CN204279923U - A kind of rudder face manipulation module mounting structure - Google Patents
A kind of rudder face manipulation module mounting structure Download PDFInfo
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- CN204279923U CN204279923U CN201420755523.2U CN201420755523U CN204279923U CN 204279923 U CN204279923 U CN 204279923U CN 201420755523 U CN201420755523 U CN 201420755523U CN 204279923 U CN204279923 U CN 204279923U
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- rudderpost
- bearing
- rudder face
- utility
- mounting base
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Abstract
The utility model relates to cruising missile control field, is specifically related to a kind of rudder face manipulation module mounting structure.Comprise bearing mounting base, bearing set, rudderpost and rocking arm, bearing set is arranged in bearing mounting base, and bearing set installs rudderpost, and rudderpost is fixedly connected with rocking arm, and rocking arm is connected with steering wheel, and rudderpost is connected with rudder face.Bearing set interference fit is arranged in bearing mounting base.The beneficial effects of the utility model are: the utility model compact conformation, take full advantage of space limited in body; Modular design, interchangeability is high, improves setting accuracy and dismounting efficiency.
Description
Technical field
The utility model relates to cruising missile control field, is specifically related to a kind of rudder face manipulation module mounting structure.
Background technology
Steering unit is a set of mechanical drive between steering wheel to controlsurface rotating shaft.Radical function has 2 points: one is make controlsurface (rudder, aileron, rotation missile wing) produce the angle of rotation corresponding to steering wheel displacement; Two is transmit steering wheel moment, in order to the hinge moment of balanced surface.It is the necessary integral link of guided missile autonomous cruise speed system, is again a component part of body.Under normal circumstances, rudder face steering unit is directly assemblied on stronger part (as shell of the projectile body reinforcing frame), the defect of this installation form has: 1. because the rolling bearing of rudder face generally adopts the assembling mode of interference fit, steering unit is caused to there is certain difficulty when dismounting, particularly when dismantling bearing, original assembly precision can be destroyed; 2. directly process on shell of the projectile body due to erection support and make, working accuracy and stress released-deformation etc. all can directly have an impact to rudder face positional precision.
Summary of the invention
The purpose of this utility model is to solve the problem, and provides a kind of rudder face manipulation module mounting structure.
In order to realize the purpose of this utility model, the technical solution adopted in the utility model is:
A kind of rudder face manipulation module mounting structure, comprise bearing mounting base, bearing set, rudderpost and rocking arm, bearing set is arranged in bearing mounting base, and bearing set installs rudderpost, and rudderpost is fixedly connected with rocking arm, and rocking arm is connected with steering wheel, and rudderpost is connected with rudder face.
Bearing set interference fit is arranged in bearing mounting base.
The beneficial effects of the utility model are: compact conformation of the present invention, take full advantage of space limited in body; Modular design, interchangeability is high, improves setting accuracy and dismounting efficiency.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation,
Fig. 2 is the structural representation after the utility model is installed.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further illustrated:
Embodiment: see Fig. 1, Fig. 2.
A kind of rudder face manipulation module mounting structure, comprise bearing mounting base 1, bearing set 3, rudderpost 2 and Rocker arm 4, bearing set 3 is arranged in bearing mounting base 1, bearing set 3 is installed rudderpost 2, rudderpost 2 is fixedly connected with Rocker arm 4, and Rocker arm 4 is connected with steering wheel 5, and rudderpost 2 is connected with rudder face 6.
Bearing set 3 interference fit is arranged in bearing mounting base 1.
One of preferred embodiment that what embodiment of the present utility model was announced is also; but be not limited thereto; those of ordinary skill in the art; very easily according to above-described embodiment; understand spirit of the present utility model; and make different amplifications and change, but only otherwise depart from spirit of the present utility model, all in protection domain of the present utility model.
Claims (2)
1. a rudder face manipulation module mounting structure, is characterized in that: comprise bearing mounting base, bearing set, rudderpost and rocking arm, and bearing set is arranged in bearing mounting base, bearing set installs rudderpost, rudderpost is fixedly connected with rocking arm, and rocking arm is connected with steering wheel, and rudderpost is connected with rudder face.
2. a kind of rudder face manipulation module mounting structure according to claim 1, is characterized in that: bearing set interference fit is arranged in bearing mounting base.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201420755523.2U CN204279923U (en) | 2014-12-05 | 2014-12-05 | A kind of rudder face manipulation module mounting structure |
Applications Claiming Priority (1)
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CN201420755523.2U CN204279923U (en) | 2014-12-05 | 2014-12-05 | A kind of rudder face manipulation module mounting structure |
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CN204279923U true CN204279923U (en) | 2015-04-22 |
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CN201420755523.2U Active CN204279923U (en) | 2014-12-05 | 2014-12-05 | A kind of rudder face manipulation module mounting structure |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107882884A (en) * | 2016-09-30 | 2018-04-06 | 北京自动化控制设备研究所 | A kind of limited angle of oscillation combination bearing |
CN108318211A (en) * | 2018-01-21 | 2018-07-24 | 南京航空航天大学 | A kind of high-speed wind tunnel rotating model simultaneous test device |
CN108583932A (en) * | 2018-01-21 | 2018-09-28 | 南京航空航天大学 | A kind of rudder face of adjustable deflection angle beats executive device partially |
CN110979641A (en) * | 2019-11-28 | 2020-04-10 | 北京自动化控制设备研究所 | Rudder shaft supporting mechanism based on crossed roller bearing |
CN113978704A (en) * | 2021-12-17 | 2022-01-28 | 江西洪都航空工业集团有限责任公司 | Steering engine installation device |
-
2014
- 2014-12-05 CN CN201420755523.2U patent/CN204279923U/en active Active
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107882884A (en) * | 2016-09-30 | 2018-04-06 | 北京自动化控制设备研究所 | A kind of limited angle of oscillation combination bearing |
CN107882884B (en) * | 2016-09-30 | 2019-09-13 | 北京自动化控制设备研究所 | A kind of limited angle of oscillation combination bearing |
CN108318211A (en) * | 2018-01-21 | 2018-07-24 | 南京航空航天大学 | A kind of high-speed wind tunnel rotating model simultaneous test device |
CN108583932A (en) * | 2018-01-21 | 2018-09-28 | 南京航空航天大学 | A kind of rudder face of adjustable deflection angle beats executive device partially |
CN110979641A (en) * | 2019-11-28 | 2020-04-10 | 北京自动化控制设备研究所 | Rudder shaft supporting mechanism based on crossed roller bearing |
CN110979641B (en) * | 2019-11-28 | 2021-02-05 | 北京自动化控制设备研究所 | Rudder shaft supporting mechanism based on crossed roller bearing |
CN113978704A (en) * | 2021-12-17 | 2022-01-28 | 江西洪都航空工业集团有限责任公司 | Steering engine installation device |
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