CN107933893A - A kind of propeller phase lock mechanism - Google Patents
A kind of propeller phase lock mechanism Download PDFInfo
- Publication number
- CN107933893A CN107933893A CN201711228721.8A CN201711228721A CN107933893A CN 107933893 A CN107933893 A CN 107933893A CN 201711228721 A CN201711228721 A CN 201711228721A CN 107933893 A CN107933893 A CN 107933893A
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- CN
- China
- Prior art keywords
- propeller
- guide pin
- guide
- connecting rod
- rod
- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
The present invention discloses a kind of propeller phase lock mechanism, including start steering engine, guide groove, guide rod and fusiformis guide pin.Wherein, fusiformis guide pin is installed on propeller motor output shaft；Middle part relative side is straight flange, as spacing cooperation side.The rotary motion of itself output shaft is changed into linear motion by start steering engine by multi-connecting-rod mechanism, drives guide rod to move up and down in guide groove；When the upward motion contact of guide rod is to guide pin, driving guide pin rotation, so as to drive propeller rotational by machine shaft, when guide rod is bonded with the spacing cooperation side of guide pin, guide pin and propeller stop operating, and propeller phase is locked.Propeller phase lock mechanism reliability of the present invention is high, lightweight construction, it is easy to accomplish, it is of low cost, meet requirement of the variation diving aircraft to propeller PGC demodulation.
Description
Technical field
The invention belongs to field of flight vehicle design, specifically devises a kind of propeller phase lock mechanism.
Background technology
Conventional aircraft flies in atmosphere, its dynamical system propeller etc. is usually changeless, and diving flies
Machine will not only navigate by water in atmosphere, also navigate by water in water.More than 800 times of the density difference of air and water, becomes diving aircraft in sky
The flow dynamics that gas is neutralized in water differ greatly.Under the conditions of current technology, diving aircraft navigates by water under water and sky
Middle navigation cannot use same set of dynamical system.Therefore for the requirement for meeting to navigate by water with navigate by water in water in the air at the same time, diving
Aircraft needs suitably to change configuration.In view of water takeoff and the requirement of aerial navigation, the propeller for aerial power
When needing to be placed in outside fuselage, and navigating by water under water, which needs to be accommodated in fuselage, to reduce the resistance of underwater navigation
Power.In order to enable propeller to be accommodated in fuselage, it is necessary to which propeller is fixed on a certain phase.
The content of the invention
To solve the above problems, the present invention proposes a kind of propeller phase lock mechanism, meet diving aircraft storage spiral shell
Requirement when revolving paddle to locking screw paddle phase.
Propeller phase lock mechanism of the present invention, guide pin is fixedly mounted on propeller motor；Guide pin is shuttle-type knot
Structure, middle part opposite sides are straight flange, as spacing cooperation side, coordinate with the guide rod of elongation and realize that propeller motor exports
The rotation limitation of axis.Guide rod is driven by start servo driving, and multi-connecting-rod mechanism is driven the rotation of start steering engine output shaft
Movement is changed into linear motion, drives the stretching motion in guide sleeve.
When the upward motion contact of guide rod is to guide pin, driving guide pin rotation, so as to drive spiral shell by machine shaft
Revolve paddle to rotate, when guide rod is bonded with the spacing cooperation side of guide pin, guide pin and propeller stop operating, propeller
Phase is locked.
The advantage of the invention is that：
1st, propeller phase lock mechanism of the present invention, guide rod is not by the shaft of fusiformis guide pin, during start
Without dead point.
2nd, propeller phase lock mechanism of the present invention, it is versatile, it can apply to most motor helical paddle phase locks
It is fixed.
3rd, propeller phase lock mechanism of the present invention, reliable stabilization, lightweight construction are of low cost.
Brief description of the drawings
Fig. 1 is propeller phase lock mechanism overall schematic of the present invention；
Fig. 2 is guide pin structure diagram in propeller phase lock mechanism of the present invention；
Schematic diagram when Fig. 3 is propeller phase lock mechanism locking screw paddle phase of the present invention；
In figure：
1- guide pin 2- motor rack 3- start steering engines
4- pilot sleeve 5- guide rod 6- multi-jointed gear units
7- propeller motor 8- propeller 101- center sections
The spacing cooperation sides of 102- left half 103- right halfs 104-
601- steering engine rocking arm 602- first connecting rod 603- second connecting rods
604- third connecting rods
Embodiment
Specifically name is done further to the present invention below in conjunction with the accompanying drawings.
Propeller phase lock mechanism of the present invention, including guide pin 1, motor rack 2, start steering engine 3, pilot sleeve 4, lead
To bar 5 and multi-jointed gear unit 6, as shown in Figure 1.
The guide pin 1 has center section 101, left half 102 and right half 103, as shown in Figure 2.Wherein, it is middle
Part 101 for rectangle up and down side be limited position coordinate side 104, left and right side respectively with 103 phase of left half 102 and right half
Connect.Left half 102 and 103 symmetrical configuration of right half, are the triangle of end taper；Thus it is in fusiformis knot to make overall guide pin 1
Structure.Guide pin 1 is connected by the perforate on 101 center of center section and is installed in the shaft of propeller motor 7；Then
Propeller 8 also is secured in the shaft of propeller motor 7, and make the center section of guide pin 1 about 101 side parallel to
The blade of propeller 8.Above-mentioned propeller motor 7 is supported fixation by the motor support 201 of 2 top design of motor rack, makes spiral shell
7 output shaft of rotation paddle motor is set along horizontal x-axis direction.
3 output shaft of start steering engine is set along space y-axis direction, is fixedly installed in the left and right of 2 lower part of motor rack design
Side sheet room, positioned at 7 lower rear position of propeller motor.
The guide rod 5 is placed in being set along vertical z-axis direction along pilot sleeve 4 for motor rack top installation；Pilot sleeve
4 are located at 7 lower front of propeller motor, and are in 1 position directly below of guide pin.
The multi-connecting-rod mechanism 6 is used for connecting start steering engine 3 and guide rod 5, by multi-connecting-rod mechanism 6 by start steering engine 3
The rotary motion of output shaft is changed into linear motion, drives guide rod 5 to move up and down in pilot sleeve 4.
The multi-connecting-rod mechanism 6 includes steering engine rocking arm 601, first connecting rod 602, second connecting rod 603 and third connecting rod 604.
Wherein, 601 input terminal of steering engine rocking arm is fixedly installed on 3 output shaft of start steering engine；601 output terminal of steering engine rocking arm and first connects
602 input terminal of bar is hinged, and 602 output terminal of first connecting rod is hinged with 603 input terminal of second connecting rod；603 output terminal of second connecting rod with
604 input terminal of third connecting rod is hinged, and 604 output terminal of third connecting rod is hinged with 5 bottom of guide rod.The axis of above-mentioned each articulated shaft
Along the y-axis direction, and wherein 603 center of second connecting rod is connected on 2 lower part side plate of motor rack by shaft, is formed and turned
Dynamic pair.
After propeller 8 stalls, guide rod 5 is driven to move upwards by start steering engine 3,5 upward motion process of guide rod
In, top touches 1 side wall of guide pin first, promotes guide pin 1 to rotate by guide rod 5 at this time, so as to pass through propeller motor
7 shaft drives propeller 8 to rotate.It is subsequently directed to bar 5 to continue to move up, is eventually led to 5 side wall of bar and 1 center section of guide pin
Side wall is close to, and guide pin 1 and propeller 8 stop operating at this time, and 8 phase of propeller is locked, as shown in Figure 3；Propeller at this time
8 blade is along the z-axis direction.In the above process, the movement of guide rod 5 is not by the shaft of guide pin 1, so that in start process
In avoid dead point.
Claims (4)
- A kind of 1. propeller phase lock mechanism, it is characterised in that：Guide pin is fixedly mounted on propeller motor；In guide pin Portion's opposite sides is straight flange, as spacing cooperation side, coordinates with the guide rod of elongation and realizes turning for propeller motor output shaft Dynamic limitation.
- A kind of 2. propeller phase lock mechanism as claimed in claim 1, it is characterised in that：Guide pin be with center section, Left half and right half；Wherein, center section for rectangle up and down side be limited position coordinate side, left and right side respectively with left half Connect with right half；Left half and right half symmetrical configuration, are the triangle of end taper, it is in fusiformis knot to make overall guide pin Structure.
- A kind of 3. propeller phase lock mechanism as claimed in claim 1, it is characterised in that：Guide rod passes through start servo driving The rotary motion of start steering engine output shaft is changed into linear motion, drives stretching in guide sleeve by driving, multi-connecting-rod mechanism transmission Contracting movement.
- A kind of 4. propeller phase lock mechanism as claimed in claim 3, it is characterised in that：Multi-connecting-rod mechanism shakes including steering engine Arm, first connecting rod, second connecting rod and third connecting rod；Wherein, steering engine rocking arm input terminal is fixedly installed on start steering engine output shaft； Steering engine rocking arm output terminal is hinged with first connecting rod input terminal, and first connecting rod output terminal is hinged with second connecting rod input terminal；Second connects Bar output terminal is hinged with third connecting rod input terminal, and third connecting rod output terminal is hinged with guide rod bottom；And wherein in second connecting rod Heart position is connected on the side plate of motor rack lower part by shaft, forms revolute pair.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711228721.8A CN107933893A (en) | 2017-11-29 | 2017-11-29 | A kind of propeller phase lock mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711228721.8A CN107933893A (en) | 2017-11-29 | 2017-11-29 | A kind of propeller phase lock mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107933893A true CN107933893A (en) | 2018-04-20 |
Family
ID=61946694
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711228721.8A Pending CN107933893A (en) | 2017-11-29 | 2017-11-29 | A kind of propeller phase lock mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107933893A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639311A (en) * | 2018-07-10 | 2018-10-12 | 湖南鲲鹏智汇无人机技术有限公司 | Fly the limiting device of propeller before a kind of complete electric type VTOL fixed-wing unmanned plane |
| CN109703754A (en) * | 2019-01-30 | 2019-05-03 | 拓攻（南京）机器人有限公司 | A kind of locking of propeller mechanism and the Unmanned Aerial Vehicle Powerplants containing it |
| CN110481759A (en) * | 2019-09-18 | 2019-11-22 | 大连理工大学 | A kind of blade allosteric type across medium aircraft |
| WO2020048383A1 (en) * | 2018-09-05 | 2020-03-12 | Ningbo Geely Automobile Research & Development Co., Ltd. | A transmission |
| CN111003153A (en) * | 2019-12-25 | 2020-04-14 | 中国航空工业集团公司西安飞机设计研究所 | Paddle locking device |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2332837A2 (en) * | 2009-12-09 | 2011-06-15 | The Boeing Company | Blade handling apparatus |
| CN106829570A (en) * | 2017-03-13 | 2017-06-13 | 佛山市恒昌达安全印务印刷有限公司 | A kind of benefit paper platform being applied on printing equipment |
| CN107010197A (en) * | 2016-11-22 | 2017-08-04 | 中国人民解放军空军工程大学 | A kind of stationary spiral oar specific direction generation and fixed mechanism |
| CN107352028A (en) * | 2017-08-01 | 2017-11-17 | 禅诺有限公司 | Rotor locking mechanism |
-
2017
- 2017-11-29 CN CN201711228721.8A patent/CN107933893A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2332837A2 (en) * | 2009-12-09 | 2011-06-15 | The Boeing Company | Blade handling apparatus |
| CN107010197A (en) * | 2016-11-22 | 2017-08-04 | 中国人民解放军空军工程大学 | A kind of stationary spiral oar specific direction generation and fixed mechanism |
| CN106829570A (en) * | 2017-03-13 | 2017-06-13 | 佛山市恒昌达安全印务印刷有限公司 | A kind of benefit paper platform being applied on printing equipment |
| CN107352028A (en) * | 2017-08-01 | 2017-11-17 | 禅诺有限公司 | Rotor locking mechanism |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639311A (en) * | 2018-07-10 | 2018-10-12 | 湖南鲲鹏智汇无人机技术有限公司 | Fly the limiting device of propeller before a kind of complete electric type VTOL fixed-wing unmanned plane |
| CN108639311B (en) * | 2018-07-10 | 2020-06-02 | 湖南鲲鹏智汇无人机技术有限公司 | Stop device of full-electric vertical take-off and landing fixed wing unmanned aerial vehicle front flying propeller |
| WO2020048383A1 (en) * | 2018-09-05 | 2020-03-12 | Ningbo Geely Automobile Research & Development Co., Ltd. | A transmission |
| US11982320B2 (en) | 2018-09-05 | 2024-05-14 | Ningbo Geely Automobile Research & Dev. Co., Ltd. | Transmission |
| CN109703754A (en) * | 2019-01-30 | 2019-05-03 | 拓攻（南京）机器人有限公司 | A kind of locking of propeller mechanism and the Unmanned Aerial Vehicle Powerplants containing it |
| CN110481759A (en) * | 2019-09-18 | 2019-11-22 | 大连理工大学 | A kind of blade allosteric type across medium aircraft |
| CN111003153A (en) * | 2019-12-25 | 2020-04-14 | 中国航空工业集团公司西安飞机设计研究所 | Paddle locking device |
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| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180420 |
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| RJ01 | Rejection of invention patent application after publication |