing, described platform 2 includes magnetic rubber board 201 and nonmagnetic supporting plate 202, magnetic rubber
Plate 201 is removably attachable to the upper surface of supporting plate 202；Supporting plate 202 uses the foamed board of two pieces of identical rectangles（It is such as existing
PVC foam plate in technology etc.）It is spliced, the long 1000mm of every piece of foamed board × wide 600mm, the support that two pieces of foamed boards are formed
202 long 1200mm of plate × wide 1000mm；Each long side of supporting plate 202（1200mm）Pass through bolt（To prevent foamed board from damaging,
A pad fitted bolt can be increased to use）It is fixedly connected on the angle support frame 6 of the rectangular shape of a strip and cross section
On（That is two angle support frames that two long sides correspondingly be arranged in parallel）, the both ends of angle support frame 6 respectively connect a floating support saddle 4
（That is corresponding four floating support saddles of two angle support frames）；Floating support saddle 4 includes a square bottom plate and two side plates, two
Side plate and a bottom plate three are vertical two-by-two, and the junction of each side plate and bottom plate is equipped with one for the insertion of angle support frame 6
For jack to realize angle support frame 6 and the grafting of floating support saddle 4, the lower end of floating support saddle 4 is provided with sleeve 401, each portion of floating support saddle 4
Divide welding or integrally casting；The lower section of each floating support saddle 4 is correspondingly arranged one group of telescoping mechanism 3（I.e. four floating support saddles are corresponding
Four group telescoping mechanisms）, described telescoping mechanism 3 includes loop bar 301, portable stanchion 302, coarse adjustment bolt 303 and fine setting pillar
304, loop bar 301 is arranged on roof 1, and portable stanchion 302 is set in loop bar 301 and coordinated with the gap of loop bar 301, coarse adjustment spiral shell
Bolt 303 is threadedly coupled along inside and outside the radial penetration loop bar 301 of loop bar 301 and with loop bar 301, loop bar 301, portable stanchion 302
The coarse adjustment mechanism of telescoping mechanism 3 is collectively formed with coarse adjustment bolt 303, portable stanchion 302 can be made along loop bar by unclamping coarse adjustment bolt 303
301 are radially slided and realize elongating or shortening for telescoping mechanism 3, and portable stanchion 302 and loop bar can be locked by screwing coarse adjustment bolt 303
301 relative position prevents both are relative from sliding, and finely tunes both lower end and the upper end edge of portable stanchion 302 of pillar 304 axial screws
Line connects the micro-adjusting mechanism for collectively forming telescoping mechanism 3, realizes that telescoping mechanism 3 elongates or shortens by rotary fine adjustment pillar 304
Fine setting, finely tune and be additionally provided with rotation hand wheel on pillar 304 in order to finely tune the rotation of pillar 304, the upper end of fine setting pillar 304 is in
Dome shape, the dome shape part be set in the sleeve 401 of the lower end of floating support saddle 4 and with the top surface of sleeve 401（Floating support saddle bottom
Face）Tangent, therefore floating support saddle 4 can realize the floating type of the upper end of telescoping mechanism 3 and supporting plate 202 around the rotation of 360 degree of sphere
Connection, four groups of telescoping mechanisms collectively form levelling device and are used for leveling supporting plate 202；It is also associated with using bracing wire on floating support saddle 4
501, the one end of bracing wire 501 is detachably connected on floating support saddle 4, needs to select according to during practical adjustments（Or adjustment）Bracing wire is grown
Degree, the other end of bracing wire 501 are adsorbed on roof 1 by vacuum cup 502, and bracing wire 501 forms bracing means with vacuum cup 502
5 are used to prevent floating support saddle 4 from telescoping mechanism 3 departing from while stabilization and reinforcement effect are played to whole landing platform.
Operation instruction：The use of the present invention needs the undercarriage of aircraft to be installed by magnetic absorption or on undercarriage
Can be by the device of magnetic absorption, for this, present invention also offers the accessory for coordinating the present invention to use, i.e., steel as shown in Figure 4
Elastic force pin folder；Before aircraft takeoff, portable landing platform is arranged on roof, leveling supporting plate 202, not installed now
Magnetic rubber board, upper elasticity pin folder is covered on aircraft landing gear, aircraft, which is placed in supporting plate 202, to take off；Take off
Fixed magnetic rubber slab 201 is laid in supporting plate 202 afterwards, when aircraft lands, is adsorbed aircraft landing gear using magnetic force
On magnetic rubber board 201, now elastic force pin folder and foamed board（That is supporting plate）Certain cushioning effect can be played, makes flight
Device initial contact magnetic rubber board 201 is completed safe falling, no longer upspring.
Above example is only the explanation made to the technology of the present invention design, any not depart from basic idea of the present invention
In the case of the replacement made or improvement all should include protection scope of the present invention.
Claims (10)
1. a kind of vehicle-mounted landing platform of aircraft, including it is arranged on roof（1）Top is used for the platform of aircraft landing（2）,
Platform（2）With roof（1）Between be provided with for leveling platform（2）Levelling device, it is characterised in that：Described platform（2）
Including magnetic rubber board（201）With nonmagnetic supporting plate（202）, magnetic rubber board（201）Removably it is arranged on supporting plate
（202）Upper surface, supporting plate（202）It is arranged on levelling device upper end.
A kind of 2. vehicle-mounted landing platform of aircraft according to claim 1, it is characterised in that：Described levelling device bag
Include at least three groups of telescoping mechanisms（3）, telescoping mechanism（3）Lower end be arranged on roof, telescoping mechanism（3）Upper end and supporting plate
（202）Floating connection.
A kind of 3. vehicle-mounted landing platform of aircraft according to claim 2, it is characterised in that：Described levelling device bag
Include four groups of telescoping mechanisms（3）.
A kind of 4. vehicle-mounted landing platform of aircraft according to claim 2, it is characterised in that：The telescoping mechanism（3）
Including coarse adjustment mechanism and micro-adjusting mechanism.
A kind of 5. vehicle-mounted landing platform of aircraft according to claim 4, it is characterised in that：Telescoping mechanism（3）It is thick
Regulating mechanism includes loop bar（301）, portable stanchion（302）With coarse adjustment bolt（303）, loop bar（301）Lower end is arranged on roof（1）
On, portable stanchion（302）It is set in loop bar（301）Interior and and loop bar（301）Gap coordinates, coarse adjustment bolt（303）Along loop bar
（301）Radial penetration loop bar（301）Inside and outside and and loop bar（301）Threaded connection；Or/and；Telescoping mechanism（3）Freqency fine adjustment machine
Structure includes the portable stanchion being threadedly coupled vertically（302）With fine setting pillar（304）, finely tune pillar（304）Upper end and support
Plate（202）Floating connection.
A kind of 6. vehicle-mounted landing platform of aircraft according to claim 2, it is characterised in that：Telescoping mechanism（3）It is upper
Hold spherical shape and pass through floating support saddle（4）With supporting plate（202）Floating connection, floating support saddle（4）Lower end is provided with sleeve
（401）, sleeve（401）It is set in telescoping mechanism（3）The sphere of upper end is outer and sleeve（401）Top surface and the sphere are tangent, float
Dynamic bearing（4）Upper end and supporting plate（202）It is detachably connected, floating support saddle（4）On be also associated be used for prevent floating support saddle（4）
With telescoping mechanism（3）Depart from and stablize the bracing means of the landing platform（5）.
A kind of 7. vehicle-mounted landing platform of aircraft according to claim 6, it is characterised in that：Described bracing means
（5）Including bracing wire（501）And vacuum cup（502）, bracing wire（501）One end is detachably connected on floating support saddle（4）On, bracing wire
（501）The other end passes through vacuum cup（502）Absorption is in roof（1）On.
A kind of 8. vehicle-mounted landing platform of aircraft according to claim 6, it is characterised in that：Described supporting plate
（202）By the angle support frame for two bar shapeds be arrangeding in parallel（6）With floating support saddle（4）Connection, angle support frame（6）Both ends it is each
With a floating support saddle（4）It is detachably connected.
A kind of 9. vehicle-mounted landing platform of aircraft according to claim 8, it is characterised in that：The angle support frame（6）
The rectangular shape in cross section, described supporting plate（202）For rectangle and supporting plate（202）A pair of parallel side be connected to two
Individual angle support frame（6）On.
A kind of 10. vehicle-mounted landing platform of aircraft according to claim 8, it is characterised in that：Angle support frame（6）With floating
Dynamic bearing（4）Grafting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710667728.3A CN107416225A (en) | 2017-08-07 | 2017-08-07 | A kind of vehicle-mounted landing platform of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710667728.3A CN107416225A (en) | 2017-08-07 | 2017-08-07 | A kind of vehicle-mounted landing platform of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107416225A true CN107416225A (en) | 2017-12-01 |
Family
ID=60436670
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710667728.3A Pending CN107416225A (en) | 2017-08-07 | 2017-08-07 | A kind of vehicle-mounted landing platform of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107416225A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111422140A (en) * | 2020-04-24 | 2020-07-17 | 新余国科特种装备有限公司 | Vehicle-mounted automatic leveling platform for meteorological radar |
| CN112089238A (en) * | 2020-08-14 | 2020-12-18 | 安徽附利整体家居有限公司 | Stable-state log composite board and panel furniture |
| CN112432575A (en) * | 2021-01-28 | 2021-03-02 | 纽科伦（新乡）起重机有限公司 | Method and device for detecting precision of gourd drum |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007052277A1 (en) * | 2006-11-08 | 2009-11-05 | Paley, Anatoly, Prof. dRF | Method for emergency landing of aircraft, involves landing aircraft on emergency carriage with fully or partly retracted appropriate chassis in autonomous, motorized and remote-controlled manner |
| CN203384604U (en) * | 2013-05-30 | 2014-01-08 | 中国电子科技集团公司第二十七研究所 | Tripod for servo turntable |
| CN104295869A (en) * | 2014-08-15 | 2015-01-21 | 湖北三江航天万峰科技发展有限公司 | Tripod capable of being fast leveled |
| CN104527991A (en) * | 2014-11-11 | 2015-04-22 | 国网辽宁省电力有限公司检修分公司 | Portable dust preventive lifting platform for UAV (unmanned aerial vehicle) in mountainous region |
| CN204477633U (en) * | 2015-03-09 | 2015-07-15 | 浙江海洋学院 | Integral type projector mount |
| CN106379550A (en) * | 2016-06-15 | 2017-02-08 | 珠海市磐石电子科技有限公司 | Take-off and landing platform for aircraft |
| CN106500590A (en) * | 2016-12-15 | 2017-03-15 | 宁夏共享模具有限公司 | A kind of laser interferometer interferoscope adjusts platform |
| CN107010241A (en) * | 2017-05-27 | 2017-08-04 | 辛亚行 | A kind of vehicle-mounted unmanned aerial vehicle landing platform |
| CN207173993U (en) * | 2017-08-07 | 2018-04-03 | 洛阳理工学院 | A kind of vehicle-mounted landing platform of aircraft |
-
2017
- 2017-08-07 CN CN201710667728.3A patent/CN107416225A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007052277A1 (en) * | 2006-11-08 | 2009-11-05 | Paley, Anatoly, Prof. dRF | Method for emergency landing of aircraft, involves landing aircraft on emergency carriage with fully or partly retracted appropriate chassis in autonomous, motorized and remote-controlled manner |
| CN203384604U (en) * | 2013-05-30 | 2014-01-08 | 中国电子科技集团公司第二十七研究所 | Tripod for servo turntable |
| CN104295869A (en) * | 2014-08-15 | 2015-01-21 | 湖北三江航天万峰科技发展有限公司 | Tripod capable of being fast leveled |
| CN104527991A (en) * | 2014-11-11 | 2015-04-22 | 国网辽宁省电力有限公司检修分公司 | Portable dust preventive lifting platform for UAV (unmanned aerial vehicle) in mountainous region |
| CN204477633U (en) * | 2015-03-09 | 2015-07-15 | 浙江海洋学院 | Integral type projector mount |
| CN106379550A (en) * | 2016-06-15 | 2017-02-08 | 珠海市磐石电子科技有限公司 | Take-off and landing platform for aircraft |
| CN106500590A (en) * | 2016-12-15 | 2017-03-15 | 宁夏共享模具有限公司 | A kind of laser interferometer interferoscope adjusts platform |
| CN107010241A (en) * | 2017-05-27 | 2017-08-04 | 辛亚行 | A kind of vehicle-mounted unmanned aerial vehicle landing platform |
| CN207173993U (en) * | 2017-08-07 | 2018-04-03 | 洛阳理工学院 | A kind of vehicle-mounted landing platform of aircraft |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111422140A (en) * | 2020-04-24 | 2020-07-17 | 新余国科特种装备有限公司 | Vehicle-mounted automatic leveling platform for meteorological radar |
| CN112089238A (en) * | 2020-08-14 | 2020-12-18 | 安徽附利整体家居有限公司 | Stable-state log composite board and panel furniture |
| CN112432575A (en) * | 2021-01-28 | 2021-03-02 | 纽科伦（新乡）起重机有限公司 | Method and device for detecting precision of gourd drum |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107416225A (en) | A kind of vehicle-mounted landing platform of aircraft | |
| CN205098463U (en) | Full topography helicopter undercarriage | |
| CN106005360B (en) | SUAV can be opened and closed hatch door load lift mechanism | |
| CN109311525A (en) | For personnel and equipment to be transferred to the channel of second device from first device | |
| CN104401502B (en) | A kind of large-scale undercarriage flexible installing with deposit dual-purpose apparatus | |
| CN108263924A (en) | A kind of elevator shock-absorbing device | |
| CN207173993U (en) | A kind of vehicle-mounted landing platform of aircraft | |
| CN206050021U (en) | A kind of support peculiar to vessel | |
| CN108190718A (en) | A kind of multi-functional ship combination hydraulic A type frame | |
| CN104029824B (en) | Large thruster arranges the posture adjustment assembly method bottom spacecraft | |
| CN106976545B (en) | A kind of captive balloon utricule ground lifting apparatus | |
| CN205941197U (en) | Multi -functional technology bogie of quiet pressure test of rail vehicle automobile body | |
| CN106460368A (en) | Guardrail for construction equipment | |
| CN101520364A (en) | Inverted cup-type drop test bed cradle | |
| US20150183622A1 (en) | Crane | |
| CN207659004U (en) | A kind of boss rod enters cabin installation ancillary equipment | |
| CN208345719U (en) | A kind of intelligence airport loading/unloading platform vehicle | |
| CN205292854U (en) | Jumbo mobile device | |
| CN108058804A (en) | A kind of plug-in helicopter safeguards pedal | |
| CN106364537A (en) | Adjustable underwater robot bracket for scientific investigation vessel | |
| CN206019816U (en) | New automobile weighing device for planar movement | |
| CN110203122A (en) | A kind of radome of fighter dismounting unwheeling | |
| CN206943718U (en) | Lifting pedestal | |
| CN206766077U (en) | A kind of car door mounting bracket carrier | |
| CN107025822A (en) | A kind of passenger train gear box teaching training apparatus |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171201 |
|
| RJ01 | Rejection of invention patent application after publication |