CN104134865A - Energy-saving satellite rotation base - Google Patents

Energy-saving satellite rotation base Download PDF

Info

Publication number
CN104134865A
CN104134865A CN201410407172.0A CN201410407172A CN104134865A CN 104134865 A CN104134865 A CN 104134865A CN 201410407172 A CN201410407172 A CN 201410407172A CN 104134865 A CN104134865 A CN 104134865A
Authority
CN
China
Prior art keywords
slip cap
motor
rolling disc
sensing unit
driving head
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
Application number
CN201410407172.0A
Other languages
Chinese (zh)
Inventor
陈敏
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.)
JIANGSU SATELLITE NAVIGATION AND COMMUNICATION Co Ltd
Original Assignee
JIANGSU SATELLITE NAVIGATION AND COMMUNICATION 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 JIANGSU SATELLITE NAVIGATION AND COMMUNICATION Co Ltd filed Critical JIANGSU SATELLITE NAVIGATION AND COMMUNICATION Co Ltd
Priority to CN201410407172.0A priority Critical patent/CN104134865A/en
Publication of CN104134865A publication Critical patent/CN104134865A/en
Pending legal-status Critical Current

Links

Landscapes

  • Details Of Aerials (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

The invention discloses a speed-regulating rotation base. A rotation control mechanism is arranged in the rotation base and a signal sensing unit is arranged at one end of the head portion of a main rotation shaft of the rotation base, so that the signal sensing unit controls the rotation control mechanism to achieve idle rotation or loaded rotation of a motor, the satellite antenna driving force is regulated and energy is saved.

Description

A kind of energy-conservation satellite rotating base
Technical field
The present invention relates to a kind of energy-conservation satellite rotating base, belong to satellite fields.
Background technology
Along with social development, people's awareness of saving energy is more and more stronger, and under different external environments, the transmission capacity of satellite and the ability to accept of satellite antenna are also different, if can manufacture a kind of satellite rotating base that decides satellite antenna velocity of rotation according to signal strength signal intensity, just can realize energy-conservation largely.
Summary of the invention
The object of the invention is to: a kind of energy-saving satellite rotating base is provided.
The present invention realizes by the following method:
A kind of energy-conservation satellite rotating base, described rotating base comprises main shaft, driving head, sensing unit, control device for pivoting, motor, antenna, described antenna is arranged on driving head, described driving head rotates around main shaft, described motor is arranged on driving head internal drive rotating base and rotates, described sensing unit is arranged on main shaft, described control device for pivoting is arranged on driving head inside, and described sensing unit is connected with control device for pivoting to be controlled the rotation of rotating base and stops;
Described control device for pivoting comprises clutch plate, rolling disc, slip cap, suspension rod, linear stepping motor, described clutch plate is fixed on driving head, the coil of described motor is arranged on stator, the magnetic patch of described motor is arranged on the shell of motor, shell and the rolling disc of described motor are fixed, on described slip cap socket rolling disc, on described rolling disc, be provided with some keyways, on described slip cap, be provided with some protruding keys, described slip cap coordinates being slidably connected of realization and rolling disc by key and keyway, described slider disc is provided with a rubbing surface, described rolling disc contacts with clutch plate static friction by rubbing surface, on described main shaft, be processed with several strip grooves parallel with main shaft, described slip cap is circular, described slip cap radial center is provided with some connecting rods that pointed to the circle ring center of slip cap by slip cap inwall, the connection central vertical of described connecting rod is fixed with suspension rod, described suspension rod is connected with linear stepping motor, described connecting rod moves along strip groove under the drive of linear stepping motor by suspension rod, described slip cap is by the movement of connecting rod and the rubbing surface of rolling disc contact or separated,
Described control device for pivoting is connected with sensing unit by linear stepping motor, and linear stepping motor moves suspension rod under the control of sensing unit.
As further innovation of the present invention, described stepping motor is fixed in rotating shaft.
beneficial effect
The present invention is provided with sensing unit by a rotation controling mechanism while is set in rotating base inside in head one end of the main shaft of rotating base, when signal is experienced when stronger in sensing unit, can driving clutch mechanism, make antenna reduce velocity of rotation or stop operating, reduce the load of motor, realize energy-conservation.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is slip cap scheme of installation of the present invention.
In figure: 1, clutch plate; 2, driving head; 3, slip cap; 4, connecting rod; 5, rolling disc; 6, shell; 7, rotor; 8, magnetic patch; 9, main shaft; 10, suspension rod; 11, linear stepping motor; 12, sensing unit.
Embodiment
Below in conjunction with accompanying drawing, be described further
A kind of energy-conservation satellite rotating base, described rotating base comprises main shaft 9, driving head 2, sensing unit 12, control device for pivoting, motor, antenna, described antenna is arranged on driving head 2, described driving head 2 rotates around main shaft 9, described motor is arranged on driving head 2 internal drive rotating bases and rotates, described sensing unit 12 is arranged on main shaft, described control device for pivoting is arranged on driving head 2 inside, and described sensing unit 12 is connected with control device for pivoting to be controlled the rotation of rotating base and stops;
Described control device for pivoting comprises clutch plate 1, rolling disc 5, slip cap 3, suspension rod 10, linear stepping motor 11, described clutch plate 1 is fixed on driving head 2, the coil of described motor is arranged on rotor 7, the magnetic patch 8 of described motor is arranged on the shell 6 of motor, the shell 6 of described motor and rolling disc 5 are fixing, on described slip cap 3 socket rolling discs 5, on described rolling disc 5, be provided with some keyways, on described slip cap 3, be provided with some protruding keys, described slip cap 3 coordinates being slidably connected of realization and rolling disc 5 by key and keyway, described slider disc is provided with a rubbing surface, described rolling disc 5 contacts with clutch plate 1 static friction by rubbing surface, on described main shaft 9, be processed with several strip grooves parallel with main shaft 9, described slip cap 3 is circular, described slip cap 3 radial center are provided with some connecting rods 4 that pointed to the circle ring center of slip cap 3 by slip cap 3 inwalls, the connection central vertical of described connecting rod 4 is fixed with suspension rod 10, described suspension rod 10 is connected with linear stepping motor 11, described connecting rod 4 moves along strip groove under the drive of linear stepping motor 11 by suspension rod 10, described slip cap 3 is by the movement of connecting rod 4 and the rubbing surface of rolling disc 5 contact or separated,
Described control device for pivoting is connected with sensing unit 12 by linear stepping motor 11, and linear stepping motor 11 moves suspension rod 10 under the control of sensing unit 12;
Described stepping motor is fixed in rotating shaft.
By sensing unit 12, control pivoting controller, when signal is experienced when stronger in sensing unit 12, sensing unit 12 is controlled linear stepping motor 11 slip cap 3 is moved with respect to rolling disc 5, make slip cap 3 leave clutch plate 1, there is idle running and stop gradually in motor now, driving head 2 is also because the rotating speed that runs out of steam is slack-off until stop, when signal weaker is experienced in sensing unit 12, control linear stepping motor 11 by slip cap 3 moving contact clutch plates 1, now rotating base recovers to rotate, the advantage of this rotating base is that this rotating base can be as traditional rotating base, high-speed starting stops at a high speed, produce great energy resource consumption, this rotating base again can be according to signal strength signal intensity free adjustment velocity of rotation simultaneously, prevent unnecessary energy resource consumption.

Claims (2)

1. an energy-conservation satellite rotating base, it is characterized in that: described rotating base comprises main shaft, driving head, sensing unit, control device for pivoting, motor, antenna, described antenna is arranged on driving head, described driving head rotates around main shaft, described motor is arranged on driving head internal drive rotating base and rotates, described sensing unit is arranged on main shaft, described control device for pivoting is arranged on driving head inside, and described sensing unit is connected with control device for pivoting to be controlled the rotation of rotating base and stops;
Described control device for pivoting comprises clutch plate, rolling disc, slip cap, suspension rod, linear stepping motor, described clutch plate is fixed on driving head, the coil of described motor is arranged on stator, the magnetic patch of described motor is arranged on the shell of motor, shell and the rolling disc of described motor are fixed, on described slip cap socket rolling disc, on described rolling disc, be provided with some keyways, on described slip cap, be provided with some protruding keys, described slip cap coordinates being slidably connected of realization and rolling disc by key and keyway, described slider disc is provided with a rubbing surface, described rolling disc contacts with clutch plate static friction by rubbing surface, on described main shaft, be processed with several strip grooves parallel with main shaft, described slip cap is circular, described slip cap radial center is provided with some connecting rods that pointed to the circle ring center of slip cap by slip cap inwall, the connection central vertical of described connecting rod is fixed with suspension rod, described suspension rod is connected with linear stepping motor, described connecting rod moves along strip groove under the drive of linear stepping motor by suspension rod, described slip cap is by the movement of connecting rod and the rubbing surface of rolling disc contact or separated,
Described control device for pivoting is connected with sensing unit by linear stepping motor, and linear stepping motor moves suspension rod under the control of sensing unit.
2. a kind of energy-conservation satellite rotating base as claimed in claim 1, is characterized in that: described stepping motor is fixed in rotating shaft.
CN201410407172.0A 2014-08-19 2014-08-19 Energy-saving satellite rotation base Pending CN104134865A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410407172.0A CN104134865A (en) 2014-08-19 2014-08-19 Energy-saving satellite rotation base

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410407172.0A CN104134865A (en) 2014-08-19 2014-08-19 Energy-saving satellite rotation base

Publications (1)

Publication Number Publication Date
CN104134865A true CN104134865A (en) 2014-11-05

Family

ID=51807453

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410407172.0A Pending CN104134865A (en) 2014-08-19 2014-08-19 Energy-saving satellite rotation base

Country Status (1)

Country Link
CN (1) CN104134865A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09148818A (en) * 1995-11-24 1997-06-06 Matsushita Electric Works Ltd Driving device of tracking antenna
CN2696142Y (en) * 2004-01-07 2005-04-27 胡锦昌 Remote controlled antenna steering apparatus without gear
CN102437428A (en) * 2011-09-19 2012-05-02 四川九洲电器集团有限责任公司 Embedded one-dimensional (1D) antenna rotating platform
CN102712268A (en) * 2010-01-14 2012-10-03 布罗泽汽车部件制造哈尔施塔特有限公司 Device for controlling an adjustable drive element of an adjusting device and adjusting device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09148818A (en) * 1995-11-24 1997-06-06 Matsushita Electric Works Ltd Driving device of tracking antenna
CN2696142Y (en) * 2004-01-07 2005-04-27 胡锦昌 Remote controlled antenna steering apparatus without gear
CN102712268A (en) * 2010-01-14 2012-10-03 布罗泽汽车部件制造哈尔施塔特有限公司 Device for controlling an adjustable drive element of an adjusting device and adjusting device
CN102437428A (en) * 2011-09-19 2012-05-02 四川九洲电器集团有限责任公司 Embedded one-dimensional (1D) antenna rotating platform

Similar Documents

Publication Publication Date Title
CN103326538B (en) Permanent magnet intelligent speed-regulating energy-saving device
CN102324829B (en) Adjustable axial asynchronous magnetic force coupler
CN204741386U (en) Birotor axial magnetic circuit machinery becomes magnetic flow permanent -magnet type synchronous machine
CN110504816B (en) Monopole magnet rotary speed-adjustable cage type magnetic coupler
CN101814820A (en) Permanent-magnetic drive speed adjustor
CN203457028U (en) Coaxial sleeve type permanent magnetic eddy current coupling employing magnet-gathering type magnetic circuit structure
CN103580447B (en) A kind of double disc type permanent magnet retarder for vehicle
CN204761271U (en) Three cylinder magnetic transmission speed regulators
CN206988292U (en) A kind of permanent-magnet suspender
CN102367142A (en) Inner rotor switch reluctance traction driving device
CN104836372A (en) Conical rotor DC permanent magnet brake motor
CN202864570U (en) Take-up machine fixing center
CN204794548U (en) Toper rotor direct current permanent magnetism brake motor
CN104134865A (en) Energy-saving satellite rotation base
CN204236759U (en) A kind of electromagnetic power propelling unit group, propelling unit and structure thereof
CN103107679A (en) Permanent magnet eddy coupling with smaller time-lag effects in disc type
CN202321890U (en) Switched reluctance traction drive device for inner rotors
CN203788120U (en) Permanent-magnet speed-regulating energy-saving device for oil pumping unit
CN101552510B (en) Electromagnetic induction energy-saving governor
CN203416149U (en) Permanent-magnet intelligent speed-regulation energy-saving apparatus
CN211142279U (en) Mixed magnetic suspension bearing for driving spindle of rotor ultra-high-speed motor
CN103490589A (en) Coaxial sleeve type permanent magnet eddy-current coupling with magnetic coagulation type magnetic circuit structure
CN103915980A (en) Disc-shaped rotary-plate permanent magnetic coupler
CN203788124U (en) Double flat plate type permanent magnet eddy current coupling with end face being fixed
CN102606658B (en) Permanent magnet motor electromagnetic braking clutch utilizing permanent magnet rotor end face magnetic force

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20141105