CN205901843U - Portable satellite communication phone - Google Patents
Portable satellite communication phone Download PDFInfo
- Publication number
- CN205901843U CN205901843U CN201620897039.2U CN201620897039U CN205901843U CN 205901843 U CN205901843 U CN 205901843U CN 201620897039 U CN201620897039 U CN 201620897039U CN 205901843 U CN205901843 U CN 205901843U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- rotating disk
- gear
- latch
- satellite
- 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 - Fee Related
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Abstract
The utility model discloses a portable satellite communication phone, including satellite antenna, satellite communication system, battery module, microphone module, speaker module and fuselage, battery module, microphone module, speaker module, satellite antenna all connect the satellite communication system, satellite antenna's one end articulates at the back of fuselage, is provided with on the back of fuselage to be used for ordering about satellite antenna pivoted elasticity locking mechanical system, the utility model discloses the antenna that portable satellite communication phone opened the satellite phone only needs one -hand operation, and is quick convenient, can not be too quickly because of hard, and lead to the impaired phenomenon of the antenna of satellite phone, the experience of using has improved.
Description
Technical field
This utility model is related to a kind of portable satellite communication phone.
Background technology
Satellite phone is to be exactly satellite relay communication based on satellite communication system come the communication of transmission information.In satellite
The communication that continues is the product of present mobile communication, and its major function is to fill up existing communication (wire communication, radio communication) terminal
The region that cannot cover, the work for people provides more sound service.In modern communicationses, satellite communication is cannot be by other
Communication mode is substituted, all communication functions that existing conventional communication is provided, and is all applied in satellite communication.Existing
Some satellite phones are limited by technical limitations, and the size of the antenna of satellite phone is larger, receives for convenience, need to fold rear
Just deposit, the antenna of manual unlocking satellite phone needs bimanualness, cause certain not convenient, and easily because firmly
Too quickly, lead to the antenna of satellite phone impaired, affect experience.
Utility model content
The purpose of this utility model is to overcome above-mentioned deficiency present in prior art, and provides a kind of structure design to close
Reason, singlehanded can open the portable satellite communication phone of the antenna of satellite phone.
The technical scheme in the invention for solving the above technical problem is:
A kind of portable satellite communication phone, including satellite antenna, Satellite Communication System, battery module, microphone module,
Loudspeaker module and fuselage, battery module, microphone module, loudspeaker module, satellite antenna are all connected with Satellite Communication System,
One end of described satellite antenna be hinged on fuselage the back side it is characterised in that: be provided with for ordering about satellite on the back side of fuselage
Antenna rotate elastic locking mechanism, described elastic locking mechanism include first gear, second gear, rotating shaft, the first connection sheet,
Second connection sheet, torque spring, stage clip, control rotating disk, latch, latch spring, one end of first gear and satellite antenna is fixed,
Control rotating disk and second gear to be rotatably installed in rotating shaft, first gear and second gear engage, control rotating disk and rotating shaft to adopt
Axial restraint, rotating shaft is vertically slidably mounted on fuselage, controls rotating disk and second gear to fix, described latch is slidably mounted on machine
With, perpendicular to the axis of rotating shaft, the two ends of described latch spring are against latch and fuselage respectively, make latch pressure for the axis of latch
To the wall controlling rotating disk, the wall controlling rotating disk offers the lock slots for inserting latch, lock slots are upwardly-directed gone up
Be gradually reduced after groove so that the groove bottom of lock slots and control rotating disk wall rounding off, the first connection sheet, the second connection sheet
It is fixed in rotating shaft, control rotating disk and second gear to be respectively positioned between the first connection sheet, the second connection sheet, the upper end of described stage clip
It is against respectively in the second connection sheet and fuselage with lower end, thus rotating shaft is pushed up upwards by stage clip, the inner of described torque spring
Connect second gear and fuselage with outer end respectively, the upper end of rotating shaft is fixed with button, described button passes through the outer wall of fuselage to machine
Outside body.Using this structure, when needing to open satellite antenna, press the button, control rotating disk to glide, be originally plugged in lock
Determine the latch in groove and slide into the wall controlling rotating disk, latch departs from lock slots, and in the presence of torque spring, second gear turns
Dynamic, drive first gear to rotate, thus opening satellite antenna；When folding satellite antenna, rotate backward satellite antenna manually,
First gear drives second gear to rotate, and when latch snaps in lock slots, completes to fold, torque spring completes storage power simultaneously.
Preferably, controlling the offside of rotating disk upper locking groove, it is provided with the lobe protruding from the wall controlling rotating disk, convex
The wall of the wall in the portion of rising and control rotating disk is in the arc transition of inner concavity, and the axis of described latch with the wall controlling rotating disk is in
Angle is arranged.Using this structure, in satellite antenna opening procedure, the wall of the end relation control rotating disk of latch moves, by
In axis and the wall setting in angle controlling rotating disk of latch, when the end of latch acts on the wall of lobe, can
To form the resistance stoping satellite antenna from rotating, realize certain buffering effect.
This utility model compared with prior art, has advantages below and effect: this utility model portable satellite communication
The antenna that satellite phone opened by phone only needs to one-handed performance, quick and convenient, because of overexerting, and will not lead to satellite phone
The impaired phenomenon of antenna, improve the experience of use；In satellite antenna rotation process, carry buffering effect, thus can carry
The high texture using.
Brief description
Fig. 1 is the structural representation of this utility model embodiment portable satellite communication phone.
Fig. 2 is the structural representation at this utility model embodiment portable satellite communication phone back side.
Fig. 3 is the mounting structure schematic diagram of this utility model embodiment satellite antenna.
Fig. 4 is the mounting structure schematic diagram of this utility model embodiment latch.
Specific embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings and by embodiment, and following examples are right
Of the present utility model explain and this utility model is not limited to following examples.
Referring to Fig. 1-Fig. 4, a kind of the present embodiment portable satellite communication phone, including satellite antenna 1, satellite communication system
System, battery module, microphone module 21, loudspeaker module 22 and fuselage 3, battery module, microphone module 21, speaker mould
Block 22, satellite antenna 1 are all connected with Satellite Communication System, and one end of described satellite antenna 1 is hinged on the back side of fuselage 3, fuselage 3
Elastic locking mechanism for ordering about satellite antenna 1 rotation is provided with the back side, described elastic locking mechanism includes first gear
41st, second gear 42, rotating shaft 43, the first connection sheet 44, the second connection sheet 45, spiral spring, stage clip 46, control rotating disk 47, latch 48,
Latch spring 49, one end of first gear 41 and satellite antenna 1 is fixed, and controls rotating disk 47 and second gear 42 to be rotatably installed in
On axle 43, first gear 41 and second gear 42 engage, and control rotating disk 47 and rotating shaft 43 to adopt axial restraint, rotating shaft 43 is vertically slided
Move and be arranged on fuselage 3, control rotating disk 47 and second gear 42 to fix, described latch 48 is slidably mounted on fuselage 3, latch 48
Axis perpendicular to rotating shaft 43 axis, the two ends of described latch spring 49 are against latch 48 and fuselage 3 respectively, so that latch 48 is pressed
To the wall controlling rotating disk 47, the wall controlling rotating disk 47 offers the lock slots 471 for inserting latch 48, lock slots
471 upwardly-directed go up groove after be gradually reduced so that the groove bottom of lock slots 471 and the wall rounding off controlling rotating disk 47, the
A connecting piece 44, the second connection sheet 45 are fixed in rotating shaft 43, control rotating disk 47 and second gear 42 to be respectively positioned on the first connection sheet
44th, between the second connection sheet 45, the top and bottom of described stage clip 46 are against on the second connection sheet 45 and fuselage 3 respectively.Thus
By stage clip 46, rotating shaft 43 is pushed up upwards, the inner of described spiral spring and outer end connect second gear 42 and fuselage 3, rotating shaft 43 respectively
Upper end be fixed with button 410, described button 410 pass through fuselage 3 outer wall to outside fuselage 3.
Control the offside of rotating disk 47 upper locking groove 471, be provided with the lobe 472 protruding from the wall controlling rotating disk 47,
The wall of lobe 472 and the arc transition in inner concavity for the wall controlling rotating disk 47, the axis of described latch 48 and control turn
The wall of disk 47 is in that angle is arranged.
Above content described in this specification is only to this utility model example explanation.This utility model
Person of ordinary skill in the field can make various modifications or supplement or adopt class to described specific embodiment
As mode substitute, the content without departing from this utility model description or surmount model defined in the claims
Enclose, protection domain of the present utility model all should be belonged to.
Claims (2)
1. a kind of portable satellite communication phone, including satellite antenna, Satellite Communication System, battery module, microphone module, raises
Sound device module and fuselage, battery module, microphone module, loudspeaker module, satellite antenna are all connected with Satellite Communication System, institute
State satellite antenna one end be hinged on fuselage the back side it is characterised in that: be provided with for ordering about satellite sky on the back side of fuselage
The elastic locking mechanism that line rotates, described elastic locking mechanism include first gear, second gear, rotating shaft, the first connection sheet, the
Two connection sheets, torque spring, stage clip, control rotating disk, latch, latch spring, one end of first gear and satellite antenna is fixed, control
Rotating disk processed and second gear are rotatably installed in rotating shaft, and first gear and second gear engage, and control rotating disk and rotating shaft to adopt axle
To fixation, rotating shaft is vertically slidably mounted on fuselage, controls rotating disk and second gear to fix, described latch is slidably mounted on fuselage
On, perpendicular to the axis of rotating shaft, the two ends of described latch spring are against latch and fuselage respectively, so that latch is pressed to for the axis of latch
Control the wall of rotating disk, the wall controlling rotating disk offers the lock slots for inserting latch, lock slots upwardly-directed go up groove
It is gradually reduced afterwards so that the groove bottom of lock slots and the wall rounding off controlling the transformation of ownership, the first connection sheet, the second connection sheet are solid
Be scheduled in rotating shaft, control rotating disk and second gear to be respectively positioned between the first connection sheet, the second connection sheet, the upper end of described stage clip and
Lower end is against on the second connection sheet and fuselage respectively, thus rotating shaft is pushed up upwards by stage clip, the inner of described torque spring and
Outer end connects second gear and fuselage respectively, and the upper end of rotating shaft is fixed with button, and described button passes through the outer wall of fuselage to fuselage
Outward.
2. portable satellite communication phone according to claim 1 it is characterised in that: control rotating disk upper locking groove right
Side, is provided with the lobe protruding from the wall controlling rotating disk, the wall of lobe and the wall controlling rotating disk are in inner concavity
Arc transition, the axis of described latch and the wall controlling rotating disk are in that angle is arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620897039.2U CN205901843U (en) | 2016-08-18 | 2016-08-18 | Portable satellite communication phone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620897039.2U CN205901843U (en) | 2016-08-18 | 2016-08-18 | Portable satellite communication phone |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205901843U true CN205901843U (en) | 2017-01-18 |
Family
ID=57779753
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620897039.2U Expired - Fee Related CN205901843U (en) | 2016-08-18 | 2016-08-18 | Portable satellite communication phone |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205901843U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111710954A (en) * | 2020-05-18 | 2020-09-25 | 宇龙计算机通信科技(深圳)有限公司 | Antenna device, antenna device control method, antenna device control device and terminal |
| CN112822313A (en) * | 2021-01-18 | 2021-05-18 | 深圳市云天智能通讯有限公司 | Satellite telephone distress method based on heaven-earth satellite and terminal equipment |
| CN112909489A (en) * | 2021-01-21 | 2021-06-04 | 杭州永谐科技有限公司上海分公司 | Foldable structure and log-periodic antenna with same |
-
2016
- 2016-08-18 CN CN201620897039.2U patent/CN205901843U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111710954A (en) * | 2020-05-18 | 2020-09-25 | 宇龙计算机通信科技(深圳)有限公司 | Antenna device, antenna device control method, antenna device control device and terminal |
| CN112822313A (en) * | 2021-01-18 | 2021-05-18 | 深圳市云天智能通讯有限公司 | Satellite telephone distress method based on heaven-earth satellite and terminal equipment |
| CN112909489A (en) * | 2021-01-21 | 2021-06-04 | 杭州永谐科技有限公司上海分公司 | Foldable structure and log-periodic antenna with same |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170118 Termination date: 20190818 |