CN108995826A - The assembly method of mixed power plant - Google Patents
The assembly method of mixed power plant Download PDFInfo
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- CN108995826A CN108995826A CN201810860422.4A CN201810860422A CN108995826A CN 108995826 A CN108995826 A CN 108995826A CN 201810860422 A CN201810860422 A CN 201810860422A CN 108995826 A CN108995826 A CN 108995826A
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- Prior art keywords
- main support
- mounting plate
- upper rack
- support
- rack posts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
Abstract
The invention discloses a kind of assembly methods of mixed power plant, and using integrated mounting system, distance increasing unit is mounted in distance increasing unit support device comprising steps of S1, distance increasing unit support device is mounted on the body of hybrid power aeroplane by assembly method；S2, motor mounting plate is mounted in distance increasing unit support device, driving motor is mounted on motor mounting plate；S3, the first controller mounting plate is mounted on the body of hybrid power aeroplane, the first controller is mounted on the first controller mounting plate.The assembly method of mixed power plant of the present invention, by using integrated mounting system, it can make the distance increasing unit, driving motor and controller integrated installation of mixed power plant, the assembly efficiency and integrally-built compactedness of mixed power plant can be improved, facilitate arrangement of the mixed power plant on hybrid power aeroplane, it is convenient for disassembly and assembly, operation easy to repair.
Description
Technical field
The invention belongs to vehicle technology fields, and specifically, the present invention relates to a kind of assembly sides of mixed power plant
Method.
Background technique
Hybrid power aeroplane can keep higher continuation of the journey while reducing environmental pollution as a kind of new energy aircraft
Ability has preferable development prospect in general-purpose aircraft field at present.Due to power device traditional engine used instead it is a set of
Mixed power plant replaces, therefore how in limited nacelle space, and realizing will mixed dynamic distance increasing unit, driving motor and major control
Device processed is simply and easily laid out, safety is installed, and is made it easy to dismounting, maintenance, is become one of hybrid power aeroplane structure development
Important technology.
Summary of the invention
The present invention is directed at least solve one of the technical problems existing in the prior art.For this purpose, the present invention provides a kind of mix
Close the assembly method of power device, it is therefore an objective to improve assembly efficiency.
To achieve the goals above, the technical scheme adopted by the invention is as follows: the assembly method of mixed power plant, using collection
At installation system, integrated mounting system includes distance increasing unit support device, motor mounting plate and the first controller mounting plate, the dress
Method of completing the square comprising steps of
S1, distance increasing unit support device is mounted on the body of hybrid power aeroplane, distance increasing unit is mounted on distance increasing unit branch
On support arrangement；
S2, motor mounting plate is mounted in distance increasing unit support device, driving motor is mounted on motor mounting plate；
S3, the first controller mounting plate is mounted on the body of hybrid power aeroplane, the first controller is mounted on
On one controller mounting plate.
In the step S1, the distance increasing unit support device is attached with three positions of distance increasing unit, distance increasing unit
Support device includes the first Auxiliary support component connecting with the first position of distance increasing unit, connect with the second position of distance increasing unit
Second Auxiliary support component and the main support member being connect with the third position of distance increasing unit, the first Auxiliary support component and second auxiliary
Support member is helped to connect with main support member.
It is detachable connection between the distance increasing unit support device and three positions of distance increasing unit.
The main support member includes the first main support, the second main support, third main support, the 4th main support and with the
The main connecting plate that one main support, the second main support, third main support and the 4th main support connect；In the step S2, first
Main support, the second main support, third main support and the 4th main support are attached with the motor mounting plate.
First main support and second main support are positioned opposite, the third main support and the 4th main branch
Frame be it is positioned opposite, third main support is located at the lower section of the first main support, and the 4th main support is located at the lower section of the second main support.
First main support include the first upper rack posts that need to be attached with the motor mounting plate and with first on prop up
The first lower fulcrum bar stretched out on the outside of bar connection and the first upper rack posts of direction, second main support include and the motor mounting plate
Second upper rack posts of connection and the second lower fulcrum bar for connecting with the second upper rack posts and being stretched out on the outside of the second upper rack posts of direction, the master
Connecting plate is connect between the first lower fulcrum bar and the second lower fulcrum bar and with the first lower fulcrum bar and the second lower fulcrum bar.
The third main support include the third upper rack posts that need to be attached with the motor mounting plate and with propped up in third
Bar connection and towards the third lower fulcrum bar stretched out on the outside of third upper rack posts, the 4th main support include need and motor mounting plate into
4th upper rack posts of row connection and the 4th lower fulcrum bar for connecting with the 4th upper rack posts and being stretched out on the outside of the 4th upper rack posts of direction, it is described
Main connecting plate is connect between third lower fulcrum bar and the 4th lower fulcrum bar and with third lower fulcrum bar and the 4th lower fulcrum bar, is propped up under third
Bar is located at the lower section of first lower fulcrum bar, and the 4th lower fulcrum bar is located at the lower section of second lower fulcrum bar.
The first Auxiliary support component includes the carriage mounting plate and carriage mounting plate connecting with the 4th main support
The diagonal support of connection, the first connecting plate being connect with diagonal support and first turn connect for the first position with distance increasing unit
Fishplate bar and the resilient cushion being clipped between the first connecting plate and the first pinboard, the first connecting plate be located at the third main support and
Between 4th main support.
In the step S1, the carriage mounting plate is attached by clip and the 4th main support, hoop sleeve
On the 4th main support and clip is attached by fastener and carriage mounting plate.
The first Auxiliary support component further includes first connect with first connecting plate and second main support
Auxiliary stand, the first auxiliary stand are located at the top of the diagonal support, in the step S1, are assisted by bolt by first
Bracket is attached with the first connecting plate.
The assembly method of mixed power plant of the present invention can make mixed power plant by using integrated mounting system
Distance increasing unit, driving motor and controller integrated installation, the assembly efficiency of mixed power plant and integrally-built can be improved
Compactedness facilitates arrangement of the mixed power plant on hybrid power aeroplane, convenient for disassembly and assembly, operation easy to repair；And it is integrated
The structural stability of installation system is good, and globality is strong, load trans path clear and definite, it is ensured that the safety of mixed power plant
Reliable installation.
Detailed description of the invention
This specification includes the following drawings, and shown content is respectively:
Fig. 1 is the assembling schematic diagram of integrated mounting system and mixed power plant；
Fig. 2 is the structural schematic diagram of integrated mounting system；
Fig. 3 is A direction view in Fig. 2；
Fig. 4 is B direction view in Fig. 2；
Fig. 5 is the rear structure schematic diagram of integrated mounting system；
Fig. 6 is the axonometric drawing after integrated mounting system and mixed power plant assembly；
Fig. 7 is the cross-sectional view of resilient cushion Yu pinboard and connecting plate junction；
In the figure, it is marked as 1, motor mounting plate；2, the first main support；201, the first upper rack posts；202, the first lower fulcrum bar；3,
Second main support；301, the second upper rack posts；302, the second lower fulcrum bar；4, third main support；401, third upper rack posts；402, third
Lower fulcrum bar；5, the 4th main support；501, the 4th upper rack posts；502, the 4th lower fulcrum bar；6, main connecting plate；7, the first Auxiliary support portion
Part；701, carriage mounting plate；702, diagonal support；703, the first connecting plate；704, the first auxiliary stand；705, clip；706,
First pinboard；8, the second Auxiliary support component；801, the second connecting plate；802, the second pinboard；803, the second auxiliary stand；
804, third auxiliary stand；805, third connecting plate；806, third pinboard；9, the first controller mounting plate；10, the second control
Device mounting plate；11, distance increasing unit；12, driving motor；13, the first controller；14, second controller；15, resilient cushion；16, main to turn
Fishplate bar；17, the first rear portion strut；18, the second rear portion strut；19, third rear portion strut；20, the 4th rear portion strut；21, the 5th
Rear portion strut；22, center connecting rod.
Specific embodiment
Below against attached drawing, by the description of the embodiment, making to a specific embodiment of the invention further details of
Explanation, it is therefore an objective to those skilled in the art be helped to have more complete, accurate and deep reason to design of the invention, technical solution
Solution, and facilitate its implementation.
As shown in Figures 1 to 7, the present invention provides a kind of assembly methods of mixed power plant, using integrated installation system
System, integrated mounting system include distance increasing unit support device, motor mounting plate 1 and the first controller mounting plate 9, distance increasing unit support dress
Set be for connect with distance increasing unit and for distance increasing unit provide support, motor mounting plate 1 be for install driving motor and with
The connection of distance increasing unit support device, the first controller mounting plate 9 be for installing the first controller, the first controller mounting plate 9 with
Distance increasing unit support device is fixedly connected.Assembly method of the invention comprises the following steps that
S1, distance increasing unit support device is mounted on the body of hybrid power aeroplane, distance increasing unit is mounted on distance increasing unit branch
On support arrangement；
S2, motor mounting plate is mounted in distance increasing unit support device, driving motor is mounted on motor mounting plate；
S3, the first controller mounting plate is mounted on the body of hybrid power aeroplane, the first controller is mounted on
On one controller mounting plate.
Specifically, the mixed power plant of hybrid power aeroplane is mainly by distance increasing unit, driving motor, the first controller
It is formed with second controller, distance increasing unit is by engine and generating set at engine connect with generator and drives generator
It generates electricity, engine and generator link into an integrated entity structure, and power battery is for storing electric energy and power battery as driving electricity
Machine provides electric energy, and driving motor is used to propeller and provides driving force, and driving propeller is rotated, and to generate pulling force, is
Aircraft provides the kinetic energy to advance.Integrated mounting system is for distance increasing unit, driving motor and the first control to mixed power plant
Device processed provides installation site, so that the distance increasing unit of mixed power plant, driving motor and the first controller collection are integral, forms collection
Accepted way of doing sth installation, can be improved the integrally-built compactedness of mixed power plant, and then facilitate mixed power plant in hybrid power
It is arranged in the limited nacelle in space on aircraft, structural stability is good, convenient for disassembly and assembly, all parts of mixed power plant
It can independently dismount, it is easy to operate, convenient for the daily maintenance and breakdown maintenance in entire hybrid power engine cabin.
As shown in Figures 1 to 6, motor mounting plate 1 and the first controller mounting plate 9 are connect with distance increasing unit support device, electricity
Machine mounting plate 1 and the first controller mounting plate 9 are mounted in distance increasing unit support device, and distance increasing unit is mounted on distance increasing unit support device
On, the first controller is mounted on the first controller mounting plate 9, and driving motor is mounted on motor mounting plate 1.In above-mentioned steps
In S1, distance increasing unit support device is attached with three positions of distance increasing unit, and distance increasing unit support device includes and distance increasing unit
First Auxiliary support component 7 of first position connection, the second Auxiliary support component 8 for being connect with the second position of distance increasing unit and with
The main support member of the third position connection of distance increasing unit, the first Auxiliary support component 7 and the second Auxiliary support component 8 and main support
Component connection.Distance increasing unit support device and distance increasing unit are detachable connection, easy disassembly, and distance increasing unit support device and increase
Three components of journey device are attached, it is ensured that the reliability of connection and the stability to distance increasing unit support.Distance increasing unit support
Device is to connect with the body of hybrid power aeroplane, and being can between distance increasing unit support device and the body of hybrid power aeroplane
It is detachably connected with, easy disassembly.Motor mounting plate 1 is fixedly connected with one end of distance increasing unit support device, the installation of the first controller
Plate 9 is fixedly connected with the other end of distance increasing unit support device, motor mounting plate 1 and the first controller mounting plate 9 be it is positioned opposite,
Motor mounting plate 1 is located at the front end of distance increasing unit support device, after the first controller mounting plate 9 is located at distance increasing unit support device
End, distance increasing unit is between driving motor and the first controller.Preferably, driving motor is removable with motor mounting plate 1
Formula connection is unloaded, the first controller and the first controller mounting plate 9 are also detachable connection, easy disassembly, so that mixing
The all parts of power device can be dismounted independently, convenient for safeguarding.
As shown in Figures 1 to 6, the third position of main support member and distance increasing unit is detachable connection, main support member
Play the role of carrying, is main load bearing component, motor mounting plate 1, the first Auxiliary support component 7 and the second Auxiliary support component
8 are fixedly connected with main support member, form integral structure.Main support member includes the first main support 2, the second main support 3, third
It main support 4, the 4th main support 5 and is connect with the first main support 2, the second main support 3, third main support 4 and the 4th main support 5
Main connecting plate 6, the first main support 2, the second main support 3, third main support 4 and the 4th main support 5 connect with motor mounting plate 1
It connects, the first Auxiliary support component 7 is connect with the second main support 3 and the 4th main support 5, and the first Auxiliary support component 7 is mounted on
On two main supports 3 and the 4th main support 5, based on the first main support 2, the second main support 3, third main support 4 and the 4th main support 5
The load and Force transmission parts wanted.First main support 2 and the second main support 3 are positioned opposite, third main support 4 and the 4th main support
5 is positioned opposite, and third main support 4 is located at the lower section of the first main support 2, and the 4th main support 5 is located under the second main support 3
Side.First main support 2 is fixedly connected with the first position of motor mounting plate 1, the second main support 3 and the second of motor mounting plate 1
Position is fixedly connected, and third main support 4 is fixedly connected with the third member of motor mounting plate 1, and the 4th main support 5 is installed with motor
4th component of plate 1 is fixedly connected, and first position, second position, third position and the 4th position of motor mounting plate 1 are in rectangle
Distribution, the first position and second position of motor mounting plate 1 are on the same straight line parallel with first direction, motor installation
The third position and the 4th position of plate 1 are also on the same straight line parallel with first direction, and first of motor mounting plate 1
Position and third position are on the same straight line parallel with second direction, the second position of motor mounting plate 1 and the 4th position
It is also on the same straight line parallel with second direction, first direction and second direction is perpendicular and first direction and second party
Axis to the output shaft with driving motor is perpendicular, the first position of motor mounting plate 1, second position, third position
The outside surrounding of the axis of the output shaft of driving motor is distributed in the 4th position, in this way, structural stability is more preferable, support
High reliablity.First main support 2, the second main support 3, third main support 4 and the 4th main support 5 are thin-winding pipe molding, are had
Effect drop stress concentration, main supporting part structure intensity is high, good reliability.
As shown in Figures 1 to 6, the first main support 2 includes the first upper rack posts 201 connecting with motor mounting plate 1 and with
The first lower fulcrum bar 202 stretched out on the outside of the connection of one upper rack posts 201 and the first upper rack posts 201 of direction, the second main support 3 include and electricity
The second upper rack posts 301 and connect with the second upper rack posts 301 and stretched out on the outside of the second upper rack posts 301 of direction that machine mounting plate 1 connects
The second lower fulcrum bar 302, main connecting plate 6 between the first lower fulcrum bar 202 and the second lower fulcrum bar 302 and with the first lower fulcrum bar
202 and second lower fulcrum bar 302 connect.The length direction of main connecting plate 6 is parallel with second direction, the thickness side of main connecting plate 6
To parallel with first direction, main connecting plate 6 and between motor mounting plate 1 and the second Auxiliary support component 8.It is propped up on first
Bar 201 and the first lower fulcrum bar 202 all have certain length, and first of one end of the first upper rack posts 201 and motor mounting plate 1
The body of position connection, the other ends of the first upper rack posts 201 and hybrid power aeroplane connects, one end of the first lower fulcrum bar 202 and the
One upper rack posts 201 be fixedly connected and the first lower fulcrum bar 202 be at position between the both ends of the first upper rack posts 201 with first on
Strut 201 is fixedly connected, and the other end of the first lower fulcrum bar 202 is fixedly connected with the upper end of main connecting plate 6.Second upper rack posts 301
Certain length is all had with the second lower fulcrum bar 302, one end of the second upper rack posts 301 and the second position of motor mounting plate 1 connect
It connects, the other end of the second upper rack posts 301 and the body of hybrid power aeroplane connect, on one end and second of the second lower fulcrum bar 302
Strut 301 be fixedly connected and the second lower fulcrum bar 302 be at position between the both ends of the second upper rack posts 301 with the second upper rack posts
301 are fixedly connected, and the other end of the second lower fulcrum bar 302 is connect with the upper end of main connecting plate 6, under the first lower fulcrum bar 202 and second
Strut 302 is located at the side of main connecting plate 6, and main connecting plate 6 is located proximate to the first upper rack posts 201, the first lower fulcrum bar 202
Length less than the second lower fulcrum bar 302 length, convenient for the third position of distance increasing unit be adapted.First lower fulcrum bar 202 and
Two lower fulcrum bars 302 are arc-shaped rod component, the tie point and the second lower fulcrum bar of the first lower fulcrum bar 202 and the first upper rack posts 201
302 are on the same straight line parallel with first direction with the tie point of the second upper rack posts 301, the length of the first upper rack posts 201
There is angle between degree direction and first direction and the angle is less than 90 degree, the length direction and first party of the second upper rack posts 301
There is angle between and the angle is less than 90 degree, the first upper rack posts 201 and the V-shaped arrangement of the second upper rack posts 301, propped up on first
Between the end that the end and the second upper rack posts 301 that bar 201 is connected with motor mounting plate 1 are connected with motor mounting plate 1
End that vertical range is connected less than the first upper rack posts 201 with the body of hybrid power aeroplane and the second upper rack posts 301 with it is mixed
The vertical range between end that the body of conjunction motor plane is connected.
Preferably, the first upper rack posts 201, the first lower fulcrum bar 202, the second upper rack posts 301,302 and of the second lower fulcrum bar
The material of main connecting plate 6 is steel alloy, and the first upper rack posts 201 and the first lower fulcrum bar 202 are to be welded to connect, the second upper rack posts 301
It is to be welded to connect with the second lower fulcrum bar 302, the first lower fulcrum bar 202 and the second lower fulcrum bar 302 and main connecting plate 6 are welded connecting,
Overall structural strength is high, and stability of strutting system is good.
As shown in Figures 1 to 6, third main support 4 includes third upper rack posts 401 connecting with motor mounting plate 1 and with
Three upper rack posts 401 connection and towards the third lower fulcrum bar 402 stretched out on the outside of third upper rack posts 401, the 4th main support 5 includes and electricity
The 4th upper rack posts 501 and connect with the 4th upper rack posts 501 and stretched out on the outside of the 4th upper rack posts 501 of direction that machine mounting plate 1 connects
The 4th lower fulcrum bar 502, main connecting plate 6 between third lower fulcrum bar 402 and the 4th lower fulcrum bar 502 and with third lower fulcrum bar
402 and the 4th lower fulcrum bar 502 connect, third lower fulcrum bar 402 is located at the lower section of the first lower fulcrum bar 202, and the 4th lower fulcrum bar 502 is located at
The lower section of second lower fulcrum bar 302, third upper rack posts 401 also are located at the lower section of the first upper rack posts 201 and the first lower fulcrum bar 202, the
Four upper rack posts 501 also are located at the lower section of the second upper rack posts 301 and the second lower fulcrum bar 302.Main connecting plate 6 is located at third upper rack posts
401 and the 4th between upper rack posts 501, and third upper rack posts 401 and third lower fulcrum bar 402 all have certain length, prop up in third
One end of bar 401 is connect with the third position of motor mounting plate 1, the other ends of third upper rack posts 401 and hybrid power aeroplane
Body connection, one end of third lower fulcrum bar 402 is fixedly connected with third upper rack posts 401 and third lower fulcrum bar 402 is in third
It is fixedly connected at position between the both ends of strut 401 with third upper rack posts 401, the other end of third lower fulcrum bar 402 and main company
The lower end of fishplate bar 6 is fixedly connected.4th upper rack posts 501 and the 4th lower fulcrum bar 502 all have certain length, the 4th upper rack posts
501 one end is connect with the 4th position of motor mounting plate 1, the other end of the 4th upper rack posts 501 and the machine of hybrid power aeroplane
Body connection, one end of the 4th lower fulcrum bar 502 is fixedly connected with the 4th upper rack posts 501 and the 4th lower fulcrum bar 502 is propped up on the 4th
It is fixedly connected at position between the both ends of bar 501 with the 4th upper rack posts 501, the other end of the 4th lower fulcrum bar 502 and main connection
The upper end of plate 6 is fixedly connected, and third lower fulcrum bar 402 and the 4th lower fulcrum bar 502 are located at the side of main connecting plate 6, main connection
Plate 6 is located proximate to third upper rack posts 401, the length of third lower fulcrum bar 402 less than the 4th lower fulcrum bar 502 length, convenient for
The third position of distance increasing unit is adapted.Third lower fulcrum bar 402 and the 4th lower fulcrum bar 502 are arc-shaped rod-like structure, are propped up under third
The tie point and the 4th lower fulcrum bar 502 of bar 402 and third upper rack posts 401 and the tie point of the 4th upper rack posts 501 are in and first
On the parallel same straight line in direction, there is angle and the angle between the length direction and third direction of third upper rack posts 401
There is angle less than 90 degree, between the length direction and third direction of the 4th upper rack posts 501 and the angle is less than 90 degree, in third
Strut 401 and the V-shaped arrangement of the 4th upper rack posts 501, the end and the 4th that third upper rack posts 401 are connected with motor mounting plate 1
The vertical range between end that upper rack posts 501 are connected with motor mounting plate 1 is less than third upper rack posts 401 and hybrid power flies
It is vertical between the end that the end and the 4th upper rack posts 501 that the body of machine is connected are connected with the body of hybrid power aeroplane
Distance, and the end that is connected with the body of hybrid power aeroplane of the first upper rack posts 201 and the second upper rack posts 301 with mix it is dynamic
The vertical range between end that the body of power aircraft is connected is greater than the body phase of third upper rack posts 401 and hybrid power aeroplane
The vertical range between end that the end of connection and the 4th upper rack posts 501 are connected with the body of hybrid power aeroplane, first
The body of end and the second upper rack posts 301 and hybrid power aeroplane that upper rack posts 201 are connected with the body of hybrid power aeroplane
The end being connected is in sustained height, the end and the 4th that third upper rack posts 401 are connected with the body of hybrid power aeroplane
The end that upper rack posts 501 are connected with the body of hybrid power aeroplane is also at sustained height, third upper rack posts 401 with mix it is dynamic
The height for the end that the body of power aircraft is connected is less than the end that the first upper rack posts 201 are connected with the body of hybrid power aeroplane
The height in portion, the height of the first position of motor mounting plate 1 are greater than the height at the third position of motor mounting plate 1, motor installation
The height at the third position of plate 1 is greater than the height for the end that the first upper rack posts 201 are connected with the body of hybrid power aeroplane, the
One upper rack posts 201, the second upper rack posts 301, third upper rack posts 401 and the 4th upper rack posts 501 are that inclination is extended.
Preferably, third upper rack posts 401, third lower fulcrum bar 402, the 4th upper rack posts 501 and the 4th lower fulcrum bar 502
Material is steel alloy, and third upper rack posts 401 and third lower fulcrum bar 402 are to be welded to connect, the 4th upper rack posts 501 and the 4th lower fulcrum bar
502 is are welded to connect, and third lower fulcrum bar 402 and the 4th lower fulcrum bar 502 and main connecting plate 6 are welded connecting, overall structural strength
Height, stability of strutting system are good.
Mainly it is made of the first main support 2 of above structure, the second main support 3, third main support 4 and the 4th main support 5
Main support member be tower structure, inner space is big, is convenient for the dismounting and maintenance of distance increasing unit, and structural strength is high, makes
It is long with the service life, it is easy to process.
As shown in Figures 1 to 6, main support member further includes the main pinboard 16 connecting for the third position with distance increasing unit
With the resilient cushion being set on main connecting plate 6, main pinboard 16 is located at the side of main connecting plate 6 and main pinboard 16 and main connection
Plate 6 is parallel, and resilient cushion has elastic property, and resilient cushion can produce certain elastic deformation amount, to play cushioning effect, damping
Pad is fixedly connected with main pinboard 16 and resilient cushion is clipped between main connecting plate 6 and main pinboard 16, and then can play vibration damping
Effect, the caused vibration of decaying distance increasing unit, realizes the flexible connection with distance increasing unit, improves reliability.Resilient cushion has a variety of
Form, the rubber block as made of using rubber material.
Preferably, main connecting plate 6 has as shown in fig. 7, resilient cushion is to be fixedly connected by bolt with main pinboard 16
There is the mounting hole for allowing resilient cushion to fill in, resilient cushion is fixedly connected with main connecting plate 6.Main pinboard 16 is by bolt and distance increasing unit
It is attached, with easy disassembly, main pinboard 16 has the through-hole for allowing bolt to pass through.
As shown in Figures 1 to 7, the first Auxiliary support component 7 include the carriage mounting plate 701 being connect with the 4th main support 5,
The diagonal support 702 being connect with carriage mounting plate 701 and the first connecting plate 703 being connect with diagonal support 702, the first connecting plate
703 between third main support 4 and the 4th main support 5.Carriage mounting plate 701 is mounted on the 4th upper rack posts 501, diagonal brace branch
One end of frame 702 is fixedly connected with carriage mounting plate 701, and the other end and carriage mounting plate 701 of diagonal support 702 are fixed to be connected
It connects, carriage mounting plate 701 and diagonal support 702 are located at the lower section of distance increasing unit, and the height of the first connecting plate 703, which is greater than on the 4th, props up
The height for the end that bar 501 is connected with the body of hybrid power aeroplane.First Auxiliary support component 7 further include for increase journey
The first of the first position connection of device pinboard 706 and the resilient cushion that is set on the first connecting plate 703, the first pinboard 706
Positioned at the first connecting plate 703 side and the first pinboard 706 it is parallel with the first connecting plate 703, the first connecting plate 703 with it is main
Connecting plate 6 is parallel.Resilient cushion has elastic property, and resilient cushion can produce certain elastic deformation amount, to play cushioning effect,
Resilient cushion is fixedly connected with the first pinboard 706 and resilient cushion is clipped between the first connecting plate 703 and the first pinboard 706, into
And effectiveness in vibration suppression can be played, vibration caused by decaying distance increasing unit realizes the flexible connection with distance increasing unit, improves reliability.
Resilient cushion has diversified forms, the rubber block as made of using rubber material.
Preferably, first connects as shown in fig. 7, resilient cushion is to be fixedly connected by bolt with the first pinboard 706
Plate 703 has the mounting hole for allowing resilient cushion to fill in, and resilient cushion is fixedly connected with the first connecting plate 703.First pinboard 706 is logical
It crosses bolt to be attached with distance increasing unit, with easy disassembly, the first pinboard 706 has the through-hole for allowing bolt to pass through.
As shown in Figures 1 to 6, the first Auxiliary support component 7 further includes connecting with the first connecting plate 703 and the second main support 3
The first auxiliary stand 704 connect, the first auxiliary stand 704 are located at the top of diagonal support 702.First auxiliary stand 704 is set
Set, improve the bonding strength of the first Auxiliary support component 7 with main support member, improve to the stability of distance increasing unit support and
Reliability.One end of first auxiliary stand 704 connect with the first connecting plate 703 and is between the two detachable connection, and first
The other end of auxiliary stand 704 is fixedly connected with the end of the second upper rack posts 301 and the end of the second upper rack posts 301 is second
The length of the one end of upper rack posts 301 being connected with the body of hybrid power aeroplane, the first auxiliary stand 704 is greater than diagonal support
702 length.First auxiliary stand 704 and diagonal support 702 are the rod component with certain length, the first auxiliary stand
704, the material of diagonal support 702, the first connecting plate 703 and the first pinboard 706 is steel alloy, the first auxiliary stand 704 with
Second upper rack posts 301 are to be welded to connect, and diagonal support 702 and the first connecting plate 703 and the first pinboard 706 are to be welded to connect.
First Auxiliary support component, 7 overall structural strength is high, and stability of strutting system is good.
As shown in Figures 1 to 6, carriage mounting plate 701 is connect by clip 705 with the 4th main support 5, and clip 705 is arranged
In on the 4th main support 5 and clip 705 is connect with carriage mounting plate 701 by fastener.Preferably, clip 705 is arranged
Multiple and all clips 705 are sequentially arranged for the length direction along the 4th upper rack posts 501, and clip 705 is c-type structure, clip 705
Cover on the 4th upper rack posts 501, carriage mounting plate 701 is located at the side of the 4th upper rack posts 501, clip 705 be by two by
The fastener that screw bolt and nut is constituted is connect with carriage mounting plate 701, and the both ends of clip 705 and carriage mounting plate 701 are equipped with
Allow the through-hole that bolt passes through, clip 705 is matched with carriage mounting plate 701 clamps the 4th upper rack posts 501, realize and the 4th on prop up
Bar 501 is fixedly connected.
In the present embodiment, as shown in Figure 3 and Figure 6, clip 705 is arranged two.Clip 705 and carriage mounting plate 701 it
Between form detachable connection so that forming detachable company between the first Auxiliary support component 7 and the 4th main support 5
It connects.In this way when being assembled with distance increasing unit, position-adjustable of the first Auxiliary support component 7 on the 4th main support 5, thus
Build-up tolerance is compensated, with convenient for assembly, helps to improve assembly efficiency.
As shown in Figures 1 to 7, the second Auxiliary support component 8 includes the second auxiliary stand connecting with main support member
803, the second connecting plate 801 being connect with the second auxiliary stand 803, the second switching being connect for the second position with distance increasing unit
Plate 802 and the resilient cushion being set on the second connecting plate 801, the second pinboard 802 are located at the side of the second connecting plate 801 and the
Two pinboards 802 are parallel with the second connecting plate 801, and the second connecting plate 801 is parallel with main connecting plate 6, and main connecting plate 6 is located at
Between motor mounting plate 1 and the second connecting plate 801.One end of second auxiliary stand 803 is fixedly connected with main support member, and second
The other end of auxiliary stand 803 is fixedly connected with the second connecting plate 801, and the height of main support member is greater than the first connecting plate 703
Height, the tie point of the second auxiliary stand 803 and main support member is located at the lower section of the second connecting plate 801.It is set to second
Resilient cushion on connecting plate 801 has elastic property, and resilient cushion can produce certain elastic deformation amount, to play cushioning effect,
Resilient cushion is fixedly connected with the second pinboard 802 and resilient cushion is clipped between the second connecting plate 801 and the second pinboard 802, into
And effectiveness in vibration suppression can be played, vibration caused by decaying distance increasing unit realizes the flexible connection with distance increasing unit, improves reliability.
Resilient cushion has diversified forms, the rubber block as made of using rubber material.
Preferably, second connects as shown in fig. 7, resilient cushion is to be fixedly connected by bolt with the second pinboard 802
Plate 801 has the mounting hole for allowing resilient cushion to fill in, and resilient cushion is fixedly connected with the second connecting plate 801.Second pinboard 802 is logical
It crosses bolt to be attached with distance increasing unit, with easy disassembly, the second pinboard 802 has the through-hole for allowing bolt to pass through.
As shown in Figures 1 to 7, the second Auxiliary support component 8 further includes the third auxiliary branch connecting with the second connecting plate 801
Frame 804, third auxiliary stand 804 are located at the top of the second auxiliary stand 803.The setting of third auxiliary stand 804 improves
The structural strength of two Auxiliary support components 8 improves stability and reliability to distance increasing unit support.Third auxiliary stand 804
One end be fixedly connected with the second connecting plate 801, the other end of third auxiliary stand 804 and the first controller mounting plate 9 are fixed
Connection, the length of third auxiliary stand 804 are greater than the length of the second auxiliary stand 803, and third auxiliary stand 804 towards second is auxiliary
The back sweep of bracket 803 is helped to extend, the length direction and first direction of third auxiliary stand 804 and the second auxiliary stand 803
It is perpendicular, there is angle and the folder between the length direction of third auxiliary stand 804 and the length direction of the second auxiliary stand 803
Angle is acute angle.Second auxiliary stand 803 and third auxiliary stand 804 are the rod component with certain length, the second auxiliary branch
Frame 803, third auxiliary stand 804, the second connecting plate 801 and the second pinboard 802 material be steel alloy, the second auxiliary stand
803 upper end and the upper end of third auxiliary stand 804 and the second connecting plate 801 are to be welded to connect, under the second auxiliary stand 803
End is to be welded to connect with main support member.Second Auxiliary support component, 8 overall structural strength is high, to the stability of strutting system of distance increasing unit
It is good.
As shown in Figures 1 to 7, the second Auxiliary support component 8 further includes the third connecting plate connecting with main support member
805, the third pinboard 806 connecting for the second position with distance increasing unit and the resilient cushion being set on third connecting plate 805,
Third pinboard 806 is located at the side of third connecting plate 805 and third pinboard 806 is parallel with third connecting plate 805, third
Connecting plate 805 is parallel with main connecting plate 6, and third connecting plate 805 is located at the lower section of the second connecting plate 801 and third connecting plate
805 and second connecting plate 801 be on the same straight line parallel with second direction, third pinboard 806 and the second pinboard
802 are also on the same straight line parallel with second direction.One end of third connecting plate 805 and the fixed company of main support member
It connects, resilient cushion is set to the other end of third connecting plate 805, and third connecting plate 805 is located at the lower section of the second auxiliary stand 803.
The resilient cushion being set on third connecting plate 805 has elastic property, and resilient cushion can produce certain elastic deformation amount, to play
Cushioning effect, resilient cushion is fixedly connected with third pinboard 806 and resilient cushion is clipped in third connecting plate 805 and third pinboard
Between 806, and then effectiveness in vibration suppression can be played, vibration caused by decaying distance increasing unit realizes the flexible connection with distance increasing unit, mentions
High reliability.Resilient cushion has diversified forms, the rubber block as made of using rubber material.
Preferably, third connects as shown in fig. 7, resilient cushion is to be fixedly connected by bolt with third pinboard 806
Plate 805 has the mounting hole for allowing resilient cushion to fill in, and resilient cushion is fixedly connected with third connecting plate 805.Third pinboard 806 is logical
It crosses bolt to be attached with distance increasing unit, with easy disassembly, third pinboard 806 has the through-hole for allowing bolt to pass through.Third connection
The material of plate 805 is steel alloy, and third connecting plate 805 and main support member are to be welded to connect.
As shown in Figures 1 to 6, main support member further includes rear end reinforcement structure, rear end reinforcement structure and the second auxiliary branch
Knot is reinforced in support part part 8, the first controller mounting plate 9, the first main support 2, third main support 4 and the connection of the 4th main support 5, rear end
Structure and motor mounting plate 1 be it is positioned opposite, main connecting plate 6 is positioned at rear end reinforcement structure and motor mounting plate 1 between, rear end reinforcement
Structure is located at the rear side of distance increasing unit, and main connecting plate 6 is located at the front side of distance increasing unit, the first upper rack posts 201,401 and of third upper rack posts
One end of 4th upper rack posts 501 is fixedly connected with motor mounting plate 1, on the first upper rack posts 201, third upper rack posts 401 and the 4th
The other end of strut 501 is fixedly connected with rear end reinforcement structure.Rear end reinforcement structure be used for the body of hybrid power aeroplane into
Row connects and is detachable connection between rear end reinforcement structure and the body of hybrid power aeroplane, and rear end reinforcement structure is set
It sets, further improves the overall structural strength of main support member and the connection reliability with hybrid power aeroplane body.Make
To be preferred, rear end reinforcement structure includes center connecting rod 22, the first rear portion strut 17, the second rear portion strut 18, third rear portion
Strut 19, the 4th rear portion strut 20 and the 5th rear portion strut 21, the end of one end of the first rear portion strut 17 and the first upper rack posts 201
Portion is fixedly connected and the end of the first upper rack posts 201 is being connected with the body of hybrid power aeroplane for the first upper rack posts 201
One end, the other end of the first rear portion strut 17 is fixedly connected with a first controller mounting plate 9, first controller installation
Plate 9 is simultaneously attached by the body of bolt and hybrid power aeroplane, and the first rear portion strut 17 is used for first controller
Mounting plate 9 provides a supporting role, and the first rear portion strut 17 extends towards the top of the first upper rack posts 201, the first rear portion strut 17
Length direction it is parallel with second direction.One end of second rear portion strut 18 is fixedly connected with the end of the first upper rack posts 201
And first upper rack posts 201 the end be the first upper rack posts 201 the one end being connected with the body of hybrid power aeroplane, second
The other end of rear portion strut 18 is fixedly connected with center connecting rod 22, and the length direction of the second rear portion strut 18 is equal with first party
Row, the second rear portion strut 18 are located at the lower section of third auxiliary stand 804.One end of 5th rear portion strut 21 and center connecting rod 22
It is fixedly connected, the other end of the 5th rear portion strut 21 is fixedly connected with another the first controller mounting plate 9, third auxiliary stand
804 are also fixedly connected with the first controller mounting plate 9, and the 5th rear portion strut 21 and third auxiliary stand 804 are matched and be used for
One the first controller mounting plate 9 is provided a supporting role, the 5th rear portion strut 21 is located at the lower section of third auxiliary stand 804,
The length of 5th rear portion strut 21 is less than the length of the second auxiliary stand 803, and the 5th rear portion strut 21 is towards center connecting rod 22
Top extend, the second auxiliary stand 803 also towards center connecting rod 22 top extend, the lower end of the second auxiliary stand 803
Be fixedly connected with center connecting rod 22, the length direction of the length direction of the second auxiliary stand 803 and the 5th rear portion strut 21 it
Between there is angle and the angle to be acute angle.One end of third rear portion strut 19 be fixedly connected with the end of third upper rack posts 401 and
The end of third upper rack posts 401 is the one end of third upper rack posts 401 being connected with the body of hybrid power aeroplane, after third
The other end of portion's strut 19 is fixedly connected with center connecting rod 22, and third rear portion strut 19 is located under the second rear portion strut 18
Side has angle between the length direction of the second rear portion strut 18 and the length direction of third rear portion strut 19 and the angle is sharp
Angle, the length direction of third rear portion strut 19 and the length direction of center connecting rod 22 are perpendicular.
One end of 4th rear portion strut 20 be fixedly connected with the end of the 4th upper rack posts 501 and the 4th upper rack posts 501 should
End is the one end of the 4th upper rack posts 501 being connected with the body of hybrid power aeroplane, the other end of the 4th rear portion strut 20
It is fixedly connected with center connecting rod 22, between the length direction of the 4th rear portion strut 20 and the length direction of third rear portion strut 19
With angle and the angle is obtuse angle, and the length direction of the 4th rear portion strut 20 mutually hangs down with the length direction of center connecting rod 22
Directly, center connecting rod 22 is in sustained height with the end of the first upper rack posts 201 being connected with the body of hybrid power aeroplane,
Third rear portion strut 19 and the inclined downward of the 4th rear portion strut 20 towards center connecting rod 22 extend.
Center connecting rod 22, the first rear portion strut 17, the second rear portion strut 18, third rear portion strut 19, the 4th rear portion branch
Bar 20 and the 5th rear portion strut 21 are the rod component with certain length, center connecting rod 22, the first rear portion strut 17, second
Rear portion strut 18, third rear portion strut 19, the 4th rear portion strut 20 and the 5th rear portion strut 21 material be steel alloy, center connects
After extension bar 22 and the second auxiliary stand 803, the second rear portion strut 18, third rear portion strut 19, the 4th rear portion strut 20 and the 5th
Portion's strut 21 is to be welded to connect, and the first rear portion strut 17 and the second rear portion strut 18 and the first upper rack posts 201 are to be welded to connect, the
Three rear portion struts 19 are to be welded to connect with third upper rack posts 401, and the 4th rear portion strut 20 and the 4th upper rack posts 501 are that welding connects
It connects.
Preferably, in above-mentioned steps S1, main support member be by the body of bolt and hybrid power aeroplane into
Row connection namely the first upper rack posts 201, the second upper rack posts 301, third upper rack posts 401, the 4th upper rack posts 501 are connected with center
Bar 22 forms detachable connection by the body of bolt and hybrid power aeroplane, and this connection type is convenient for disassembly and assembly, correspondingly,
First upper rack posts 201, the second upper rack posts 301, third upper rack posts 401, the 4th upper rack posts 501 and center connecting rod 22, which have, allows spiral shell
The through-hole that bolt passes through.
Preferably, between the second main support 3 and main connecting plate 6, the body of hybrid power aeroplane and motor mounting plate 1
For detachable connection, the second main support 3 can be disassembled individually, and the end of the second lower fulcrum bar 302 is by bolt and main company
Fishplate bar 6 is attached, and the end of the second upper rack posts 301 is to be connect by bolt with motor mounting plate 1, the second lower fulcrum bar 302 with
Detachable connection is formed between main connecting plate 6, formed between the second upper rack posts 301 and motor mounting plate 1 it is detachable, second
The end of lower fulcrum bar 302 has the through-hole for allowing bolt to pass through.The end of first auxiliary stand 704 is to be connect by bolt with first
Plate 703 is attached, and the first auxiliary stand 704 has the through-hole for allowing bolt to pass through, the first auxiliary stand 704 and the first connecting plate
Detachable connection is formed between 703, also forms detachable connection between the first Auxiliary support component 7 and the 4th main support 5.
This connection type is convenient for disassembly and assembly, in above-mentioned steps S1, after by the second main support 3 and the disassembly of the first Auxiliary support component 7,
The side of main support member is in opening-wide state, and operating space is big, is convenient for the installation of distance increasing unit, when being also convenient for follow-up maintenance pair
Distance increasing unit is dismantled.
As shown in Figures 1 to 6, parallel two, two the first controller mounting plates are arranged in the first controller mounting plate 9
9 match, and provide a supporting role to the first controller, and in above-mentioned steps S3, the first controller is mounted on two by bolt
On first controller mounting plate 9, using the connection type of bolt, facilitate the dismounting of the first controller.
As shown in figs. 1,2 and 6, second controller is mounted on second controller mounting plate 10 by bolt, the
Two controller mounting plates 10 are directly installed on the body of hybrid power aeroplane, using the connection type of bolt, facilitate second
The dismounting of controller.The length direction of second controller mounting plate 10 is parallel with the length direction of the first controller mounting plate 9,
Second controller mounting plate 10 and the first controller mounting plate 9 are on the same straight line parallel with first direction, the second control
Device mounting plate 10 processed and the first controller mounting plate 9 are in sustained height, and multiple, Suo You is arranged in second controller mounting plate 10
Two controller mounting plates 10 match, and provide a supporting role to second controller.
In above-mentioned steps S1, pass through bolt first for the third position of the main pinboard 16 of main support member and distance increasing unit
It is attached, is then connected the second pinboard 802 and third connecting plate 805 and the second position of distance increasing unit by bolt
It connects, is then attached the first position of the first connecting plate 703 and distance increasing unit by bolt, then by the first Auxiliary support portion
The carriage mounting plate 701 of part 7 is attached by clip 705 and bolt with the 4th main support 5, then main by second by bolt
Bracket 3 is attached with motor mounting plate 1, is attached the first auxiliary stand 704 and the first connecting plate 703 by bolt,
Complete the installation of distance increasing unit.
In above-mentioned steps S1, before the installation for carrying out distance increasing unit, the first auxiliary stand 704 and the first connecting plate 703
In discrete state, the first Auxiliary support component 7 and the 4th main support 5 are also at discrete state, the first auxiliary stand 704 and
Two main supports 3 are structure as a whole, and the side of main support member is in opening-wide state, are convenient for distance increasing unit being put into main support member in this way
Inside.
It is by bolt that the first main support 2, the second main support 3, third main support 4 and the 4th is main in above-mentioned steps S2
Bracket 5 is attached with motor mounting plate 1, and then driving motor is mounted on motor mounting plate 1 by bolt, completes driving
The installation of motor.
In above-mentioned steps S3, the body of the first controller mounting plate 9 and hybrid power aeroplane is connected by bolt
It connects, then the first controller is mounted on the first controller mounting plate 9 by bolt, complete the installation of the first controller.
The assembly method of mixed power plant of the present invention include thes steps that as follows:
S4, second controller mounting plate 10 is mounted on the body of hybrid power aeroplane, second controller is mounted on
On second controller mounting plate 10.
In above-mentioned steps S4, second controller mounting plate 10 and the body of hybrid power aeroplane are connected by bolt
It connects, then second controller is mounted on second controller mounting plate 10 by bolt, completes the installation of second controller.
The present invention is exemplarily described in conjunction with attached drawing above.Obviously, present invention specific implementation is not by above-mentioned side
The limitation of formula.As long as using the improvement for the various unsubstantialities that the inventive concept and technical scheme of the present invention carry out；Or not
It is improved, above-mentioned conception and technical scheme of the invention are directly applied into other occasions, in protection scope of the present invention
Within.
Claims (10)
1. the assembly method of mixed power plant, which is characterized in that use integrated mounting system, integrated mounting system includes increasing journey
Device support device, motor mounting plate and the first controller mounting plate, the assembly method comprising steps of
S1, distance increasing unit support device is mounted on the body of hybrid power aeroplane, distance increasing unit is mounted on distance increasing unit support dress
It sets；
S2, motor mounting plate is mounted in distance increasing unit support device, driving motor is mounted on motor mounting plate；
S3, the first controller mounting plate is mounted on the body of hybrid power aeroplane, the first controller is mounted on the first control
On device mounting plate processed.
2. the assembly method of mixed power plant according to claim 1, which is characterized in that in the step S1, institute
Stating distance increasing unit support device is attached with three positions of distance increasing unit, and distance increasing unit support device includes first with distance increasing unit
First Auxiliary support component of position connection, the second Auxiliary support component and and distance increasing unit being connect with the second position of distance increasing unit
The connection of third position main support member, the first Auxiliary support component and the second Auxiliary support component and main support member connect
It connects.
3. the assembly method of mixed power plant according to claim 2, which is characterized in that the distance increasing unit support device
It is detachable connection between three positions of distance increasing unit.
4. the assembly method of mixed power plant according to claim 2 or 3, which is characterized in that the main support member
Including the first main support, the second main support, third main support, the 4th main support and with the first main support, the second main support,
The main connecting plate of three main supports and the connection of the 4th main support；In the step S2, the first main support, the second main support, third
Main support and the 4th main support are attached with the motor mounting plate.
5. the assembly method of mixed power plant according to claim 4, which is characterized in that first main support and institute
State the second main support be it is positioned opposite, the third main support and the 4th main support are positioned opposite, third main support position
In the lower section of the first main support, the 4th main support is located at the lower section of the second main support.
6. the assembly method of mixed power plant according to claim 4, which is characterized in that first main support includes
It the first upper rack posts that need to be attached with the motor mounting plate and is connect with the first upper rack posts and towards on the outside of the first upper rack posts
Stretch out the first lower fulcrum bar, second main support include the second upper rack posts being connect with the motor mounting plate and with second on
The second lower fulcrum bar stretched out on the outside of strut connection and the second upper rack posts of direction, the main connecting plate are located at the first lower fulcrum bar and second
It is connect between lower fulcrum bar and with the first lower fulcrum bar and the second lower fulcrum bar.
7. the assembly method of mixed power plant according to claim 6, which is characterized in that the third main support includes
It the third upper rack posts that need to be attached with the motor mounting plate and is connect with third upper rack posts and towards on the outside of third upper rack posts
The third lower fulcrum bar of stretching, the 4th main support include the 4th upper rack posts that need to be attached with motor mounting plate and with the 4th
Upper rack posts connection and towards the 4th lower fulcrum bar stretched out on the outside of the 4th upper rack posts, the main connecting plate are located at third lower fulcrum bar and the
It is connect between four lower fulcrum bars and with third lower fulcrum bar and the 4th lower fulcrum bar, third lower fulcrum bar is located under first lower fulcrum bar
Side, the 4th lower fulcrum bar are located at the lower section of second lower fulcrum bar.
8. according to the assembly method of any mixed power plant of claim 4 to 7, which is characterized in that described first is auxiliary
Help support member include the carriage mounting plate being connect with the 4th main support, the diagonal support being connect with carriage mounting plate, with
First connecting plate of diagonal support connection and the first pinboard connecting for the first position with distance increasing unit and it is clipped in first
Resilient cushion between connecting plate and the first pinboard, the first connecting plate be located at the third main support and the 4th main support it
Between.
9. the assembly method of mixed power plant according to claim 8, which is characterized in that in the step S1, institute
It states carriage mounting plate to be attached by clip and the 4th main support, hoop sleeve is set on the 4th main support and clip passes through
Fastener is attached with carriage mounting plate.
10. the assembly method of mixed power plant according to claim 8 or claim 9, which is characterized in that the first auxiliary branch
Support part part further includes the first auxiliary stand connecting with first connecting plate and second main support, the first auxiliary stand position
In the top of the diagonal support, in the step S1, the first auxiliary stand and the first connecting plate are connected by bolt
It connects.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810860422.4A CN108995826B (en) | 2018-08-01 | 2018-08-01 | Method for assembling hybrid power device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810860422.4A CN108995826B (en) | 2018-08-01 | 2018-08-01 | Method for assembling hybrid power device |
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| CN108995826B CN108995826B (en) | 2020-04-21 |
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| CN207403948U (en) * | 2017-11-13 | 2018-05-25 | 南京婆娑航空科技有限公司 | A kind of oil electric mixed dynamic unmanned plane dynamical system assembling framework |
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2018
- 2018-08-01 CN CN201810860422.4A patent/CN108995826B/en active Active
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203094307U (en) * | 2013-02-28 | 2013-07-31 | 重庆宗申发动机制造有限公司 | Power system arranging structure of oil-electric hybrid power tricycle |
| CN103921936A (en) * | 2014-02-12 | 2014-07-16 | 无锡汉和航空技术有限公司 | Oil and power mixed small unmanned helicopter and its power principle |
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