CN104960658A - Tilting device - Google Patents

Tilting device Download PDF

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Publication number
CN104960658A
CN104960658A CN201510430977.1A CN201510430977A CN104960658A CN 104960658 A CN104960658 A CN 104960658A CN 201510430977 A CN201510430977 A CN 201510430977A CN 104960658 A CN104960658 A CN 104960658A
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CN
China
Prior art keywords
reclining device
tiliting axis
bearing plate
stay bearing
axis
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Pending
Application number
CN201510430977.1A
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Chinese (zh)
Inventor
聂营
张泰华
何泽青
黄宛宁
张冬辉
王生
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Academy of Opto Electronics of CAS
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Academy of Opto Electronics of CAS
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Application filed by Academy of Opto Electronics of CAS filed Critical Academy of Opto Electronics of CAS
Priority to CN201510430977.1A priority Critical patent/CN104960658A/en
Publication of CN104960658A publication Critical patent/CN104960658A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a tilting device. The tilting device for an electric vectored thruster comprises a tilting shaft and a driving device, wherein the tilting shaft is used for driving the thruster to do tilting motion; the driving device is used for driving the tilting shaft to rotate; the tilting shaft corresponds to one thruster; the tilting device further comprises a control device used for controlling a working state of the driving device; the driving device is a servo motor; the tilting device further comprises a reduction gear used for reducing rotation speed of the tilting shaft. According to the tilting device provided by the invention, the weight born on the tilting device is reduced, the reliability of the tilting device is improved, and the tilting device can also bear thrusters with greater weights and higher powers; therefore, it is possible to apply high-power thrusters to the technical field of airships.

Description

A kind of reclining device
Technical field
The present invention relates to propulsion system technical field, be specifically related to a kind of reclining device.
Background technology
Dirigible a kind ofly has propelling and the aerostatics of flight control unit, with regard to its structure, generally include be filled with helium hull, be positioned at gondola below hull, play the empennage of stability contorting effect and the propulsion system of power is provided.Dirigible because of its good reliability and safety, and can carry out the feature of spot hover, is widely used in current taking photo by plane, surveys and draws, in the field such as advertisement.
In recent years, along with the enhancing of common people's environmental consciousness and the progress of electronic Push Technology, and the arrival of advection layer altitude research boom, electronic dirigible becomes the focus of current dirigible field of research.Current electronic dirigible, its flying speed is lower, and for improving the handling under its low speed, so in current design, its propulsion system is all the vector propeller adopting band reclining device usually.
In current electronic dirigible structure, vector propeller is generally two, be arranged in the both sides of gondola respectively, reclining device is then placed in gondola inside, and the structure of reclining device mainly includes motor, driving device, the axis that is simultaneously in transmission connection with two vector propellers, is carrying out in manipulation process, stepping motor is rotated by actuator drives axis, axis synchronously drives two vector propellers be attached thereto, and so, realizes synchronously verting to two vector propellers.
In current reclining device structure, axis stage casing is by arranging bearing or other strut members support, the end, two ends of axis is connected with a vector propeller respectively, like this realization coordinates the vector propeller that both ends are arranged that verts, such as Chinese patent application " the high altitude region electric power unwrapping wire Powered Propulsion assembly of electronic dirigible " (number of patent application: CN201220311406.8), it discloses a kind of Powered Propulsion assembly for electronic dirigible, include Linkage steering, propulsion electric machine is connected with at the two ends of Linkage steering, the propulsion electric machine at two ends is driven to rotate the adjustment realizing direction of propulsion by Linkage steering, such as Chinese patent application " Helium Airship duct inclining rotary mechanism " (number of patent application: CN201320012062.5) again, it discloses a kind of Helium Airship duct inclining rotary mechanism, comprise worm couple, for the motor driving the worm screw of this worm couple to rotate, the worm gear of this worm couple is arranged on duct axle, a duct circle is respectively equipped with at duct axle two ends, described motor is connected with driving device worm screw through coupler, described duct circle is built with Helium Airship propelling unit, in this application, worm screw drives worm gear wheel, worm gear drives propelling unit again, such as Chinese patent application " a kind of gravity-center adjustable airship gondola " (number of patent application: CN201320360328.5) again, the propulsion system involved by it is the two ends being arranged on screw mandrel, coordinates the propulsion system of rotating two ends by the rotation of screw mandrel.
Although the reclining device of said structure is used in current dirigible structure widely, find after follow-up study careful for a long time present inventor, the reclining device essence of said structure also exists unavoidable defect, and reason is:
In above-mentioned reclining device, no matter be Linkage steering, worm screw, screw mandrel or axis, its effect is all for making propelling unit realize verting, then simple beam structure is formed between its structure itself and actuating device or bracing or strutting arrangement, the angle of rake weight in two ends is completely by Linkage steering, worm screw, screw mandrel or axis carrying, and, Linkage steering, worm screw, screw mandrel or axis need to run through whole gondola completely and can realize being connected with two propelling units simultaneously, make Linkage steering, worm screw, screw mandrel or axis are all in slender rod piece structure, the single supported beam of this slender rod piece structure is less along the load-carrying capacity in crossbeam radial direction, rigidity is also less, and also there will be the concentrated situation of stress in support place, specific in dirigible field, be embodied in following several aspect:
(1), because load-carrying capacity is less, rigidity is also less, so can only be applicable to the little and lightweight propelling unit of power, seriously limits high-power angle of rake use, and then limits the development of high-power airship technology;
(2), under actual applying working condition environment, dirigible is taking off, when flight or landing, whole dirigible more or less all can be impacted unavoidably, and the reclining device of simple beam structure, its Linkage steering, worm screw, screw mandrel or axis are all slim-lined construction, rigidity is low, impact resistance is weak, and then when impact occurs as easy as rolling off a log because of impact bending, once Linkage steering, worm screw, screw mandrel or axis occur bending, the control being just difficult to obtain again coordinating of verting of its two ends propelling unit, so, make the reliability of dirigible and handling all poor, serious potential safety hazard is brought to the use of dirigible,
(3), with regard to the structure of above-mentioned reclining device, owing to having an elongated connecting rod, worm screw, screw mandrel or axis between two propelling units, and hull itself is the structure of sealing, so when propelling unit is arranged on hull both sides, above-mentioned reclining device is also inapplicable, so also limit the Applicable scope of reclining device.
So, based on above-mentioned technical matters, need one at present badly and neither limit propelling unit model and power, various dirigible structure can be applicable to again, and also there is good reliability and handling reclining device.
Summary of the invention
The object of the invention is to, for current reclining device above shortcomings, provide one neither to limit propelling unit model and power, various dirigible structure can be applicable to again, and also there is good reliability and handling reclining device.
To achieve these goals, the technical solution used in the present invention is:
A kind of reclining device, includes the actuating device driving the tiliting axis of propelling unit generation pitch motion and drive described tiliting axis to rotate, the corresponding described propelling unit of described tiliting axis.
In the such scheme of the application, the reclining device provided, essence is each reclining device only corresponding propelling unit, need to carry two propelling unit weight compared to traditional reclining device simultaneously, be first alleviate the weight that reclining device carries, improve the reliability of reclining device, and, also make the reclining device of the application can load capacity larger, the propelling unit that power is higher, what so realize high-power propelling unit to apply to airship technology field may;
Simultaneously, also just because of each reclining device only corresponding propelling unit, the reclining device of the application can be arranged according to angle of rake actual design position, and the relative position relation between each propelling unit need not be considered, significantly increase the Applicable scope of reclining device;
Again on the one hand, described above, the reclining device of the application can be arranged according to angle of rake actual design position, that is, in actual design process, the length of tiliting axis can be shortened to greatest extent, and then, avoid the simple beam structure occurring slender rod piece in reclining device, further optimize the mechanical property of the application's tiliting axis, tiliting axis is made to have good load-carrying capacity and good rigidity, can not only actv. avoid stress concentrate problem, but also reduce when being subject to impacting, the risk occured bending and deformation, further improve the good reliability of the application's reclining device and handling.
As further preferred version, described reclining device also includes the speed reduction gearing for reducing described tiliting axis rotating speed, the input shaft of described speed reduction gearing and the output shaft of described actuating device are connected, and output shaft and the described tiliting axis of described speed reduction gearing are connected.In this programme, by arranging speed reduction gearing, and then make in the design process, high-revolving actuating device can be selected, reduce its rotating speed by speed reduction gearing and be converted to larger moment of torsion, that is, making tiliting axis obtain larger moment of torsion, make the reclining device of the application can be applicable to high-power propelling unit, also make reclining device high efficiencyly to operate simultaneously.
As further preferred version, the second retarder that described speed reduction gearing includes the first retarder and is in transmission connection with described first retarder, described in the input shaft one of described first retarder, the output shaft of actuating device is connected, and output shaft and the described tiliting axis of described second retarder are connected.In this programme, realize double reduction by the cooperation of the first retarder and the second retarder, improve the reduction ratio of speed reduction gearing.
As further preferred version, described reclining device also includes the bracing or strutting arrangement for supporting described tiliting axis, described bracing or strutting arrangement includes the supporting seat be fixedly connected with the housing of described speed reduction gearing, and is arranged on the bearing matched on described supporting seat and with described tiliting axis.In this programme, by arranging bracing or strutting arrangement, tiliting axis is supported, further improve the load-carrying capacity of tiliting axis, and, also reduce unsettled section of tiliting axis, further reduce tiliting axis and occur diastrophic risk because being hit, further improve unfailing performance and the safety performance of the application's reclining device.
As further preferred version, described supporting seat includes the first stay bearing plate and the second stay bearing plate that are oppositely arranged, be connected with at least two connecting panels between described first stay bearing plate and the second stay bearing plate, described first stay bearing plate, the second stay bearing plate and connecting panel form frame supporting structure; Described connecting panel is provided with the boss matched with described first stay bearing plate and the second stay bearing plate.In this programme, bracing or strutting arrangement is set to frame supporting structure, first, frame supporting structure has good stability, so can be good tiliting axis is supported, simultaneously, frame supporting structure also has lighter weight, so, the overall weight of reclining device can also be alleviated, reduce the burden of dirigible in actual use.In this programme, connecting panel arranges the boss matched with the first stay bearing plate and the second stay bearing plate, is first be convenient to connecting panel be connected with the contraposition between the first stay bearing plate and the second stay bearing plate, simultaneously, boss also plays the effect of reinforced rib, and then also improves the Joint strenght of connecting panel.
As further preferred version, described bearing is two, one of them bearing is arranged on described first stay bearing plate, what bearing described in another was corresponding is arranged on described second stay bearing plate, match with described speed reduction gearing in described tiliting axis one end, the other end, successively through after two described bearings, reaches described bracing or strutting arrangement outside and matches with described propelling unit.In this programme, coordinating with tiliting axis by arranging two bearings, ensureing that tiliting axis obtains failure-free and supports, improving the load-carrying capacity of tiliting axis further.
As further preferred version, described reclining device also includes the inhibiting device limiting described tiliting axis rotational angle, and described inhibiting device ensures that the tilt angle of described reclining device is being born between 50 degree and positive 180 degree.
As further preferred version, described reclining device also includes the inhibiting device limiting described tiliting axis rotational angle, and described inhibiting device ensures that the tilt angle of described reclining device is being born between 50 degree and positive 120 degree.In this programme, the flight manipulation practice long-term by present inventor and summary, show that the tilt angle of reclining device is when bearing between 50 degree and positive 120 degree, can not only make dirigible have brake function, but also make reclining device compact conformation unified, there is good reliability.
As further preferred version, described inhibiting device includes the dwang be fixedly connected with described tiliting axis, and limits the blocking mechanism of described dwang rotational angle; Described blocking mechanism includes two pins be spaced apart each other, and described pin connects and between described first stay bearing plate and the second stay bearing plate, and parallels with the central axis of described tiliting axis.In this programme, when tiliting axis rotates, drive dwang to rotate together, when dwang is stopped by blocking mechanism, tiliting axis is braked, and so, realizes the limit function to tiliting axis.In this programme, blocking mechanism is set to two pins, and two pins connect and between the first stay bearing plate and the second stay bearing plate, make, blocking mechanism not only plays position-limiting action, also plays the effect strengthening bracing or strutting arrangement simultaneously, further improves the stability of support device structure.
As further preferred version, two described pins are adjustable along the angle in described tiliting axis sagittal plane.In this programme, pin adjustable along the angle in tiliting axis sagittal plane, that is, makes the spacing adjustable angle of inhibiting device, and then can regulate the scope of tiliting axis tilt angle according to actual needs, increases the Applicable scope of the application's reclining device.
Owing to have employed the technical scheme of the application, the invention has the beneficial effects as follows:
1, alleviate the weight that reclining device carries, improve the reliability of reclining device, and also make reclining device can load capacity is larger, power is higher propelling unit, what so realize high-power propelling unit to apply to airship technology field may;
2, the reclining device of the application can be arranged according to angle of rake actual design position, and need not consider the relative position relation between each propelling unit, significantly increases the Applicable scope of reclining device;
3, the tiliting axis of the application has good load-carrying capacity and good rigidity, can not only actv. avoid stress concentrate problem, but also reducing when being subject to impacting, the risk occured bending and deformation, further improves the good reliability of the application's reclining device and handling.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is birds-eye view of the present invention;
Fig. 3 is A-A cutaway view in Fig. 2;
The structural representation of Fig. 4 bracing or strutting arrangement of the present invention;
Fig. 5 is the structural representation of inhibiting device of the present invention;
Fig. 6 is D-D cutaway view in Fig. 5;
The structural representation of Fig. 7 tilt angle of the present invention;
Fig. 8 is the structural representation of tiliting axis of the present invention,
Reference numeral: 1-tiliting axis, 2-actuating device, 3-control setup, 4-speed reduction gearing, 5-first retarder, 6-second retarder, 7-bracing or strutting arrangement, 8-supporting seat, 9-bearing, 10-first stay bearing plate, 11-second stay bearing plate, 12-connecting panel, 13-boss, 14-lightening hole, 15-Connection Block, 16-adapter plate, 17-axle sleeve, 18-inhibiting device, 19-dwang, 20-blocking mechanism, 21-pin.
Detailed description of the invention
In order to make object of the present invention, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be understood to, specific embodiment described herein only in order to explain the present invention, but is not intended to limit the present invention.
Embodiment 1:
A kind of reclining device as shown in the figure, include the actuating device 2 driving the tiliting axis 1 of propelling unit generation pitch motion and drive described tiliting axis 1 to rotate, the corresponding described propelling unit of described tiliting axis 1, described reclining device 1 also includes the control setup 3 controlling described actuating device 2 mode of operation, and described actuating device 2 is servomotor.Described reclining device also includes the speed reduction gearing 4 for reducing described tiliting axis 11 rotating speed, the input shaft of described speed reduction gearing 4 and the output shaft of described actuating device 2 are connected, output shaft and the described tiliting axis 1 of described speed reduction gearing 4 are connected, the second retarder 6 that described speed reduction gearing 4 includes the first retarder 5 and is in transmission connection with described first retarder 5, described in the input shaft one of described first retarder 5, the output shaft of actuating device 2 is connected, output shaft and the described tiliting axis 1 of described second retarder 6 are connected, described second retarder 6 is worm type of reduction gearing.
In the above-described embodiments, the reclining device provided, essence is each reclining device only corresponding propelling unit, need to carry two propelling unit weight compared to traditional reclining device simultaneously, be first alleviate the weight that reclining device carries, improve the reliability of reclining device, and, also make the reclining device of the present embodiment can load capacity larger, the propelling unit that power is higher, what so realize high-power propelling unit to apply to airship technology field may;
Simultaneously, also just because of each reclining device only corresponding propelling unit, the reclining device of the present embodiment can be arranged according to angle of rake actual design position, and the relative position relation between each propelling unit need not be considered, significantly increase the Applicable scope of reclining device;
Again on the one hand, described above, the reclining device of the present embodiment can be arranged according to angle of rake actual design position, that is, in actual design process, the length of tiliting axis 1 can be shortened to greatest extent, and then, avoid the simple beam structure occurring slender rod piece in reclining device, further optimize the mechanical property of the present embodiment tiliting axis 1, tiliting axis 1 is made to have good load-carrying capacity and good rigidity, can not only actv. avoid stress concentrate problem, but also reduce when being subject to impacting, the risk occured bending and deformation, further improve the good reliability of the present embodiment reclining device and handling,
In embodiment 1, by the cooperation of control setup 3 with servomotor, realize accurate control reclining device being exported to action of verting, the present embodiment reclining device is made to have further good and handling accurately, by arranging speed reduction gearing 4, and then make in the design process, high-revolving actuating device 2 can be selected, reduce its rotating speed by speed reduction gearing 4 and be converted to larger moment of torsion, namely, tiliting axis 1 is made to obtain larger moment of torsion, make the reclining device of the present embodiment can be applicable to high-power propelling unit, also make reclining device high efficiencyly to operate simultaneously, realize double reduction by the cooperation of the first retarder 5 and the second retarder 6, improve the retardation efficiency of speed reduction gearing 4, and, select worm type of reduction gearing, it has the advantages such as compact conformation, transmitting ratio be large and easy for installation, particularly there is auto-lock function, so adopt worm type of reduction gearing as the second retarder 6, can by self functional realiey of worm type of reduction gearing to the locking of tiliting axis 1, avoid in the course of the work, because when propelling unit is subject to resistance generation fluctuation, and make tiliting axis 1 rotate change propeller thrust direction, so, further improve unfailing performance and the safety performance of the present embodiment reclining device.
Embodiment 2:
As shown in the figure, on the architecture basics of reclining device as described in Example 1, described reclining device also includes the bracing or strutting arrangement 7 for supporting described tiliting axis 1, described bracing or strutting arrangement 7 includes the supporting seat 8 be fixedly connected with the housing of described speed reduction gearing 4, with be arranged on the bearing 9 matched on described supporting seat 8 and with described tiliting axis 1, described supporting seat 8 includes the first stay bearing plate 10 and the second stay bearing plate 11 be oppositely arranged, at least two connecting panels 12 are connected with between described first stay bearing plate 10 and the second stay bearing plate 11, described first stay bearing plate 10, second stay bearing plate 11 and connecting panel 12 form frame supporting structure, described connecting panel 12 is provided with the boss 13 matched with described first stay bearing plate 10 and the second stay bearing plate 11, described first stay bearing plate 10 and/or the second stay bearing plate 11 and/or connecting panel 12 are provided with and are arranged at intervals with some lightening holes 14 for alleviating deadweight, the side of connecting panel 12 described in one of them stretches out and forms the Connection Block 15 that is connected with described speed reduction gearing 4, described bracing or strutting arrangement 7 is achieved a fixed connection with described speed reduction gearing 4 by described Connection Block 15, described bearing 9 is two, one of them bearing 9 is arranged on described first stay bearing plate 10, what described in another, bearing 9 was corresponding is arranged on described second stay bearing plate 11, match with described speed reduction gearing 4 in described tiliting axis 1 one end, the other end is successively through after two described bearings 9, reach described bracing or strutting arrangement 7 outside to match with described propelling unit, also be provided with for installing described angle of rake adapter plate 16 between described tiliting axis 1 and described propelling unit, described adapter plate 16 is fixedly connected with described tiliting axis 1, described tiliting axis 1 is also arranged with axle sleeve 17, described axle sleeve 17 is between two described bearings 9.
The embodiment 2 of the present embodiment, support by arranging bracing or strutting arrangement 7 pairs of tiliting axiss 1, further improve the load-carrying capacity of tiliting axis 1, and, also reduce unsettled section of tiliting axis 1, further reduce tiliting axis 1 and occur diastrophic risk because being hit, further improve unfailing performance and the safety performance of the present embodiment reclining device; Bracing or strutting arrangement 7 is set to frame supporting structure, first, frame supporting structure has good stability, and then can be good tiliting axis 1 is supported, meanwhile, frame supporting structure also has lighter weight, so, the overall weight of reclining device can also be alleviated, reduce the burden of dirigible in actual use; Connecting panel 12 arranges the boss 13 matched with the first stay bearing plate 10 and the second stay bearing plate 11, first be convenient to connecting panel 12 be connected with the contraposition between the first stay bearing plate 10 and the second stay bearing plate 11, simultaneously, boss 13 also plays the effect of reinforced rib, and then also improves the Joint strenght of connecting panel 12; By arranging lightening hole 14, further optimizing the mechanical property of each component, the more important thing is the own wt alleviating each component, further alleviate the overall weight of reclining device; Bracing or strutting arrangement 7 arranges the Connection Block 15 being used for being connected with speed reduction gearing 4, makes to obtain failure-free between bracing or strutting arrangement 7 with speed reduction gearing 4 and be connected, improve the reliability of the present embodiment reclining device; Coordinating with tiliting axis 1 by arranging two bearings 9, ensureing that tiliting axis 1 obtains failure-free and supports, improving the load-carrying capacity of tiliting axis 1 further; Make tiliting axis 1 by arranging adapter plate 16 and obtain failure-free between propelling unit and be connected; Tiliting axis 1 essence between two bearings 9 is unsettled section, although in the technical scheme of the present embodiment, this unsettled section is significantly shortened, but when it is subject to impacting, still there is this diastrophic risk, so, the tiliting axis 1 between two bearings 9 arranges axle sleeve 17, increasing the rigidity of tiliting axis 1, avoiding the risk that it is occured bending and deformation because impacting.
Embodiment 3:
As shown in the figure, on the architecture basics of the reclining device described in embodiment 2, described reclining device also includes the inhibiting device 18 limiting described tiliting axis 1 rotational angle, and described inhibiting device 18 ensures that the tilt angle of described reclining device is being born between 50 degree and positive 180 degree.
Tradition reclining device tilt angle is generally designed to positive 90 degree and negative 90 degree, namely, reclining device can drive propelling unit to be rotated upwardly to horizontal direction of propulsion angle to be the angle of 90 degree, also propelling unit can be driven to be rotated down to being the angle of 90 degree with horizontal direction of propulsion angle, but, by long-term design effort and flight manipulation practice, the contriver of the present embodiment finds, in dirigible practical work process, due to the buoyancy of dirigible self, so the angle that reclining device is rotated down more than 45 degree is used hardly; And arbitrarily angled between positive 90 degree and negative 90 degree, even if reclining device is rotated upwardly to positive 90 degree, propelling unit also cannot be utilized to carry out brake and to make dirigible quick deceleration, so, current dirigible, when braking, can only rely on the resistance of dirigible self, and reduction of speed is slowly.So in the reclining device of the present embodiment, by arranging inhibiting device 18, the tilt angle of reclining device is controlled between 50 degree and positive 180 degree, first be eliminate the tilt angle be of little use, make the Stability Analysis of Structures of reclining device reliable, simultaneously, when dirigible needs brake or slows down, the tilt angle of reclining device can be rotated between positive 90 degree to positive 180, when tilt angle is greater than positive 90 degree, angle of rake part component using as dirigible brake needed for braking force, when tilt angle is 180 degree, angle of rake whole thrust is all as the braking force of dirigible brake, so, make it possible to fast speed braking dirigible, further raising dirigible handling.
Embodiment 4:
As shown in the figure, on the architecture basics of the reclining device described in embodiment 3, described reclining device also includes the inhibiting device 18 limiting described tiliting axis 1 rotational angle, described inhibiting device 18 ensures that the tilt angle of described reclining device is being born between 50 degree and positive 120 degree, described inhibiting device 18 includes the dwang 19 be fixedly connected with described tiliting axis 1, with the blocking mechanism 20 limiting described dwang rotational angle, described blocking mechanism 20 includes two pins be spaced apart each other 21, described pin 21 connects and between described first stay bearing plate 10 and the second stay bearing plate 11, and parallel with the central axis of described tiliting axis 1, two described pins 21 are adjustable along the angle in described tiliting axis 1 sagittal plane, described dwang 19 is arranged on described tiliting axis 1, the central axis of described dwang 19 and the central axis of described tiliting axis 1 perpendicular.
In the present embodiment, the flight manipulation practice long-term by the present embodiment contriver and summary, show that the tilt angle of reclining device is when bearing between 50 degree and positive 120 degree, can not only make dirigible have brake function, but also make reclining device compact conformation unified, there is good reliability; When tiliting axis 1 rotates, drive dwang 19 to rotate together, when dwang 19 is stopped by blocking mechanism 20, tiliting axis 1 is braked, and so, realizes the limit function to tiliting axis 1; Blocking mechanism 20 is set to two pins 21, and two pins 21 connect and between the first stay bearing plate 10 and the second stay bearing plate 11, make, blocking mechanism 20 not only plays position-limiting action, also play the effect strengthening bracing or strutting arrangement 7 simultaneously, further improve the stability of bracing or strutting arrangement 7 structure; Pin 21 adjustable along the angle in tiliting axis 1 sagittal plane, that is, makes the spacing adjustable angle of inhibiting device 18, and then can regulate the scope of tiliting axis 1 tilt angle according to actual needs, increases the Applicable scope of the present embodiment reclining device; The central axis of dwang 19 and the central axis of tiliting axis 1 perpendicular, make, when dwang 19 contacts with pin 21, be therebetween positive pressure, so, optimize the stressing conditions of inhibiting device 18, improve the reliability of inhibiting device 18.
All any amendments done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within protection scope of the present invention.

Claims (10)

1. a reclining device, includes the actuating device driving the tiliting axis of propelling unit generation pitch motion and drive described tiliting axis to rotate, it is characterized in that, the corresponding described propelling unit of described tiliting axis.
2. reclining device as claimed in claim 1, it is characterized in that, described reclining device also includes the speed reduction gearing for reducing described tiliting axis rotating speed, the input shaft of described speed reduction gearing and the output shaft of described actuating device are connected, and output shaft and the described tiliting axis of described speed reduction gearing are connected.
3. reclining device as claimed in claim 2, it is characterized in that, the second retarder that described speed reduction gearing includes the first retarder and is in transmission connection with described first retarder, described in the input shaft one of described first retarder, the output shaft of actuating device is connected, and output shaft and the described tiliting axis of described second retarder are connected.
4. the reclining device as described in any one of claim 2-3, it is characterized in that, also include the bracing or strutting arrangement for supporting described tiliting axis, described bracing or strutting arrangement includes the supporting seat be fixedly connected with the housing of described speed reduction gearing, and is arranged on the bearing matched on described supporting seat and with described tiliting axis.
5. reclining device as claimed in claim 4, it is characterized in that, described supporting seat includes the first stay bearing plate and the second stay bearing plate that are oppositely arranged, be connected with at least two connecting panels between described first stay bearing plate and the second stay bearing plate, described first stay bearing plate, the second stay bearing plate and connecting panel form frame supporting structure; Described connecting panel is provided with the boss matched with described first stay bearing plate and the second stay bearing plate.
6. reclining device as claimed in claim 5, it is characterized in that, described bearing is two, one of them bearing is arranged on described first stay bearing plate, what bearing described in another was corresponding is arranged on described second stay bearing plate, match with described speed reduction gearing in described tiliting axis one end, the other end, successively through after two described bearings, reaches described bracing or strutting arrangement outside and matches with described propelling unit.
7. reclining device as claimed in claim 5, is characterized in that, also include the inhibiting device limiting described tiliting axis rotational angle, and described inhibiting device ensures that the tilt angle of described reclining device is being born between 50 degree and positive 180 degree.
8. reclining device as claimed in claim 7, it is characterized in that, described reclining device also includes the inhibiting device limiting described tiliting axis rotational angle, and described inhibiting device ensures that the tilt angle of described reclining device is being born between 50 degree and positive 120 degree.
9. reclining device as claimed in claim 8, it is characterized in that, described inhibiting device includes the dwang be fixedly connected with described tiliting axis, and limits the blocking mechanism of described dwang rotational angle; Described blocking mechanism includes two pins be spaced apart each other, and described pin connects and between described first stay bearing plate and the second stay bearing plate, and parallels with the central axis of described tiliting axis.
10. reclining device as claimed in claim 9, it is characterized in that, two described pins are adjustable along the angle in described tiliting axis sagittal plane.
CN201510430977.1A 2015-07-21 2015-07-21 Tilting device Pending CN104960658A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106892080A (en) * 2017-02-28 2017-06-27 北京天恒长鹰科技股份有限公司 Near space dirigible and the vector propulsion device near space dirigible

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WO2004074091A2 (en) * 2003-02-24 2004-09-02 Charles Raymond Luffman Air vehicle
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