CN107521667A - A kind of two-output impulse generator operating mechanism - Google Patents
A kind of two-output impulse generator operating mechanism Download PDFInfo
- Publication number
- CN107521667A CN107521667A CN201710596902.XA CN201710596902A CN107521667A CN 107521667 A CN107521667 A CN 107521667A CN 201710596902 A CN201710596902 A CN 201710596902A CN 107521667 A CN107521667 A CN 107521667A
- Authority
- CN
- China
- Prior art keywords
- rocking arm
- sleeve
- rotating shaft
- operating mechanism
- impulse generator
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
The invention discloses a kind of two-output impulse generator operating mechanism, belong to mechanical rotation technical field.The mechanism includes the first rocking arm (1), second rocking arm (2), rotating shaft (3), first rotational sleeve (6) and the second rotational sleeve (7), the end of first rocking arm (1) and the second rocking arm (2) is provided with through hole, and two rotational sleeves are fixed respectively, it is coaxial afterwards to be socketed in rotating shaft (3), fixes sleeve (4) is socketed in the rotating shaft (3), first input end and the first output end are provided with first rocking arm (1), the second input and the second output end are provided with second rocking arm (2), the first input end is connected driving structure respectively with second input, first output end is connected driven-mechanism respectively with second output end.The present invention is designed by two-output impulse generator operating mechanism and type of attachment realizes the purpose of steerable system two-output impulse generator.
Description
Technical field
The invention belongs to mechanical rotation technical field, and in particular to a kind of two-output impulse generator operating mechanism.
Background technology
Often due to the limitation of space structure, the design and installation to steerable system propose very high want in airplane design
Ask.Especially steerable system linear system it is very long in the case of (such as vertical, heading system), for example, being indulged in unmanned plane, heading system installation
Space is limited, and intensity deficiency in end where vertical, directional control system, and actuator can not install horizontal tail and rudder rudder face is attached
Closely, directly drive in the steering force output problem of rudder face and the steerable system based on machinery, generally require to meet design requirement
And the mechanism of installing space can be reduced.
The content of the invention
In order to solve the above problems, the present invention proposes a kind of dual input lose-lose for realizing that steerable system installing space is limited
Go out operating mechanism, realize in the case where installing space is limited solve the problems, such as steerable system two directions' inputing bidirectional output.
Two-output impulse generator operating mechanism of the present invention, including the first rocking arm, the second rocking arm, rotating shaft, fixes sleeve, adapter sleeve
The end of cylinder, the first rotational sleeve and the second rotational sleeve, the first rocking arm and the second rocking arm is provided with through hole, and coaxial peace
In rotating shaft, fixes sleeve is socketed in the rotating shaft, and what branch sleeve was socketed in the fixes sleeve is located at the first rocking arm
On part between the second rocking arm, the first rotational sleeve is fixedly connected with the first rocking arm, and is socketed in not covering for fixes sleeve
One of end of branch sleeve is connect, the second rotational sleeve is fixedly connected with the second rocking arm, and is socketed in fixes sleeve not
The other end of branch sleeve is socketed, is provided with first input end and the first output end on first rocking arm, described second shakes
The second input and the second output end are provided with arm, the first input end is connected driving knot with second input respectively
Structure, first output end are connected driven-mechanism respectively with second output end.
Preferably, branch sleeve coordinates with fixes sleeve gap.
Preferably, the first rotational sleeve and the first rocking arm rivet.
Preferably, the second rotational sleeve and the second rocking arm rivet.
Preferably, it is provided with gap between branch sleeve and the first rotational sleeve.
Preferably, it is provided with gap between branch sleeve and the second rotational sleeve.
Preferably, first rocking arm and the second rocking arm are all provided with being set to bending, when by first rocking arm and second
When rocking arm is connected by rotating shaft, the bending direction of first rocking arm is opposite with the bending direction of the second rocking arm.
The present invention is designed by two-output impulse generator operating mechanism and type of attachment realizes steerable system dual input lose-lose
The purpose gone out, solve because structure limitation can not be in two ends of steerable system while the defects of arrange drive device, lose-lose
The installation for entering dual output operating mechanism occupies little space, in light weight, and realizes preferable maintainability.
Brief description of the drawings
Fig. 1 is the structural representation according to a preferred embodiment of two-output impulse generator operating mechanism of the present invention.
Fig. 2 is the front view of embodiment illustrated in fig. 1 of the present invention.
Wherein, 1 is the first rocking arm, and 2 be the second rocking arm, and 3 be rotating shaft, and 4 be fixes sleeve, and 5 be branch sleeve, and 6 be first
Rotational sleeve, 7 be the second rotational sleeve, and 8 be support.
Embodiment
To make the purpose, technical scheme and advantage that the present invention is implemented clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or class
As label represent same or similar element or the element with same or like function.Described embodiment is the present invention
Part of the embodiment, rather than whole embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to uses
It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.Under
Embodiments of the invention are described in detail with reference to accompanying drawing for face.
In the description of the invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outer " is based on accompanying drawing institutes
The orientation or position relationship shown, it is for only for ease of the description present invention and simplifies description, rather than instruction or the dress for implying meaning
Put or element there must be specific orientation, with specific azimuth configuration and operation, therefore it is not intended that the present invention is protected
The limitation of scope.
The present invention proposes a kind of two-output impulse generator operating mechanism, as shown in Figures 1 and 2, mainly includes the first rocking arm
1st, the second rocking arm 2, rotating shaft 3, fixes sleeve 4, branch sleeve 5, the first rotational sleeve 6 and the second rotational sleeve 7, the first rocking arm
1 and second the end of rocking arm 2 be provided with through hole, and be coaxially mounted in rotating shaft 3, fixes sleeve 4 is socketed in the rotating shaft 3
On, branch sleeve 5 is socketed on the part between the first rocking arm and the second rocking arm of the fixes sleeve 4, and first rotates
Sleeve 6 is fixedly connected with the first rocking arm 1, and is socketed in the one of end for not being socketed branch sleeve 5 of fixes sleeve 4, the
Two rotational sleeves 7 are fixedly connected with the second rocking arm 2, and are socketed in the other end for not being socketed branch sleeve 5 of fixes sleeve 4,
First input end and the first output end are provided with first rocking arm 1, be provided with second rocking arm 2 second input with
Second output end, the first input end are connected driving structure, first output end and institute respectively with second input
State the second output end and connect driven-mechanism respectively.
With reference to figure 2, the first rocking arm 1 and the second rocking arm 2 are arcuate structure, and rotating shaft 3 is generally located on the end of two rocking arms,
Therefore, in the end correspondence position opened hole of the first rocking arm 1 and the second rocking arm 2, to install rotating shaft 3, in alternate embodiment,
The optional position for two rocking arms that rotating shaft 3 can install, for example, in 2 middle opened hole of the first rocking arm 1 and the second rocking arm, and lead to
Cross rotating shaft 3 to connect, now, first input end is separated with the first output end by the through hole of first rocking arm 1, and similarly, second is defeated
Enter end to be separated by the through hole of the second rocking arm 2 with the second output end.
It is appreciated that above-mentioned input or the Tiebar structure that input is steerable system, such as the ears piece knot in diagram
Structure, the ears piece pass through in hinge and rocking arm.
In the present embodiment, rotating shaft 3 can pass through the through hole of the above-mentioned rocking arm 2 of first rocking arm 1 and second, and in the first rocking arm 1
And the outer end of the second rocking arm 2 is provided with fixture, fixture is such as can be nut, fuse, to prevent the first rocking arm or
Skidded off on the two rocking arm axis of rotation 3.
To reduce the pivoting friction between rotating shaft and rocking arm, bearing connected mode can be used, in the present embodiment, more
Be to consider economy and convertibility, therefore, taking following measure in the present embodiment：
First it is arranged fixes sleeve 4 in rotating shaft 3, fixes sleeve 4 is divided for three parts, and center section and both ends can be worn
Two end sections of through hole on rocking arm are crossed, afterwards, branch sleeve 5 are arranged on the center section of fixes sleeve 4, in fixed cover
Rotational sleeve, i.e. the first rotational sleeve 6 and the second rotational sleeve 7 are arranged with the end part of cylinder 4.Wherein, the first rotational sleeve 6
It is fixedly connected with the first rocking arm 1, the second rotational sleeve 7 is fixedly connected with the second rocking arm 2.So, rotating shaft 3 includes being set in rotating shaft
Fixes sleeve 4 outside 3 will rotate relative to the first rotational sleeve 6 and the second rotational sleeve 7, and branch sleeve 5 is used to prevent
Only two rocking arms are drawn close to centre.It is understood that the first rotational sleeve 6 and the second rotational sleeve 7 and branch sleeve 5 is interior
External diameter should be close, the problem of being not in mutually nested, it can also be appreciated that the first rotational sleeve 6 and second rotates
The end of rotating shaft 3, and the structure limitation that the external diameter such as nut by the end of rotating shaft 3 is larger, such as first turn are pressed close in the outer end of sleeve 7
The internal diameter of moving sleeve 6 is less than the external diameter of the nut, and so, motion of two rocking arms on the axis direction of rotating shaft is limited,
It is only capable of relative to axis of rotation.
In the present embodiment, branch sleeve 5 coordinates with the gap of fixes sleeve 4, prevents because the reason such as both interference fits
Two rocking arm relative motions are made to be obstructed.
In the present embodiment, the first rotational sleeve 6 rivets with the first rocking arm 1, similarly, the second rotational sleeve 7 and the second rocking arm 2
Riveting.With specific reference to Fig. 1, by the first rotational sleeve 6 and the first rocking arm 1 it is be hinged exemplified by, the first rotational sleeve includes two parts,
The Part I of through hole on the first rocking arm 1 can be passed through, this segment outer radius is less than the through hole, and more described logical including external diameter
The big Part II of hole internal diameter, it is possible to understand that Part I forms step with Part II, and the step surface is adjacent in the first rocking arm 1
Outer face on, and with outer face rivet.It should be noted that the outer face of above-mentioned first rocking arm 1 refers to that the first rocking arm deviates from
The one side of second rocking arm, corresponding, it turns into inner face towards the one side of the second rocking arm.
In alternative, the step surface can be arranged on the inner face of the first rocking arm, and is riveted with inner face.
In the present embodiment, branch sleeve 5 coordinates with the gap of fixes sleeve 4, between the rotational sleeve 6 of branch sleeve 5 and first
Gap is provided with, gap is provided between the rotational sleeve 7 of branch sleeve 5 and second.It is understood that above-mentioned gap or gap
The connected mode of cooperation is used to ensure that the rotation between two rocking arms is more smooth smooth.
In the present embodiment, with reference to figure 1, the rocking arm 2 of the first rocking arm 1 and second is all provided with being set to bending, when by described
When one rocking arm 1 is connected with the second rocking arm 2 by rotating shaft 3, the bending side of the bending direction of first rocking arm 1 and the second rocking arm 2
To opposite.Two inputs are arranged on the side of whole operating mechanism, and two output ends are arranged on the another of whole operating mechanism
Side.
Present invention additionally comprises support 8, for fixed rotating shaft 3.Support 8 is section bar, the fixture at the both ends of rotating shaft 3 it is another
One purpose is rotating shaft 3 being fixed on support 8.So, in the present embodiment, fixes sleeve 4 and the tight fit of rotating shaft 3
Connection, so that rotating shaft 3 and fixes sleeve are relatively motionless, rotational sleeve and/or branch sleeve relative motion on the outside of it.
In the present embodiment, two rotational sleeve materials are identical, and its Material Strength is more than the Material Strength of fixes sleeve 4,
Replacing after being worn for a long time with realization to fixes sleeve 4, is easy to system maintenance.
It is last it is to be noted that：The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations.To the greatest extent
The present invention is described in detail with reference to the foregoing embodiments for pipe, it will be understood by those within the art that：It is still
Technical scheme described in foregoing embodiments can be modified, or which part technical characteristic is equally replaced
Change；And these modifications or replacement, the essence of appropriate technical solution is departed from the essence of various embodiments of the present invention technical scheme
God and scope.
Claims (7)
1. a kind of two-output impulse generator operating mechanism, it is characterised in that including the first rocking arm (1), the second rocking arm (2), rotating shaft
(3), fixes sleeve (4), branch sleeve (5), the first rotational sleeve (6) and the second rotational sleeve (7), the first rocking arm (1) with
The end of second rocking arm (2) is provided with through hole, and is coaxially mounted in rotating shaft (3), and fixes sleeve (4) is socketed in the rotating shaft
(3) on, branch sleeve (5) is socketed on the part between the first rocking arm and the second rocking arm of the fixes sleeve (4), the
One rotational sleeve (6) is fixedly connected with the first rocking arm (1), and be socketed in fixes sleeve (4) be not socketed branch sleeve (5) its
In an end, the second rotational sleeve (7) is fixedly connected with the second rocking arm (2), and is socketed in not covering in succession for fixes sleeve (4)
The other end of female connector cylinder (5), first input end and the first output end is provided with first rocking arm (1), described second shakes
The second input and the second output end are provided with arm (2), the first input end is connected drive respectively with second input
Dynamic structure, first output end are connected driven-mechanism respectively with second output end.
2. the environmental control system of electronic equipment forced air cooling as claimed in claim 1, it is characterised in that branch sleeve (5) is with consolidating
Determine the cooperation of sleeve (4) gap.
3. two-output impulse generator operating mechanism as claimed in claim 1, it is characterised in that the first rotational sleeve (6) and first
Rocking arm (1) rivets.
4. two-output impulse generator operating mechanism as claimed in claim 1, it is characterised in that the second rotational sleeve (7) and second
Rocking arm (2) rivets.
5. two-output impulse generator operating mechanism as claimed in claim 1, it is characterised in that branch sleeve (5) rotates with first
Sleeve is provided with gap between (6).
6. two-output impulse generator operating mechanism as claimed in claim 1, it is characterised in that branch sleeve (5) rotates with second
Sleeve is provided with gap between (7).
7. two-output impulse generator operating mechanism as claimed in claim 1, it is characterised in that first rocking arm (1) and second
Rocking arm (2) is all provided with being set to bending, described when first rocking arm (1) is connected with the second rocking arm (2) by rotating shaft (3)
The bending direction of first rocking arm (1) is opposite with the bending direction of the second rocking arm (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710596902.XA CN107521667B (en) | 2017-07-20 | 2017-07-20 | Double-input double-output control mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710596902.XA CN107521667B (en) | 2017-07-20 | 2017-07-20 | Double-input double-output control mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107521667A true CN107521667A (en) | 2017-12-29 |
| CN107521667B CN107521667B (en) | 2021-05-25 |
Family
ID=60748337
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710596902.XA Active CN107521667B (en) | 2017-07-20 | 2017-07-20 | Double-input double-output control mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107521667B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101975008A (en) * | 2010-10-27 | 2011-02-16 | 西安飞机工业（集团）有限责任公司 | Flexible control safety lock mechanism of cabin door |
| CN202657242U (en) * | 2012-11-02 | 2013-01-09 | 中国航空工业集团公司西安飞机设计研究所 | Rocker mechanism |
| CN103318407A (en) * | 2013-06-05 | 2013-09-25 | 王开林 | Standalone control system of coaxial double-rotor unmanned helicopter control system |
| CN104477301A (en) * | 2014-12-29 | 2015-04-01 | 山东大学苏州研究院 | Foldable object-carrier bicycle |
| CN105151280A (en) * | 2015-09-28 | 2015-12-16 | 哈尔滨工业大学深圳研究生院 | Aircraft empennage regulation mechanism with pitching and yawing completely decoupled |
| CN105782359A (en) * | 2014-12-23 | 2016-07-20 | 北京南口轨道交通机械有限责任公司 | Transmission system |
| CN106275502A (en) * | 2016-08-29 | 2017-01-04 | 中国航空工业集团公司西安飞机设计研究所 | A kind of gear test loads vacation wheel |
| CN206125406U (en) * | 2016-10-25 | 2017-04-26 | 深圳创壹通航科技有限公司 | Operating mechanism and gyroplane |
| CN106790851A (en) * | 2016-12-27 | 2017-05-31 | 东莞市联洲知识产权运营管理有限公司 | A kind of handset mounting of adjustable angle |
-
2017
- 2017-07-20 CN CN201710596902.XA patent/CN107521667B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101975008A (en) * | 2010-10-27 | 2011-02-16 | 西安飞机工业（集团）有限责任公司 | Flexible control safety lock mechanism of cabin door |
| CN202657242U (en) * | 2012-11-02 | 2013-01-09 | 中国航空工业集团公司西安飞机设计研究所 | Rocker mechanism |
| CN103318407A (en) * | 2013-06-05 | 2013-09-25 | 王开林 | Standalone control system of coaxial double-rotor unmanned helicopter control system |
| CN105782359A (en) * | 2014-12-23 | 2016-07-20 | 北京南口轨道交通机械有限责任公司 | Transmission system |
| CN104477301A (en) * | 2014-12-29 | 2015-04-01 | 山东大学苏州研究院 | Foldable object-carrier bicycle |
| CN105151280A (en) * | 2015-09-28 | 2015-12-16 | 哈尔滨工业大学深圳研究生院 | Aircraft empennage regulation mechanism with pitching and yawing completely decoupled |
| CN106275502A (en) * | 2016-08-29 | 2017-01-04 | 中国航空工业集团公司西安飞机设计研究所 | A kind of gear test loads vacation wheel |
| CN206125406U (en) * | 2016-10-25 | 2017-04-26 | 深圳创壹通航科技有限公司 | Operating mechanism and gyroplane |
| CN106790851A (en) * | 2016-12-27 | 2017-05-31 | 东莞市联洲知识产权运营管理有限公司 | A kind of handset mounting of adjustable angle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107521667B (en) | 2021-05-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102658865B (en) | Coaxial drive and control structure for coaxial contrarotation rotor helicopter | |
| CN105292469B (en) | Control system for controlling total pitch of many each blades of blade rotor and cyclicpiston in rotor craft | |
| KR101683325B1 (en) | articulated robot wrist | |
| CN106741870B (en) | A kind of cockpit steerable system and method | |
| CN105173066A (en) | Electrically-driven nose wheel steering device for unmanned aerial vehicle | |
| US9669923B2 (en) | Rotor blade control device | |
| US11077934B2 (en) | Aircraft, control surface arrangements, and methods of assembling an aircraft | |
| WO2009023941A3 (en) | Aircraft flight control systems and methods | |
| CN103600834A (en) | Airplane hatch door quick-release mechanism capable of realizing wide-angle overturn | |
| CN108528711A (en) | The flapping wings of a kind of variable amplitude and pitch angle are fluttered structure | |
| CN104454961A (en) | In-tension equivalent composite spherical hinge | |
| CN208530834U (en) | A kind of light aerocraft aileron control device | |
| CN104290901A (en) | Double-rocker transmission mechanism applicable to movable control surface of aerial vehicle | |
| CN110356544B (en) | Airplane side rod control device and airplane with same | |
| CN104647364B (en) | A kind of reconfigurable drag articulation type four axle robots | |
| WO2018120416A1 (en) | Steering wiring structure of humanoid robot, and humanoid robot | |
| CN111891336A (en) | Variable-configuration control surface for realizing composite control of airplane | |
| CN206476096U (en) | A kind of light aerocraft Aileron control system | |
| CN107512385A (en) | A kind of unmanned plane longitudinal-control system | |
| CN107521667A (en) | A kind of two-output impulse generator operating mechanism | |
| KR20100133808A (en) | Uninhabited aerial vehicle having improved structure of wing installition | |
| US9751637B2 (en) | Exterior helicopter light unit and method of operating an exterior helicopter light unit | |
| CN206171794U (en) | Light aircraft elevator hybrid control system | |
| US20090136351A1 (en) | Tail Rotor Hub | |
| CN209467317U (en) | For balancing the drag link transmission mechanism and helicopter of reaction torque |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |