CN108190037A - A kind of electronic flight data bag support of adjustable-angle and height - Google Patents
A kind of electronic flight data bag support of adjustable-angle and height Download PDFInfo
- Publication number
- CN108190037A CN108190037A CN201810029464.3A CN201810029464A CN108190037A CN 108190037 A CN108190037 A CN 108190037A CN 201810029464 A CN201810029464 A CN 201810029464A CN 108190037 A CN108190037 A CN 108190037A
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- China
- Prior art keywords
- flight data
- electronic flight
- angle
- support column
- data bag
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 17
- 230000000712 assembly Effects 0.000 claims abstract description 7
- 238000000429 assembly Methods 0.000 claims abstract description 7
- 210000000078 claw Anatomy 0.000 claims description 24
- 230000000694 effects Effects 0.000 claims description 8
- 238000010276 construction Methods 0.000 claims description 4
- 238000003032 molecular docking Methods 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 7
- 230000000295 complement effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 241001269238 Data Species 0.000 description 1
- 241000826860 Trapezium Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M13/00—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
- F16M13/02—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of adjustable-angles and the electronic flight data bag support of height, including gripper frame, support column and pedestal, gripper frame is equipped with clamp assemblies, the clamp assemblies include panel, geometrical clamp gripping member is equipped on the upside of panel, downside is equipped with movable clamping device, pedestal is equipped with bottom plate, connected unit is equipped on the upside of bottom plate, snapping plate and connected unit snapping, compensation block are mounted between connected unit and snapping plate, and support column is made of two symmetrical semicylinders, support column upper end is equipped with angle regulator, and lower end is equipped with height adjustment device.The present invention can be accustomed to being adjusted flexibly with vision coverage area according to pilot the deflection angle and height of electronic flight data packet, have Fast Installation, disassembling function, be applicable in and used with the electronic flight data packet of various models.
Description
Technical field
The present invention relates to a kind of stent, the electronic flight data bag support of more particularly to a kind of adjustable-angle and height.
Background technology
Electronic flight data packet（EFB）It is a kind of pilot flying assistant tools, for showing various aeronautical datas, carries out
Calculating and inspection or the calculating for performing some basic aeroplane performance data when various mission phases prepare.These functions exist
It is traditionally to be completed by the way of paper delivery medium reference paper, the use of electronic flight data packet is situated between instead of numerous and diverse paper
Matter file is outstanding cockpit flight auxiliary tool.Electronic flight data packet, which needs to be mounted on using stent when in use, to be driven
Position is sailed nearby so that driver uses at any time.
Chinese invention patent：A kind of aircraft cockpit electronic flight bag fixed frame（Application number：2016203090165）,
The patent solve the problems, such as electronic equipment installation after adjust it is dumb, using difficulty.But aircraft take off, land and
It in the case of encountering airwaves, easily vibrates, therefore the flight packet fixed frame of above-mentioned patent easily loosens, and causes
Its stability is bad, and the above-mentioned flight packet fixed frame for stating patent, in dismounting, can only dismantle fixed seat, and dismount all
It is extremely inconvenient.In addition, electronic flight data packet according to function difference there are many grade and model, it is big between each model
Small and thickness has difference, for ease of use, stent is needed to have the function that clamping dimension is adjusted flexibly.Therefore its is easy to use
Property also needs to further improve.
Invention content
For the foregoing reasons, it is an object of the invention to：Overcome disadvantages mentioned above, count and be further improved, providing one kind can
Regulate and control the electronic flight data bag support of angle and height, can be accustomed to according to pilot and deflection angle is adjusted flexibly in vision coverage area
Degree and height, have Fast Installation, disassembling function, are applicable in and are used with the electronic flight data packet of various models.
To achieve the above object, the technical scheme is that：
A kind of electronic flight data bag support of adjustable-angle and height, including gripper frame, support column and pedestal, the support
Column both ends connect gripper frame and pedestal respectively.Gripper frame is equipped with clamp assemblies, and the clamp assemblies include panel, panel upside
Equipped with geometrical clamp gripping member, downside is equipped with movable clamping device, and the activity clamping device includes one group of guide groove and be sleeved on to lead
Telescopic rod into slot, the guide groove are mutually inclined arranged symmetrically, and guide groove is connect with telescopic rod by tension spring, described flexible
The tail end of bar is equipped with clamping apex angle, and the geometrical clamp gripping member and clamping apex angle are bathtub construction, and slot inner underside is equipped with thickness
Adjust slope.
Pedestal is equipped with bottom plate, and connected unit, snapping plate and connected unit snapping are equipped on the upside of bottom plate, and compensation block is mounted on connection
It is circumferentially distributed on the upside of the connected unit to have at least three arc-shaped claws, claw inside length direction between platform and snapping plate
Dovetail groove is provided with, claw middle inside short transverse is provided with card hole, and the outer ring of snapping plate is circumferentially distributed connect corresponding with claw
Head, connector outer end middle part are equipped with the convex block docked with card hole, and the compensation block is circular ring shape, and the downside of compensation block is equipped at least three
A spring.
The support column is made of two symmetrical semicylinders, and the upper end of support column is equipped at least one spherical cavity,
Lower end is equipped with cylindrical cavity, and convex block is equipped at the top of cylindrical cavity cavity wall, radially pass through aperture, through hole are provided in the middle part of support column
Place connects two semicylinders equipped with locking device, and support column upper end is equipped with angle regulator, angle regulator bottom
Equipped at least one bulb, bulb is placed in spherical cavity, and support column lower end is equipped with height adjustment device, height adjustment device
Upper end is horizontally installed with cylindrical turntable, and turntable is placed in cylindrical cavity, and the turntable upper center is radially set
There is gear adjustable plate, the gear adjustable plate is sector, and the both sides of gear adjustable plate are equipped with several grooves, institute along radial direction
The top for stating angle regulator is connect with clamping frame bottom, and the bottom end of height adjustment device is connect with snapping plate.
Above technical scheme is described further below：
Further, the height of the connector and claw ratio is 1:1.2~1.6.
Further, the angle between the guide groove is 30 °~60 °.
Further, the slope surface that the thickness adjusts slope is arc.
Further, the locking device includes bolt and knob, is provided with threaded hole on knob, bolt pass through through hole with
Knob thread connects, and at least one gasket is equipped between knob and through hole.
Further, the cavity wall opening of the spherical cavity and cylindrical cavity is provided with the notch of arc.
Further, groove number of the gear adjustable plate per side is 2~12, adjacent grooves（234）Between angle
It is 5 °~60 °.
Further, connected unit upper end inner wall is equipped with a circle limit round table, and the diameter of compensation block upper end is less than limiting
The internal diameter of round platform, compensation block lower end diameter is more than the internal diameter of limit round table, less than the internal diameter of connected unit.
Further, one end of the bottom plate is equipped with pinboard, and the pinboard tilts down setting, bottom plate and pinboard
Angle be 30 °~150 °.
As a result of said program, the beneficial effects of the present invention are：
1. applicability is wide, setting activity clamping device and geometrical clamp gripping member, it is capable of length, the width range of flexible modulation clamping；
Thickness is set to adjust slope, is adjusted electronic flight data packet to thickness using the blessing power of movable clamping device and geometrical clamp gripping member
Certain altitude is boosted on the upside of slope, so as in the electronic flight data packet for stepping up different-thickness.Width, length suitable for different model
The different electronic flight data packet of degree, thickness without frequently replacing stent according to model, provides conveniently for operator.
2. regulation and control are flexible, easy to use.Support column is equipped with angle regulator and height adjustment device, can be according to driving
Deflection angle and bearing height is adjusted flexibly in vision coverage area, the operating habit multi-angle for the person of sailing；Locking device is additionally provided with, is adjusted
The angle and height adjusted can be locked by locking device after height and angle, avoid the backward shift that jolts or touch, improve
Ease of use.
3. pedestal is equipped with compensating plate, vibrations can be caused taking off, landing and encountering airwaves and jolted
When, it prevents vibrations from causing noise and colliding with, improves performance.
4. each section of the present invention is detachable connection structure, it is easy for installation and removal.
5. structure is simplified, installation is simple, easy to use.It occupies little space, does not influence driver's work, from heavy and light, be suitble to
Aviation cockpit uses.
Description of the drawings
Fig. 1 is the overall structure diagram of one embodiment of the present invention.
Fig. 2 is the whole main structure diagram of one embodiment of the present invention.
Fig. 3 is the structure diagram of gripper frame in one embodiment of the present invention.
Fig. 4 is the main structure diagram of gripper frame in one embodiment of the present invention.
Fig. 5 is the structure diagram of support column in one embodiment of the present invention.
Fig. 6 is the semi-cylindrical structure schematic diagram of support column in one embodiment of the present invention.
Fig. 7 is the structure diagram of pedestal in one embodiment of the present invention.
Fig. 8 is the sectional view of pedestal in one embodiment of the present invention.
Reference numeral：
1- gripper frames, 11- panels, 12- geometrical clamp gripping members, 121- thickness adjusting slope, 13- activity clamping devices, 131- guide grooves,
132- telescopic rods, 133- clamping apex angles, 135- tension springs.
2- support columns, 221- semicylinders, 222- spherical cavities, 223- cylindrical cavities, 224- through holes, 225- convex blocks,
226- notches, 21- angle regulators, 211- bulbs, 23- height adjustment device, 232- turntables, 233- gear adjustable plates,
234- grooves, 24- locking devices, 241- bolts, 242- knobs, 243- gaskets.
3- pedestals, 31- connected units, 311- claws, 312- dovetail grooves, 313- card holes, 32- compensation blocks, 321- springs, 33-
Snapping plate, 331- connectors, 332- convex blocks, 34- bottom plates, 314- limit round tables, 341- pinboards.
Specific embodiment
More detailed description is done to embodiments of the present invention below in conjunction with attached drawing and reference numeral, makes to be familiar with this field
Technology people can implement according to this after this specification is studied carefully.
Embodiment：Referring to attached drawing 1, attached drawing 2, the electronic flight data bag support of a kind of adjustable-angle and height, including
Gripper frame 1, support column 2 and pedestal 3,2 both ends of support column connect gripper frame 1 and pedestal 3 respectively.Pedestal 3 is mounted on aircraft
Near cockpit control panel, gripper frame 1 is used to grip electronic flight data packet.
Referring to attached drawing 3, gripper frame 1 is equipped with clamp assemblies, and the clamp assemblies include panel 11, and 11 upside of panel is equipped with
Geometrical clamp gripping member 12, downside are equipped with movable clamping device 13, and the activity clamping device 13 includes one group of guide groove 131 and suit
Telescopic rod 132 in guide groove 131, telescopic rod 132 can be extended or retracted out of guide groove 131.Guide groove 131 is length side
To the strip plate equipped with rectangle or arc-shaped slot, telescopic rod 132 is accommodated in slot, the notch of guide groove 131 is upward, and passes through fastening
Part is fixed on 1 downside of panel.
The guide groove 131 be mutually inclined it is arranged symmetrically, so as to enable two telescopic rods 132 outward diversity elongation,
So as to try out in the electronic flight data packet of different length, width.In the present embodiment, the folder between the guide groove 131
Angle is 30 °~60 °.Telescopic rod 132 grows 1~10 centimetre, and so as to make telescopic rod 132, radioactivity extends in a certain range.It is preferred that
, the angle between guide groove 131 is 45 °.
Guide groove 131 is connect with telescopic rod 132 by tension spring 135, and extension bolt is equipped in guide groove 131 and telescopic rod 132,
The both ends of tension spring 135 connect guide groove 131 and the extension bolt on telescopic rod 132 respectively, so as to connect guide groove 131 and telescopic rod
132.Tension spring 135 draws telescopic rod 132 into guide groove 131, for providing pulling force so as to clamp electronic flight data packet.Separately
Outside, after use, the pulling force of tension spring 135 can withdraw telescopic rod 132 in guide groove 131, pushed away manually without operator and put receipts
It receives, increases ease of use.
The tail end of the telescopic rod 132 is equipped with clamping apex angle 133, and the geometrical clamp gripping member 12 and clamping apex angle 133 are
Bathtub construction, the side plate two corners of electronic flight data packet are stuck in the slot of clamping apex angle 133, in the middle part of the side plate of opposite side
It is stuck in the slot of geometrical clamp gripping member 12, forms the triangle clamping frame inwardly tightened, electronic flight data packet is fixed on frame
In frame.
Referring to attached drawing 4, geometrical clamp gripping member 12 and clamping 133 slot inner underside of apex angle are equipped with thickness and adjust slope 121, thickness tune
Section slope 121 is the domatic structure that bottom gradually rises to top.When clamped electronic flight data packet thickness is less than the height of slot
When spending, the blessing power of geometrical clamp gripping member 12 and movable clamping device 13 can adjust slope 121 by electronic flight data by thickness
Packet is lifted up certain altitude, is stuck in thickness and adjusts between 121 slope wall of slope and slot upper wall.
Thickness adjusts the optional linear type of slope surface or arc on slope 121.Preferably, the slope surface on the thickness adjusting slope 121 is
Arc, the slope surface of the arc frictional force when lifting electronic flight data packet is small, and contact surface is gentler, electronic flight number not easy to wear
According to bound edge frame.
Preferably, data line or charging wire, the geometrical clamp gripping member 12 can be easily connected when in use for convenience
On be provided with jack, facilitate leak out electronic flight data packet charging socket or receiver J-Horner.
Preferably, in order to make whole device lighter and handier portable, lightening hole or lightening grooves are provided on the gripper frame 1.
Preferably, it in order to strengthen the structure of gripper frame 1, prevents from deforming, be broken, increase service life, the folder of the present embodiment
It holds 1 downside of frame and is equipped with several reinforcing ribs.
Referring to attached drawing 7, pedestal 3 is equipped with bottom plate 34, and bottom plate 34 is fixed on cockpit operating surface pallet, 34 upside of bottom plate
Equipped with connected unit 31, snapping plate 33 and 31 snapping of connected unit, the upside of snapping plate 33 connect support column 2, and compensation block 32 is mounted on
Between connected unit 31 and snapping plate 33.
31 upside of connected unit is circumferentially distributed at least three arc-shaped claws 311,311 inside length direction of claw
Dovetail groove 312 is provided with, 311 middle inside short transverse of claw is provided with card hole 313, and the card hole 313 is obliquely installed, card hole 313
Axis it is parallel with the inclined-plane of dovetail groove 312, the cross section of card hole 313 is semi-circular hole or rectangular opening.
Preferably, the shape of connected unit 31 is circular ring shape.
Preferably, the inclination angle of the dovetail groove 12 is 10 °~80 °.
The outer ring of snapping plate 33 is circumferentially distributed have with 311 corresponding connector 331 of claw, under the section configuration of connector 331 is
The narrow trapezium structure in the wide upper end in end, 312 complementary structure of connector 331 and dovetail groove can be stuck in dovetail groove 312 so as to junction button
Fishplate bar 33 and connected unit 31.The convex block 332 docked with card hole 313, convex block 332 and card hole 313 are equipped in the middle part of 331 outer end of connector
Complementary structure.
Further, the height ratio of the connector 331 and claw 311 is 1:1.2~1.6, this difference in height can make connector
331 in claw 311 there are up and down space, it is easy to disassemble：Snapping plate 33 is pressed downward, connector 331 is driven to be displaced downwardly to
The bottom of dovetail groove 312 increases the gap between connector 331 and dovetail groove 312, and turn buckle fishplate bar 33 screws out connector 331
Dovetail groove 312 realizes dismounting.
Preferably, the height ratio of connector 331 and claw 311 is 1:1.5.
Preferably, the number of the claw 311 and connector 331 is 4.
The compensation block 32 is circular ring shape, and the downside of compensation block 32 is equipped at least three springs 321, and spring 321 can make
Compensation block 32 adjusts height according to pressure size, then while encountering vibrations is capable of providing cushion effect, the compensation block 32 to be round or
Circular ring shape, in order to mitigate dead weight, preferably circular ring shape.When snapping plate 33 and 31 snapping of connected unit, under the effect of spring 321, mend
It can be that snapping plate 33 provides upward thrust to repay block 32, reduce the gap between connector 331 and dovetail groove 312, make snapping plate
33 consolidate with 31 snapping of connected unit.
During installation, first compensation block 32 is mounted in connected unit 31, snapping plate 33 is placed on 31 upside of connected unit, snapping
The bottom surface of plate 33 is contacted with compensation block 32, adjusts the gap location that snapping plate 33 makes connector 331 be located at 31 claw 311 of connected unit, to
Lower Pressing fastener fishplate bar 33 drives 32 compressed spring 321 of compensation block to move down, axial when connector 331 touches 31 end face of connected unit
Turn buckle fishplate bar 33 will be in the dovetail groove 312 of 331 precession claw 311 of connector.Since connector 331 and claw 311 have difference in height, because
This, connector 331 is located at the bottom of dovetail groove 312 at this time, has larger gap between dovetail groove 312 and claw 311.When connector 331
Stopping Pressing fastener fishplate bar 33 when the convex block 332 of front end is rotated to card hole 313, the recovery of spring 321 moves up compensation block 32,
The lift upwards of snapping plate 33 is driven, connector 331 is moved up is decreased to gapless with the gap of claw 311, realizes clamping.By snapping plate 33
It presses down on, reversely connector 331 out of dovetail groove 312 is screwed out, dismounting can be realized.
One end of bottom plate 34 described in the present embodiment is equipped with pinboard 341, and the pinboard 341 tilts down setting, bottom
Plate 34 and the angle of pinboard 341 are 30 °~150 °.Pinboard 341 makes peace for being connected with the operation panel of corner, gap
Fill more stable, more fitting airplane operation panel.
Further, referring to attached drawing 8,31 upper end inner wall of connected unit is equipped with a circle limit round table 314,32 upper end of compensation block
Diameter is less than the internal diameter of limit round table 314, and 32 upper end of compensation block is enable to stretch out limit round table 314 and is contacted with snapping plate 33, mends
The internal diameter that 32 lower end diameter of block is more than limit round table 314 is repaid, less than the internal diameter of connected unit 31.Limit round table 314 can will compensate
Block 32 is limited in 314 downside to the space of bottom plate 34 of limit round table of 31 inner ring of connected unit, can prevent dismounting snapping plate 33
Afterwards, compensation block 32 pops up.
Referring to attached drawing 5, attached drawing 6, the support column 2 is made of two symmetrical semicylinders 221, two semicylinders
221 combinations form a cylindrical support column 2, and the upper end of support column 2 is equipped at least one spherical cavity 222, and lower end is set
There is cylindrical cavity 223, convex block 225 is equipped at the top of 23 cavity wall of cylindrical cavity, 2 middle part of support column is radially provided with pass through aperture 224, passes through
It perforates and connects two semicylinders 221 equipped with locking device 24 at 24.
2 upper end of support column is equipped with angle regulator 21, and 21 bottom of angle regulator is equipped at least one bulb 211,
Bulb 211 is placed in spherical cavity 222, and bulb 211 is used for divertical motion, realizes angular adjustment, and using ball, 211 rotations are smooth,
Frictional force is small.
2 lower end of support column is equipped with height adjustment device 23, and the upper end of height adjustment device 23 is horizontally installed with cylinder
Turntable 232, turntable 232 are placed in cylindrical cavity 23, and 232 upper center of turntable is radially provided with gear adjustable plate
233, turntable 232 provides rotating fulcrum for gear adjustable plate 233, and the gear adjusts 233 as sector, gear adjustable plate 233
Both sides along radial direction be equipped with several grooves 234.
It is more smooth in order to adjust gear, service life is improved, the groove 234 is semi-circular groove, and convex block 225 is semicircle
Shape column.
Preferably, 234 numbers of groove of gear adjustable plate 233 per side are 2~12, the folder between adjacent grooves 234
Angle is 5 °~60 °.Therefore, gear adjustable plate 233 can provide 30 °~180 °, the rotation angle per 5 °~15 ° of gear, pass through tune
Height adjustment device 23 is saved, the angle between support column 22 and pedestal can reach 0 °~180 °, therefore can be by adjusting height
Regulating device 23 adjusts the top of support column 2 to the height between pedestal 3.
Most preferably, 34 numbers of groove of gear adjustable plate 233 per side are 8, and the angle between adjacent grooves 34 is
20°。
The top of the angle regulator 21 is connect with 1 bottom of gripper frame, the bottom end of height adjustment device 23 and snapping
Plate 33 connects.
Locking device 24 includes bolt 241 and knob 242 in the present embodiment, and threaded hole, bolt 241 are provided on knob 242
It is threadedly coupled across through hole 224 with knob 242, locking device 24 being capable of lock adjustment good support angle and bearing height.
First locking device 24 is unscrewed during use, spherical cavity 222 and cylindrical cavity 223 between two semicylinders 221 is made to form one
Gap is determined convenient for adjusting angle and height, and angle tightens locking device 24 after adjusting, makes spherical cavity 22 and cylindrical cavity 223
It clamps bulb 211 and gear adjustable plate 233 realizes that angle and height lock.
Meanwhile locking device 24 is additionally operable to mount and dismount entire component, is used as connection fixing device, locking of dismantling
Device 24 is two semicylinders 21 of Detachable.At least one gasket is equipped in the present embodiment between knob 242 and through hole 224
243, gasket 243 is used for increasing friction force, prevents knob 242 from loosening.
The cavity wall opening of the spherical cavity 222 and cylindrical cavity 223 is provided with the notch 226 of arc, 226 energy of notch
The adjusting space of 21 bigger of angle regulator is enough provided, avoids adjusting and interfere, while there is certain elastic buffer power, absorb
Shake stress.
Conduct oneself with dignity to mitigate, the semicylinder 221 in the present embodiment is hollow-core construction.Preferably, mitigating the same of dead weight
When, it in order to ensure integral strength, is unlikely to deform, the thickness of semicylinder 221 is 0.5~1.5 centimetre.
In use, first two apex angles of electronic flight data packet a side are stuck in clamping apex angle 133, push out
Telescopic rod 132 is pulled out, enters electronic flight data packet opposite side checkpost in geometrical clamp gripping member 12 after reserving distance enough.Unscrew lock
Tight device 24 rotates support column 2 along 232 axis direction of turntable, and different angle is adjusted so as to adjust according to gear adjustable plate 233
The inclination angle between support column 2 and control panel is saved, inclination angle is smaller, and distance of the gripper frame 1 away from panel is shorter, and height is lower,
It is on the contrary then higher.Then rotating ballhead adjusts the deflection angle of electronic flight data packet.Locking device 24 is tightened after adjustment,
The gap between spherical cavity 222 and cylindrical cavity 223 reduces at this time, and bulb 211 and turntable 232 are clamped, so as to fixed angles
Degree and height.
When needing to dismantle a part of stent temporarily, can be incited somebody to action by way of unscrewing locking device 24 and extracting bulb 211
Gripper frame 1 detaches, can also turn buckle fishplate bar 33 snapping plate 33 is detached support column 2 with the mode that connected unit 31 detaches.
In the description of the present invention, it is to be understood that term " " center ", " length ", " thickness ", " on ", " under ", " perpendicular
Directly ", the orientation of the instructions such as " level ", " bottom ", " interior ", " outer ", " circumferential direction " or position relationship be based on orientation shown in the drawings or
Position relationship is for only for ease of description and simplifies description rather than instruction or to imply that signified device must have specific
Orientation, with specific azimuth configuration and operation, therefore be not considered as limiting the invention.
The present embodiment is exemplarily described above in conjunction with attached drawing, present invention specific implementation is not by aforesaid way
Limitation, as long as employing the improvement or not improved of the various unsubstantialities of inventive concept and technical scheme of the present invention progress
The design of the present invention and technical solution are directly applied into other occasions, within protection scope of the present invention.
Claims (9)
1. a kind of electronic flight data bag support of adjustable-angle and height, including gripper frame（1）, support column（2）And pedestal
（3）, the support column（2）Both ends connect gripper frame respectively（1）And pedestal（3）, it is characterised in that：Gripper frame（1）It is equipped with folder
Component is held, the clamp assemblies include panel（11）, panel（11）Upside is equipped with geometrical clamp gripping member（12）, downside is equipped with activity and presss from both sides
Hold mechanism（13）, the activity clamping device（13）Including one group of guide groove（131）Be sleeved on guide groove（131）Interior is flexible
Bar（132）, the guide groove（131）It is mutually inclined arranged symmetrically, guide groove（131）With telescopic rod（132）Pass through tension spring（135）
Connection, the telescopic rod（132）Tail end be equipped with clamping apex angle（133）, the geometrical clamp gripping member（12）With clamping apex angle（133）
It is bathtub construction, slot inner underside is equipped with thickness and adjusts slope（121）；
Pedestal（3）It is equipped with bottom plate（34）, bottom plate（34）Upside is equipped with connected unit（31）, snapping plate（33）With connected unit（31）Button
It connects, compensation block（32）Mounted on connected unit（31）With snapping plate（33）Between, the connected unit（31）Upside is circumferentially distributed have to
Few three arc-shaped claws（311）, claw（311）Inside length direction is provided with dovetail groove（312）, claw（311）In inside
Portion's short transverse is provided with card hole（313）, snapping plate（33）Outer ring circumferentially distributed have and claw（311）Corresponding connector（331）,
Connector（331）Outer end middle part is equipped with and card hole（313）The convex block of docking（332）, the compensation block（32）For circular ring shape, compensation block
（32）Downside be equipped at least three springs（321）；
The support column（2）By two symmetrical semicylinders（221）It forms, support column（2）Upper end be equipped with it is at least one
Spherical cavity（222）, lower end is equipped with cylindrical cavity（223）, cylindrical cavity（23）Convex block is equipped at the top of cavity wall（225）, support column
（2）Middle part is radially provided with pass through aperture（224）, through hole（24）Place is equipped with locking device（24）By two semicylinders（221）
Connection, support column（2）Upper end is equipped with angle regulator（21）, angle regulator（21）Bottom is equipped at least one bulb
（211）, bulb（211）It is placed on spherical cavity（222）It is interior, support column（2）Lower end is equipped with height adjustment device（23）, height adjusting
Device（23）Upper end be horizontally installed with cylindrical turntable（232）, turntable（232）It is placed on cylindrical cavity（23）It is interior,
The turntable（232）Upper center is radially provided with gear adjustable plate（233）, the gear adjustable plate（233）For sector, gear
Adjustable plate（233）Both sides along radial direction be equipped with several grooves（234）, the angle regulator（21）Top and folder
Hold frame（1）Bottom connects, height adjustment device（23）Bottom end and snapping plate（33）Connection.
2. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：It is described to connect
Head（331）With claw（311）Height ratio be 1:1.2~1.6.
3. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：It is described to lead
To slot（131）Between angle be 30 °~60 °.
4. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：The thickness
Degree adjusts slope（21）Slope surface be arc.
5. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：The lock
Tight device（24）Including bolt（241）And knob（242）, knob（242）On be provided with threaded hole, bolt（241）Across through hole
（224）With knob（242）It is threadedly coupled, knob（242）With through hole（224）Between be equipped at least one gasket（243）.
6. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：The ball
Shape chamber（222）And cylindrical cavity（223）Cavity wall opening be provided with the notch of arc（226）.
7. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：Gear tune
Save plate（233）Groove per side（234）Number is 2~12, adjacent grooves（234）Between angle be 5 °~60 °.
8. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：The company
Connect platform（31）Upper end inner wall is equipped with a circle limit round table（314）, compensation block（32）The diameter of upper end is less than limit round table（314）'s
Internal diameter, compensation block（32）Lower end diameter is more than limit round table（314）Internal diameter, less than connected unit（31）Internal diameter.
9. a kind of aircraft cockpit electronic flight data bag support according to claim 1, it is characterised in that：The bottom
Plate（34）One end be equipped with pinboard（341）, the pinboard（341）Tilt down setting, bottom plate（34）With pinboard（341）
Angle be 30 °~150 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810029464.3A CN108190037A (en) | 2018-01-12 | 2018-01-12 | A kind of electronic flight data bag support of adjustable-angle and height |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810029464.3A CN108190037A (en) | 2018-01-12 | 2018-01-12 | A kind of electronic flight data bag support of adjustable-angle and height |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108190037A true CN108190037A (en) | 2018-06-22 |
Family
ID=62588732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810029464.3A Pending CN108190037A (en) | 2018-01-12 | 2018-01-12 | A kind of electronic flight data bag support of adjustable-angle and height |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108190037A (en) |
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| GB2576899A (en) * | 2018-09-05 | 2020-03-11 | K&G Yorkshire Ltd | Support assembly |
| CN112197109A (en) * | 2020-09-25 | 2021-01-08 | 中国直升机设计研究所 | Electronic flight bag platform support |
| CN114909587A (en) * | 2022-04-29 | 2022-08-16 | 无锡和源精密机械有限公司 | Telescopic and multidirectional-adjustable PED (foot-operated vehicle) bracket of aviation passenger seat |
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| CN114909587B (en) * | 2022-04-29 | 2024-02-20 | 无锡和源精密机械有限公司 | Scalable and multidirectional adjustable PED support of aviation passenger seat |
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Effective date of abandoning: 20240315 |