CN202923892U - Support used for onboard IPAD of airplane cockpit - Google Patents

Support used for onboard IPAD of airplane cockpit Download PDF

Info

Publication number
CN202923892U
CN202923892U CN 201220615073 CN201220615073U CN202923892U CN 202923892 U CN202923892 U CN 202923892U CN 201220615073 CN201220615073 CN 201220615073 CN 201220615073 U CN201220615073 U CN 201220615073U CN 202923892 U CN202923892 U CN 202923892U
Authority
CN
China
Prior art keywords
ipad
porthole
support
firm banking
open slot
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.)
Expired - Lifetime
Application number
CN 201220615073
Other languages
Chinese (zh)
Inventor
王瑞
孙志芳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
HAINING RED LION BAOSHENG SCIENCE AND TECHNOLOGY Co Ltd
Original Assignee
HAINING RED LION BAOSHENG SCIENCE AND TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by HAINING RED LION BAOSHENG SCIENCE AND TECHNOLOGY Co Ltd filed Critical HAINING RED LION BAOSHENG SCIENCE AND TECHNOLOGY Co Ltd
Priority to CN 201220615073 priority Critical patent/CN202923892U/en
Application granted granted Critical
Publication of CN202923892U publication Critical patent/CN202923892U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • Casings For Electric Apparatus (AREA)

Abstract

The utility model discloses a support used for an onboard IPAD of an airplane cockpit. The support comprises a support plate, a fixed base, a damping hinge and a snap fastener, wherein the support plate is connected with the fixed base through the damping hinge, one side of the fixed base is connected with the snap fastener, the snap fastener is matched to a microphone hook arranged on one side of a porthole sill, an open slot and a fixing plate are arranged on the other side of the fixed base, and the open slot and the fixing plate are matched to a chart clamp arranged on the porthole sill. According to the utility model, the IPAD is arranged in the cockpit on the premise that no structure of the cockpit is changed, and the support has the advantages of simple structure, and safe and reliable installation.

Description

A kind of support for the airborne IPAD of aircraft cockpit
Technical field
The utility model relates to the support of a kind of IPAD of support, is specifically related to a kind of support for the airborne IPAD of aircraft cockpit.
Background technology
At present, along with popularizing of IPAD panel computer, its application is extended to every field.The airline carriers of passengers chaufeur needs to carry the hard copy files such as flight airmanship, chart in flight course, these hard copy files are converted into electronic file to be deposited IPAD in and has and reduce the file amount of carrying, realize the advantage of fast finding, it is following developing direction that the aviator uses the auxiliary aerial mission of completing of IPAD.Family expenses IPAD support, vehicle-mounted IPAD support are arranged in the market, due to the restriction of the structure that is subjected to aircraft cockpit, space and flight safety, and the requirement of the aviation of airborne part specialty, these existing IPAD supports all can't directly apply to driving compartment.
Summary of the invention
Technical problem to be solved in the utility model is to provide a kind of support for the airborne IPAD of aircraft cockpit, can realize IPAD is arranged in driving compartment under the prerequisite of any structure that does not change driving compartment, and is simple in structure, installs safe and reliable.
The technical scheme that the utility model technical solution problem adopts is: a kind of support for the airborne IPAD of aircraft cockpit, comprise stay bearing plate, firm banking, damp hinge and snap lock, be connected by damp hinge between described stay bearing plate and firm banking, described firm banking one side is connected with snap lock, the microphone hook Matching installation that described snap lock and porthole windowsill one side are set, described firm banking opposite side is provided with open slot and adapter plate, and chart set on described open slot and adapter plate and porthole windowsill presss from both sides Matching installation.
The utility model utilizes chart folder, microphone hook and porthole windowsill on the driving compartment porthole to design as the fixed position according to the architectural feature of driving compartment porthole.The utility model is placed on the porthole windowsill, and firm banking and the surface applying of porthole windowsill make it not produce downward displacement; There is a gap in chart folder with porthole windowsill interplanar, design the profile that a pair of profiling panel beating adapter plate is avoided the chart folder, inserts simultaneously this gap, make the chart folder form to the IPAD support up and down, front and back and to the restriction of left dislocation; Microphone hook is positioned at the porthole side, design on the cylinder that a snap lock is hooked in microphone hook horizontal direction, forms upwards, reaches the restriction of fore-and-aft direction displacement to the right, and the rotation of the limitation of length hasp that microphone is linked up with can prevent from coming off.
The utility model can be realized symmetrical two kinds of supports to design by mirror, makes on its porthole that is arranged on respectively driver side and copilot's side, and can by changing the size of firm banking, be applied on the different types of machines such as narrow body or expanded letter.
The beneficial effects of the utility model are: simple in structure, easy for installation, need not to damage any part of driving compartment.
Description of drawings
Fig. 1 for existing aircraft cockpit porthole windowsill and on chart folder and the layout schematic diagram linked up with of microphone.
Fig. 2 is the assembling schematic diagram of the utility model embodiment.
Fig. 3 is the structural representation of the utility model embodiment permanent seat.
Fig. 4 is that the utility model embodiment is installed on the structural representation on aircraft cockpit porthole windowsill.
Below in conjunction with accompanying drawing, the utility model is described further.
The specific embodiment
By reference to the accompanying drawings, a kind of support for the airborne IPAD of aircraft cockpit comprises stay bearing plate 4, firm banking 5, damp hinge 6 and snap lock 7, is connected by damp hinge 6 between stay bearing plate 4 and firm banking 5, adopts self-clinching stud during connection; Be connected with snap lock 7 by screw 8 in firm banking 5 one sides, microphone hook 2 Matching installations that snap lock 7 and porthole windowsill 1 one sides are set, be provided with open slot 9 and a pair of adapter plate 11 at firm banking 5 opposite sides, chart set on open slot 9 and adapter plate 11 and porthole windowsill 1 presss from both sides 3 Matching installations.
During practical application, at first IPAD10 is inserted in stay bearing plate 4, then the open slot 9 of firm banking 5 is connected with chart folder 3 couplings, at last snap lock 7 is hooked in microphone and links up with the bottom, and rotate up locking and namely place and complete.Reverse order according to above-mentioned steps when taking off gets final product.

Claims (1)

1. support that is used for the airborne IPAD of aircraft cockpit, it is characterized in that: comprise stay bearing plate (4), firm banking (5), damp hinge (6) and snap lock (7), be connected by damp hinge (6) between described stay bearing plate (4) and firm banking (5), described firm banking (5) one sides are connected with snap lock (7), microphone hook (2) Matching installation that described snap lock (7) and porthole windowsill (1) one side are set, described firm banking (5) opposite side is provided with open slot (9) and adapter plate (11), described open slot (9) and adapter plate (11) and the upper set chart folder of porthole windowsill (1) (3) Matching installation.
CN 201220615073 2012-11-20 2012-11-20 Support used for onboard IPAD of airplane cockpit Expired - Lifetime CN202923892U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220615073 CN202923892U (en) 2012-11-20 2012-11-20 Support used for onboard IPAD of airplane cockpit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220615073 CN202923892U (en) 2012-11-20 2012-11-20 Support used for onboard IPAD of airplane cockpit

Publications (1)

Publication Number Publication Date
CN202923892U true CN202923892U (en) 2013-05-08

Family

ID=48213879

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220615073 Expired - Lifetime CN202923892U (en) 2012-11-20 2012-11-20 Support used for onboard IPAD of airplane cockpit

Country Status (1)

Country Link
CN (1) CN202923892U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106935135A (en) * 2017-03-08 2017-07-07 成都汇腾机电设备有限公司 It is a kind of to be applied to the combination aluminium section bar that suspension type indicates label
CN107819236A (en) * 2017-11-20 2018-03-20 镇江华京通讯科技有限公司 A kind of radio frequency (RF) coaxial connector Contiuum type dust cap

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106935135A (en) * 2017-03-08 2017-07-07 成都汇腾机电设备有限公司 It is a kind of to be applied to the combination aluminium section bar that suspension type indicates label
CN107819236A (en) * 2017-11-20 2018-03-20 镇江华京通讯科技有限公司 A kind of radio frequency (RF) coaxial connector Contiuum type dust cap

Similar Documents

Publication Publication Date Title
US9463877B2 (en) Mounting device for suspending a visual barrier of a passenger cabin of a means of transport
CN201989945U (en) Modular quick-splicing type unmanned aerial vehicle
JP6411518B2 (en) Luggage box system
CN202923892U (en) Support used for onboard IPAD of airplane cockpit
EP3231715B1 (en) Commercial aircraft interior monument protection system
US20150034686A1 (en) Electronic flight bag retention device
CN103273889A (en) Detachable vehicle-mounted computer support
CN202686768U (en) Fixing structure for plug-in airborne photoelectric pod on fixed wing aircraft
US20140042272A1 (en) Centre pedestal for aircraft cockpit and aircraft comprising such a pedestal
AU2014203442B2 (en) Joint assembly and method of assembling same
CN205113723U (en) Unmanned aerial vehicle is with quick parachute -opening umbrella cabin structure
CN205707390U (en) A kind of aircraft cockpit EFB fixed mount
CN203651647U (en) Tablet computer fixing structure of car seat
CN205010465U (en) Unmanned aerial vehicle
CN204368408U (en) For being fixedly connected with the mounting structure of model plane fuselage and wing
US11029574B2 (en) Wirelessly controlled electrically switchable window system
CN102717894B (en) Fixing structure of external onboard photoelectric pod on fixed-wing aircraft
CN103264647B (en) A kind of automobile-used bookshelf
CN203920602U (en) A kind of retractable automobile top platform
CN201971160U (en) Folding chair for airplanes
CN103523240B (en) Airborne geophysical prospecting equipment props up extension structure for pod
CN105292495A (en) Fast parachute-opening parachute bay structure for unmanned aerial vehicle
CN112078812A (en) Magnetometer carrying device for aeromagnetic system of fixed-wing unmanned aerial vehicle
CN205554557U (en) Unmanned aerial vehicle flight deck and unmanned aerial vehicle
CN205770103U (en) A kind of to increase the airline carriers of passengers driving cabin EFB bearing support that material manufacturing technology makes

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20130508

CX01 Expiry of patent term