CN203300802U - Satellite antenna elevation transmission device - Google Patents

Satellite antenna elevation transmission device Download PDF

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Publication number
CN203300802U
CN203300802U CN2013202539597U CN201320253959U CN203300802U CN 203300802 U CN203300802 U CN 203300802U CN 2013202539597 U CN2013202539597 U CN 2013202539597U CN 201320253959 U CN201320253959 U CN 201320253959U CN 203300802 U CN203300802 U CN 203300802U
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CN
China
Prior art keywords
pitching
deep groove
groove ball
ball bearing
fixedly connected
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
Application number
CN2013202539597U
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Chinese (zh)
Inventor
郑华山
张强
牛文广
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Beijing Aerospace Guanghua Electronic Technology Co Ltd
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Beijing Aerospace Guanghua Electronic Technology Co Ltd
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Priority to CN2013202539597U priority Critical patent/CN203300802U/en
Application granted granted Critical
Publication of CN203300802U publication Critical patent/CN203300802U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides a satellite antenna elevation transmission device. By powering a step motor or manually rotating a lifting hand wheel, an elevation long shaft and an elevation short shaft are driven to rotate. Speed reduction of a harmonic gear speed reducer assembly and flexible wheel output are carried out. Through an elevation flexible wheel connecting plate, a gas spring fixing plate, a support arm and an elevation ladder sleeve, the elevation movement of a paraboloid antenna array is realized. When the paraboloid antenna array moves to a predetermined angle, the paraboloid antenna array moves downward under the action of gravity due to the fact that the harmonic gear transmission does not have a self-locking function. At the moment, an elastic hand wheel is rotated to enable the end face to closely contact the end face of the elevation ladder sleeve. Certain friction is produced, so that locking of the antenna elevation movement is realized. According to the device, the harmonic gear transmission assembly is used, so that the antenna elevation transmission device has advantages of small volume, light weight and large transmission; simply through single stage transmission, the requirement of transmission ratio can be met; and the device is especially suitable for a portable satellite antenna structure form which can be carried around and is used for real time rebroadcast.

Description

A kind of satellite antenna elevating gear
Technical field
The utility model relates to the satellite antenna field, is specifically related to a kind of satellite antenna elevating gear.
Background technology
Current, the technical development of satellite antenna domain-specific rapidly, day by day ripe, the antenna structure form is also varied, and the mechanical transmission mechanism extremely important part that is antenna structure.The mechanical transmission mechanism that satellite antenna is commonly used has gear drive, toothed belt transmission, wire rope gearing and ball-screw-transmission etc., but these mechanical transmission mechanisms all exist that single staged transmission ratio is little, multilevel transmission structure is complicated, volume and the shortcoming such as quality is large, bearing capacity is less and motion artifacts is large; The disclosed radar antenna pitching device of China's CN202523846U patent, the drive mechanism form is ball-screw, and structure is comparatively complicated, and overall dimension is large, and total quality is larger, carries and transport inconvenience.
Harmonic Gears technology and transmission device are widely used in the fields such as space technology, radar communication, the energy, lathe, instrument and meter, robot, automobile, shipbuilding, weaving, metallurgy, conventional weapon, precision optics equipment, printing packaging machinery and medicine equipment, in the situation that identical speed ratio, it is simple in structure, volume is little, quality is light, is particularly suitable for the Portable satellite aerial version that can carry, relay in real time.At present also the Harmonic Gears technology is not applied in to the relevant report in the satellite antenna transmission device.
The utility model content
The technical problem that the utility model solves is: overcome the deficiencies in the prior art, propose a kind of novel antenna pitching transmission device, that this transmission device has is simple in structure, volume is little, quality is light, and the characteristics such as be easy to carry.
The technical solution of the utility model is: a kind of satellite antenna elevating gear comprises stepping motor, harmonic gear transmission device, degree of tightness handwheel, slack adjuster, pitching middle (center) bearing end cap, pitching major axis, pitching motor end cap, outside protective covers, base, lifting screw, lifting handwheel and pitching minor axis; Harmonic gear transmission device is symmetrically distributed in the two ends of stepping motor by the output shaft at stepping motor two ends; Harmonic gear transmission device comprises circlip for shaft, little end ring I, little end ring II, the air spring fixed head for the fixed air spring, the support arm for the supporting antenna front, pitching ladder axle sleeve, parabolic antenna front, the first deep groove ball bearing, the large bearing (ball) cover of pitching, pitching flexbile gear connecting plate, the second deep groove ball bearing, harmonic gear reducer assembly, key, little axle sleeve, the 3rd deep groove ball bearing, shaft coupling, spacer shell;
Described harmonic gear reducer assembly comprises wave producer, flexbile gear and has just taken turns; Wave producer is connected by key with pitching major axis, pitching minor axis, and by the shaft shoulder of pitching major axis and pitching minor axis, and the shaft orientation moving range of little axle sleeve, the 3rd deep groove ball bearing, pitching middle (center) bearing end cap, pitching motor end cap constraint wave producer; Pitching middle (center) bearing end cap, pitching motor end cap are fixedly connected with base respectively; Just wheel is fixedly connected with base; Pitching flexbile gear connecting plate, parabolic antenna front, air spring fixed head, pitching ladder axle sleeve all are fixedly connected on flexbile gear;
The first deep groove ball bearing Internal and external cycle coordinates with pitching major axis, pitching multidiameter cover gap respectively, and by the shaft orientation moving range of the shaft shoulder of pitching major axis, little end ring I, little end ring II constraint the first deep groove ball bearing; Support arm and pitching ladder axle sleeve outer ring matched in clearance, and to support arm, carry out spacing by the gentle spring dead plate of circlip for shaft;
The second deep groove ball bearing inner ring and pitching flexbile gear connecting plate interference fit, the second deep groove ball bearing outer ring and base matched in clearance, and by the shaft orientation moving range of the large bearing (ball) cover constraint of pitching the second deep groove ball bearing;
Stepping motor is fixedly connected with base by the pitching motor end cap, the output shaft at stepping motor two ends is fixedly connected with pitching major axis, pitching minor axis respectively with spacer shell by shaft coupling, and, by the transmission of harmonic gear reducer assembly, realize the drive connection between stepping motor and parabolic antenna front; Described spacer shell be the pitching major axis with the stepping motor output shaft between be connected axle sleeve;
Be used for preventing dust and be fixedly connected with base with the outside protective covers of protective effect;
One end of pitching minor axis is fixedly connected with stepping motor, and the other end of pitching minor axis is fixedly connected with the lifting handwheel, utilizes the lifting handwheel manually to adjust the pitching transmission of parabolic antenna front;
One end of pitching major axis is fixedly connected with stepping motor, and the other end of pitching major axis is threaded with the degree of tightness handwheel, rotates the degree of tightness handwheel pitching transmission of parabolic antenna front is carried out to locking control.
Described the first deep groove ball bearing is selected deep groove ball bearing 6700.
Described the second deep groove ball bearing is selected deep groove ball bearing 61911.
Described the 3rd deep groove ball bearing is selected deep groove ball bearing 61801.
The utility model advantage compared with prior art is: by the use of Harmonic Gears assembly, make that antenna pitching transmission device volume is little, quality is light and gearratio is larger, only need single-stage driving just can meet the requirement of gearratio, be particularly suitable for the Portable satellite aerial version that can carry, relay in real time; By the lifting handwheel is fixedly connected with the pitching minor axis, can realize the manual input of antenna pitching transmission, at some special occasions, motor drives in limited situation, still can realize normal pitching transmission; By the degree of tightness handwheel is threaded with the pitching major axis, can realize the locking of antenna pitching transmission device; Lifting handwheel and degree of tightness handwheel are circular configuration, and moderate dimensions is at cylindrical outer surface processing annular knurl, not only specious, has also increased certain frictional force; The rigging position of outside protective covers and base is hierarchic structure, plays dustproof effect.
The accompanying drawing explanation
Fig. 1 antenna pitching transmission device cutaway view;
Fig. 2 harmonic gear reducer assembly cutaway view.
Embodiment
Below in conjunction with drawings and Examples, the utility model is described further.
the satellite antenna elevating gear, a kind of satellite antenna elevating gear, comprise stepping motor 28, harmonic gear transmission device, degree of tightness handwheel 1, slack adjuster 2, pitching middle (center) bearing end cap 22, pitching major axis 24, pitching motor end cap 29, outside protective covers 30, base 34, lifting screw 35, lifting handwheel 36 and pitching minor axis 37 as shown in Figure 1, harmonic gear transmission device is symmetrically distributed in the two ends of stepping motor 28 by the output shaft at stepping motor 28 two ends, harmonic gear transmission device comprises circlip for shaft 3, little end ring I 4, little end ring II 5, air spring fixed head 6 for the fixed air spring, support arm 7 for the supporting antenna front, pitching ladder axle sleeve 9, parabolic antenna front 10, the first deep groove ball bearing 11, the large bearing (ball) cover 12 of pitching, pitching flexbile gear connecting plate 14, the second deep groove ball bearing 15, harmonic gear reducer assembly 16, key 19, little axle sleeve 20, the 3rd deep groove ball bearing 21, shaft coupling 25, spacer shell 27,
As shown in Figure 2, described harmonic gear reducer assembly 16 comprises wave producer 41, flexbile gear 43 and has just taken turns 42; Wave producer 41 is connected by key 19 with pitching major axis 24, pitching minor axis 37, and by the shaft shoulder of pitching major axis 24 and pitching minor axis 37, and the shaft orientation moving range of little axle sleeve 20, the 3rd deep groove ball bearing 21, pitching middle (center) bearing end cap 22, pitching motor end cap 29 constraint wave producers 41; Pitching middle (center) bearing end cap 22, pitching motor end cap 29 are fixedly connected with base 34 respectively; Just wheel 42 is fixedly connected with base 34; Pitching flexbile gear connecting plate 14, parabolic antenna front 10, air spring fixed head 6, pitching ladder axle sleeve 9 all are fixedly connected on flexbile gear 43;
The first deep groove ball bearing 11 Internal and external cycles respectively with pitching major axis 24, pitching ladder axle sleeve 9 matched in clearance, and by the shaft orientation moving range of the shaft shoulder of pitching major axis 24, little end ring I 4, little end ring II 5 constraint the first deep groove ball bearings 11; Support arm 7 and pitching ladder axle sleeve 9 outer ring matched in clearance, and undertaken spacing by 6 pairs of support arms of the gentle spring dead plate of circlip for shaft 37;
The second deep groove ball bearing 15 inner rings and pitching flexbile gear connecting plate 14 interference fit, the second deep groove ball bearing 15 outer rings and base 34 matched in clearance, and by the shaft orientation moving range of large bearing (ball) cover 12 constraint the second deep groove ball bearings 15 of pitching;
Stepping motor 28 is fixedly connected with base 34 by pitching motor end cap 29, the output shaft at stepping motor 28 two ends is fixedly connected with pitching major axis 24, pitching minor axis 37 respectively with spacer shell 27 by shaft coupling 25, and, by the transmission of harmonic gear reducer assembly 16, realize the drive connection between stepping motor 28 and parabolic antenna front 10; Described spacer shell 27 is the axle sleeve that is connected between pitching major axis 24 and stepping motor 28 output shafts;
Be used for preventing dust and be fixedly connected with base 34 with the outside protective covers 30 of protective effect;
One end of pitching minor axis 37 is fixedly connected with stepping motor 28, and the other end of pitching minor axis 37 is fixedly connected with lifting handwheel 36, utilizes the pitching transmission of 36 pairs of parabolic antenna fronts 10 of lifting handwheel manually to adjust;
One end of pitching major axis 24 is fixedly connected with stepping motor 28, and the other end of pitching major axis 24 is threaded with degree of tightness handwheel 1, rotates the pitching transmission of 1 pair of parabolic antenna front 10 of degree of tightness handwheel and carries out locking control;
The operation principle of this device is as follows:
By giving stepping motor 28 power supplies or artificial rotation and lifting handwheel 36, drive pitching major axis 24,37 rotations of pitching minor axis, through harmonic gear reducer assembly 16, slow down, and by flexbile gear 43 outputs, by pitching flexbile gear connecting plate 14, air spring fixed head 6, support arm 7, pitching ladder axle sleeve 9, realize the elevating movement of parabolic antenna front 10; When parabolic antenna front 10 moved to predetermined angular, because Harmonic Gears does not have auto-lock function, under Action of Gravity Field, parabolic antenna front 10 is motion down; At this moment, rotation degree of tightness handwheel 1, allow the end face close contact of its end face and pitching ladder axle sleeve 9, and produce certain frictional force, thereby it is locking to realize that antenna pitching moves.
The utility model not detailed description is known to the skilled person technology.

Claims (4)

1. a satellite antenna elevating gear, is characterized in that: comprise stepping motor (28), harmonic gear transmission device, degree of tightness handwheel (1), slack adjuster (2), pitching middle (center) bearing end cap (22), pitching major axis (24), pitching motor end cap (29), outside protective covers (30), base (34), lifting screw (35), lifting handwheel (36) and pitching minor axis (37), harmonic gear transmission device is symmetrically distributed in the two ends of stepping motor (28) by the output shaft at stepping motor (28) two ends, harmonic gear transmission device comprises circlip for shaft (3), little end ring I (4), little end ring II (5), air spring fixed head (6) for the fixed air spring, support arm (7) for the supporting antenna front, pitching ladder axle sleeve (9), parabolic antenna front (10), the first deep groove ball bearing (11), the large bearing (ball) cover of pitching (12), pitching flexbile gear connecting plate (14), the second deep groove ball bearing (15), harmonic gear reducer assembly (16), key (19), little axle sleeve (20), the 3rd deep groove ball bearing (21), shaft coupling (25), spacer shell (27),
Described harmonic gear reducer assembly (16) comprises wave producer (41), flexbile gear (43) and has just taken turns (42); Wave producer (41) is connected by key (19) with pitching major axis (24), pitching minor axis (37), and by the shaft shoulder of pitching major axis (24) and pitching minor axis (37), and the shaft orientation moving range of little axle sleeve (20), the 3rd deep groove ball bearing (21), pitching middle (center) bearing end cap (22), pitching motor end cap (29) constraint wave producer (41); Pitching middle (center) bearing end cap (22), pitching motor end cap (29) are fixedly connected with base (34) respectively; Just wheel (42) is fixedly connected with base (34); Pitching flexbile gear connecting plate (14), parabolic antenna front (10), air spring fixed head (6), pitching ladder axle sleeve (9) all are fixedly connected on flexbile gear (43);
The first deep groove ball bearing (11) Internal and external cycle respectively with pitching major axis (24), pitching ladder axle sleeve (9) matched in clearance, and the shaft orientation moving range of the shaft shoulder by pitching major axis (24), little end ring I (4), little end ring II (5) constraint the first deep groove ball bearing (11); Support arm (7) and pitching ladder axle sleeve (9) outer ring matched in clearance, and to support arm (7), carry out spacing by the gentle spring dead plate of circlip for shaft (3) (6);
The second deep groove ball bearing (15) inner ring and pitching flexbile gear connecting plate (14) interference fit, the second deep groove ball bearing (15) outer ring and base (34) matched in clearance, and by the shaft orientation moving range of the large bearing (ball) cover of pitching (12) constraint the second deep groove ball bearing (15);
Stepping motor (28) is fixedly connected with base (34) by pitching motor end cap (29), the output shaft at stepping motor (28) two ends is fixedly connected with pitching major axis (24), pitching minor axis (37) respectively with spacer shell (27) by shaft coupling (25), and, by the transmission of harmonic gear reducer assembly (16), realize the drive connection between stepping motor (28) and parabolic antenna front (10); Described spacer shell (27) is the axle sleeve that is connected between pitching major axis (24) and stepping motor (28) output shaft;
Be used for preventing dust and be fixedly connected with base (34) with the outside protective covers (30) of protective effect;
One end of pitching minor axis (37) is fixedly connected with stepping motor (28), and the other end of pitching minor axis (37) is fixedly connected with lifting handwheel (36), utilizes lifting handwheel (36) manually to adjust the pitching transmission of parabolic antenna front (10);
One end of pitching major axis (24) is fixedly connected with stepping motor (28), and the other end of pitching major axis (24) is threaded with degree of tightness handwheel (1), rotates degree of tightness handwheel (1) the pitching transmission of parabolic antenna front (10) is carried out to locking control.
2. a kind of satellite antenna elevating gear according to claim 1, it is characterized in that: described the first deep groove ball bearing (11) is selected deep groove ball bearing 6700.
3. a kind of satellite antenna elevating gear according to claim 1, it is characterized in that: described the second deep groove ball bearing (15) is selected deep groove ball bearing 61911.
4. a kind of satellite antenna elevating gear according to claim 1, it is characterized in that: described the 3rd deep groove ball bearing (21) is selected deep groove ball bearing 61801.
CN2013202539597U 2013-05-10 2013-05-10 Satellite antenna elevation transmission device Expired - Fee Related CN203300802U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013202539597U CN203300802U (en) 2013-05-10 2013-05-10 Satellite antenna elevation transmission device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013202539597U CN203300802U (en) 2013-05-10 2013-05-10 Satellite antenna elevation transmission device

Publications (1)

Publication Number Publication Date
CN203300802U true CN203300802U (en) 2013-11-20

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104477418A (en) * 2014-12-26 2015-04-01 中国科学院空间科学与应用研究中心 Limiting sliding fixing device
CN106025552A (en) * 2016-07-05 2016-10-12 中国电子科技集团公司第五十四研究所 Large-scale half-rotary-table antenna with high-precision posture adjustment apparatus
CN107329493A (en) * 2017-05-16 2017-11-07 上海卫星工程研究所 Double-vane sun battle array Direct to the sun drive device applied to networking moonlet
CN110600853A (en) * 2019-10-27 2019-12-20 江西中船航海仪器有限公司 Novel antenna winding and unwinding device
CN111044980A (en) * 2019-12-13 2020-04-21 中国航空工业集团公司北京航空精密机械研究所 Pitching device for simulating flight attitude

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104477418A (en) * 2014-12-26 2015-04-01 中国科学院空间科学与应用研究中心 Limiting sliding fixing device
CN106025552A (en) * 2016-07-05 2016-10-12 中国电子科技集团公司第五十四研究所 Large-scale half-rotary-table antenna with high-precision posture adjustment apparatus
CN107329493A (en) * 2017-05-16 2017-11-07 上海卫星工程研究所 Double-vane sun battle array Direct to the sun drive device applied to networking moonlet
CN110600853A (en) * 2019-10-27 2019-12-20 江西中船航海仪器有限公司 Novel antenna winding and unwinding device
CN110600853B (en) * 2019-10-27 2024-04-05 江西中船航海仪器有限公司 Novel antenna winding and unwinding device
CN111044980A (en) * 2019-12-13 2020-04-21 中国航空工业集团公司北京航空精密机械研究所 Pitching device for simulating flight attitude
CN111044980B (en) * 2019-12-13 2023-07-07 中国航空工业集团公司北京航空精密机械研究所 Pitching device for simulating flight attitude

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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: 20131120

Termination date: 20170510