CN207902730U - A kind of tiltrotor with separable function pod - Google Patents
A kind of tiltrotor with separable function pod Download PDFInfo
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- CN207902730U CN207902730U CN201721915711.7U CN201721915711U CN207902730U CN 207902730 U CN207902730 U CN 207902730U CN 201721915711 U CN201721915711 U CN 201721915711U CN 207902730 U CN207902730 U CN 207902730U
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- gondola
- separate type
- tiltrotor
- undercarriage
- type shipping
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- 230000032258 transport Effects 0.000 description 6
- 238000000926 separation method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
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Abstract
A kind of tiltrotor with separable function pod disclosed by the utility model, including：One fuselage；It is horizontally installed on the left and right wing of the waist both sides；It is separately positioned on the end of the left and right wing and respectively around the left and right rotor of the left and right wing rotation；And the empennage that is arranged on the afterbody；The lower lateral front of the fuselage is a dismountable separate type shipping gondola for loading cargo.The utility model by the lower lateral front of fuselage by being arranged to a dismountable separate type shipping gondola, separate type shipping gondola can load cargo on the ground in advance, the separate type shipping gondola for being mounted with cargo is connect with the fuselage of idle tiltrotor again, at this time tiltrotor can loading flight, it saves and loads cargo the time it takes, improve the turnaround speed and conevying efficiency of cargo.
Description
Technical field
The utility model is related to tiltrotor technical field more particularly to a kind of verting with separable function pod
Gyroplane.
Background technology
Tiltrotor is a kind of course of new aircraft that fixed wing aircraft and helicopter feature combine together, someone's image
It is called aerial " half-breed " on ground.The tiltrotor not only ability with pure helicopter VTOL and hovering, but also tool
There is the ability of the high speed cruise flight of fixed wing aircraft.Tiltrotor is a kind of rotor craft of unique properties, be
At two wing tips of similar fixed wing aircraft wing, respectively incline equipped with a set of rotor that can be rotated between horizontal position and upright position
Turn system component.The operation principle of tiltrotor is：When rotor vert system component it is in vertical position when, tiltrotor
Similar to DCB Specimen side-by-side helicopter, can hover, side flies, it is rear fly, VTOL, landing runway can be removed from；When rotor verts
When system component is horizontal, tiltrotor is equivalent to fixed wing aircraft, can make high-speed remote flight, increases flight
Envelope curve.
With the high speed development of logistic industry, logistics service provider transports medium or short range cargo using tiltrotor,
To shorten the haulage time of medium or short range cargo, the conevying efficiency of medium or short range cargo is improved.However, tiltrotor loads goods every time
Object can devote a tremendous amount of time, and can reduce the turnaround speed and conevying efficiency of cargo in this way.In addition, being used in tiltrotor
The cabin for loading cargo is normally located at fuselage interior, is easy when loading cargo to causing to damage for loading the cabin of cargo
Bad (fuselage is usually less likely to be damaged), once cabin is damaged, tiltrotor just can not fly, and need to carry out the cabin of damage
On-call maintenance just allows to fly again, can undoubtedly spend a large amount of repair time in this way, leads to turnaround speed and the transport of cargo
Efficiency further decreases.For this purpose, applicant carried out beneficial exploration and trial, result of the above problems is had found, under
The technical solution that face will be introduced generates in this background.
Utility model content
Technical problem to be solved in the utility model：A kind of quickening cargo turnover is provided in view of the deficiencies of the prior art
Speed, the tiltrotor with separable function pod for improving conevying efficiency.
Following technical scheme may be used to realize in the technical issues of the utility model is solved：
A kind of tiltrotor with separable function pod, including：
One fuselage；
It is horizontally installed on the left and right wing of the waist both sides；
It is separately positioned on the end of the left and right wing and respectively around the left and right rotation of the left and right wing rotation
The wing；And
One is arranged the empennage on the afterbody；It is characterized in that,
The lower lateral front of the fuselage is a dismountable separate type shipping gondola for loading cargo.
In a preferred embodiment of the utility model, the bottom of the separate type shipping gondola is provided with an aircraft and rises
Fall frame system, the Aircraft landing gear system on the one hand undercarriage as the tiltrotor when taking off or landing, separately
On the one hand for the separate type shipping gondola in ground moving.
In a preferred embodiment of the utility model, the Aircraft landing gear system includes front left side undercarriage, the right side
Front side undercarriage, left rear side undercarriage and right lateral side undercarriage, the front left side undercarriage, forward right side undercarriage are respectively set
In the bottom surface front part sides of the separate type shipping gondola, the left rear side undercarriage, right lateral side undercarriage are separately positioned on institute
State the both sides at the bottom surface rear portion of separate type shipping gondola.
In a preferred embodiment of the utility model, in the front left side undercarriage, forward right side undercarriage, left rear side
It is separately installed with one on undercarriage and right lateral side undercarriage and carries the pressure sensor of pressure, the separation for detecting it in real time
A control processor is provided in formula shipping gondola, the control processor connect with each pressure sensor, is used for respectively
The collected pressure signal of each pressure sensor is received, and calculation processing is carried out to these pressure signals and obtains the separation
Position of centre of gravity of the formula shipping gondola after loading cargo.
In a preferred embodiment of the utility model, one and the control are additionally provided in the separate type shipping gondola
The alarm of processor connection processed, when the separate type shipping gondola that the control processor calculation processing obtains is after loading cargo
Position of centre of gravity when deviateing normal range (NR), the control processor generates an alarm signal and is simultaneously sent to the alarm signal
The alarm, the alarm generate alarm after receiving the alarm signal, and notice loading personnel readjust separate type
Cargo location in shipping gondola.
In a preferred embodiment of the utility model, the separate type shipping gondola is additionally provided with one and the control
The trim indicator of the position of centre of gravity for separate type shipping gondola described in real-time display of processor connection.
Further include an aircraft support system, the aircraft support system in a preferred embodiment of the utility model
Including the first, second, third support undercarriage and the first, second, third undercarriage control being connect with aircraft control system
Mechanism, the first support undercarriage are mounted on that far from its propeller of the left-handed wing by the first wheel-retracting gear
In the end of one end, the second support undercarriage is mounted on the dextrorotation wing far from its spiral shell by the second wheel-retracting gear
In the end for revolving that one end of paddle, the third support undercarriage is arranged by third wheel-retracting gear in the fuselage
Rear in bottom rear and positioned at the separate type shipping gondola.
In a preferred embodiment of the utility model, the tiltrotor is unmanned tiltrotor.
As a result of technical solution as above, the beneficial effects of the utility model are：The utility model is by by machine
The lower lateral front of body is arranged to a dismountable separate type shipping gondola, and separate type shipping gondola can load on the ground in advance
Cargo, then the separate type shipping gondola for being mounted with cargo is connect with the fuselage of idle tiltrotor, at this time tilting rotor
Machine can loading flight, save load cargo the time it takes, improve the turnaround speed and conevying efficiency of cargo.This
Outside, since separate type shipping gondola and the fuselage of tiltrotor use separation design, when a certain separate type shipping gondola is sent out
After raw damage, it is only necessary to be overhauled to the separate type shipping gondola of damage, the fuselage of tiltrotor can carry other
Good separate type shipping gondola flies, and efficiently solves existing tiltrotor when spending a large amount of in terms of maintenance
Between the problem of, further improve conevying efficiency.
Description of the drawings
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor
Under, other drawings may also be obtained based on these drawings.
Fig. 1 is the three dimensional structure diagram of the utility model.
Fig. 2 is the vertical view of the utility model.
Fig. 3 is the upward view of the utility model.
Fig. 4 is the front view of the utility model.
Fig. 5 is the left view of the utility model.
Fig. 6 is the three dimensional structure diagram after the utility model removal separate type shipping gondola.
Fig. 7 is the front view after the utility model removal separate type shipping gondola.
Fig. 8 is the three dimensional structure diagram of the separate type shipping gondola of the utility model.
Fig. 9 is the front view of the separate type shipping gondola of the utility model.
Figure 10 is the vertical view of the separate type shipping gondola of the utility model.
Specific implementation mode
In order to make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, under
Face combines and is specifically illustrating, and the utility model is expanded on further.
Referring to attached drawing, what is provided in figure is a kind of tiltrotor with separable function pod, including fuselage 100,
Left and right wing 200a, 200b, left and right rotor 300a, 300b and empennage 400.Left and right wing 200a, 200b are horizontally installed on machine
The on both sides of the middle of body 100.Left and right rotor 300a, 300b are separately positioned on the end of left and right wing 200a, 200b and difference
It is rotated around left and right wing 200a, 200b.Empennage 400 is arranged on the tail portion of fuselage 100.In the present embodiment, originally
The tiltrotor of utility model is unmanned tiltrotor.
The lower lateral front of fuselage 100 is a dismountable separate type shipping gondola 110 for loading cargo, separate type goods
The top for transporting gondola 110 is a plane 111, and can be carried out by the main part of several quick locking components and fuselage 100
It is detachably connected.Separate type shipping gondola 110 can load cargo on the ground in advance, then the separate type shipping that will be mounted with cargo
Gondola 110 and the fuselage of tiltrotor of free time are attached, at this time tiltrotor can loading flight, save loading
Cargo the time it takes improves the turnaround speed and conevying efficiency of cargo.Further, since separate type shipping gondola 110 with
The fuselage 100 of tiltrotor uses separation design, after a certain separate type shipping gondola is damaged, it is only necessary to damage
Separate type shipping gondola overhauled, and the fuselage of the tiltrotor without damage can carry other good separate types
Shipping gondola flies, and efficiently solves the problems, such as that existing tiltrotor is time-consuming in terms of maintenance, into
One step improves conevying efficiency.
The bottom of separate type shipping gondola 110 is provided with an Aircraft landing gear system, on the one hand Aircraft landing gear system is made
On the other hand in ground moving, i.e., the undercarriage for being tiltrotor when taking off or landing is used for separate type shipping gondola 110
As movable pulley of the separate type shipping gondola in ground moving.Aircraft landing gear system includes front left side undercarriage 121, it is right before
Side undercarriage 122, left rear side undercarriage 123 and right lateral side undercarriage 124, front left side undercarriage 121 and forward right side undercarriage
122 are separately positioned on the bottom surface front part sides of separate type shipping gondola 110, left rear side undercarriage 123 and right lateral side undercarriage 124
It is separately positioned on the both sides at the bottom surface rear portion of separate type shipping gondola 110.
On front left side undercarriage 121, forward right side undercarriage 122, left rear side undercarriage 123 and right lateral side undercarriage 124
It is separately installed with one and carries the pressure sensor (not shown) of pressure, separate type shipping gondola 110 for detecting it in real time
It is inside provided with a control processor (not shown), which connect with each pressure sensor, be used for respectively
The collected pressure signal of each pressure sensor is received, and calculation processing is carried out to these pressure signals and obtains separate type goods
Transport position of centre of gravity of the gondola 110 after loading cargo.
An alarm (not shown) being connect with control processor is additionally provided in separate type shipping gondola 110, when
Position of centre of gravity of the separate type shipping gondola 110 that control processor calculation processing obtains after loading cargo deviates normal range (NR)
When, control processor generates an alarm signal and the alarm signal is sent to alarm, and alarm receives the alarm signal
Alarm is generated after number, notice loading personnel readjust the cargo location in separate type shipping gondola.
Separate type shipping gondola 110 be additionally provided with one connect with control processor hung for real-time display separate type shipping
The trim indicator (not shown) of the position of centre of gravity in cabin 110, the personnel of loading can be according to the separation shown by trim indicator
The position of centre of gravity of formula shipping gondola 110, position of the adjustment cargo in separate type shipping gondola 110, so that point after loading
Position of centre of gravity from formula shipping gondola meets to be required as defined in flight airmanship, ensures flight safety.
The tiltrotor of separable function pod that has of the utility model further includes an aircraft support system, aircraft branch
Support system include support undercarriage 500a, 500b, 500c and connect with aircraft control system wheel-retracting gear 600a,
600b, 600c, support undercarriage 500a are mounted on left-handed wing 300a far from its propeller by wheel-retracting gear 600a
In the end of that one end, support undercarriage 500b is mounted on dextrorotation wing 300b far from its spiral shell by wheel-retracting gear 600b
In the end for revolving that one end of paddle, support undercarriage 500c is arranged by wheel-retracting gear 600c in the bottom of fuselage 100
Rear in rear side and positioned at separate type shipping gondola 110.(left and right rotor 300a, 300b turn after tiltrotor is landed
Move to plumbness), the separate type of the tiltrotor of the utility model is placed in using the means of transport similar to ground ox trailer
The lower section of shipping gondola 110, and by tiltrotor integral jacking certain altitude, the at this time flight control system of tiltrotor
Control wheel-retracting gear 600a, 600b, 600c action so that support undercarriage 500a, 500b, 500c put down and be supported in
On ground, then the quick-locking mechanism between separate type shipping gondola 110 and fuselage 100 is unlocked so that separate type
It detaches and is fallen on means of transport between shipping gondola 110 and fuselage 100, the fortune of separate type shipping gondola 110 is carried in control
Defeated tool declines certain altitude, and then separate type shipping gondola 110 leaves means of transport in tow, at this point, tiltrotor (is free of
Separate type shipping gondola) it is supported by support undercarriage 500a, 500b, 500c and is maintained at original height.Support undercarriage
500a, 500b, 500c only play a supporting role, and structural strength need not make the intensity with normal undercarriage.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the present utility model is not limited to the above embodiments, described in above embodiments and description
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (8)
1. a kind of tiltrotor with separable function pod, including：
One fuselage；
It is horizontally installed on the left and right wing of the waist both sides；
It is separately positioned on the end of the left and right wing and respectively around the left and right rotor of the left and right wing rotation；With
And
One is arranged the empennage on the afterbody；It is characterized in that,
The lower lateral front of the fuselage is a dismountable separate type shipping gondola for loading cargo.
2. the tiltrotor with separable function pod as described in claim 1, which is characterized in that the separate type goods
The bottom of fortune gondola is provided with an Aircraft landing gear system, on the one hand the Aircraft landing gear system is used as the tiltrotor
On the other hand undercarriage when taking off or landing is used for the separate type shipping gondola in ground moving.
3. the tiltrotor with separable function pod as claimed in claim 2, which is characterized in that the aircraft takeoffs and landings
Frame system includes front left side undercarriage, forward right side undercarriage, left rear side undercarriage and right lateral side undercarriage, and the front left side rises
Fall frame, forward right side undercarriage is separately positioned on the bottom surface front part sides of the separate type shipping gondola, the left rear side undercarriage,
Right lateral side undercarriage is separately positioned on the both sides at the bottom surface rear portion of the separate type shipping gondola.
4. the tiltrotor with separable function pod as claimed in claim 3, which is characterized in that in the front left side
One is separately installed on undercarriage, forward right side undercarriage, left rear side undercarriage and right lateral side undercarriage to hold for detecting it in real time
The pressure sensor of pressure is carried, a control processor, the control processor difference are provided in the separate type shipping gondola
It is connect with each pressure sensor, for receiving the collected pressure signal of each pressure sensor, and to these pressure
Signal carries out calculation processing and obtains position of centre of gravity of the separate type shipping gondola after loading cargo.
5. the tiltrotor with separable function pod as claimed in claim 4, which is characterized in that the separate type goods
It is additionally provided with an alarm being connect with the control processor in fortune gondola, is obtained when the control processor calculation processing
For separate type shipping gondola when the position of centre of gravity after loading cargo deviates normal range (NR), the control processor generates an alarm
The alarm signal is simultaneously sent to the alarm by signal, and the alarm generates alarm after receiving the alarm signal,
Notice loading personnel readjust the cargo location in separate type shipping gondola.
6. the tiltrotor with separable function pod as claimed in claim 5, which is characterized in that the separate type goods
Fortune gondola is additionally provided with a center of gravity position for separate type shipping gondola described in real-time display being connect with the control processor
The trim indicator set.
7. the tiltrotor with separable function pod as described in claim 1, which is characterized in that further include an aircraft
Support system, the aircraft support system include the first, second, third support undercarriage and are connect with aircraft control system
First, second, third wheel-retracting gear, the first support undercarriage are mounted on institute by the first wheel-retracting gear
In the end for stating that one end of the left-handed wing far from its propeller, the second support undercarriage passes through the second wheel-retracting gear
In the end of described that one end of the dextrorotation wing far from its propeller, the third support undercarriage passes through third undercarriage
Jack is arranged in the bottom rear of the fuselage and positioned at the rear of the separate type shipping gondola.
8. the tiltrotor with separable function pod as described in any one of claim 1 to 7, which is characterized in that
The tiltrotor is unmanned tiltrotor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721915711.7U CN207902730U (en) | 2017-12-31 | 2017-12-31 | A kind of tiltrotor with separable function pod |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721915711.7U CN207902730U (en) | 2017-12-31 | 2017-12-31 | A kind of tiltrotor with separable function pod |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207902730U true CN207902730U (en) | 2018-09-25 |
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ID=63566192
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721915711.7U Active CN207902730U (en) | 2017-12-31 | 2017-12-31 | A kind of tiltrotor with separable function pod |
Country Status (1)
| Country | Link |
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| CN (1) | CN207902730U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045549A (en) * | 2017-12-31 | 2018-05-18 | 上海牧羽航空科技有限公司 | A kind of tiltrotor with separable function pod |
| CN112046754A (en) * | 2019-06-05 | 2020-12-08 | 北京京东尚科信息技术有限公司 | Externally hung box body and fixed-wing aircraft |
-
2017
- 2017-12-31 CN CN201721915711.7U patent/CN207902730U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045549A (en) * | 2017-12-31 | 2018-05-18 | 上海牧羽航空科技有限公司 | A kind of tiltrotor with separable function pod |
| CN112046754A (en) * | 2019-06-05 | 2020-12-08 | 北京京东尚科信息技术有限公司 | Externally hung box body and fixed-wing aircraft |
| CN112046754B (en) * | 2019-06-05 | 2022-12-27 | 北京京东乾石科技有限公司 | Externally hung box body and fixed-wing aircraft |
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| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240409 Address after: 214116 Zone B2, Ehu Packaging City, Ehu Town, Xishan District, Wuxi City, Jiangsu Province 3379 Patentee after: Muyutian Aviation Technology (Jiangsu) Co.,Ltd. Country or region after: China Address before: 214028 No. 75, Shuo Fang Yu An Road, new Wu District, Wuxi, Jiangsu Patentee before: MUYU AVIATION TECHNOLOGY (JIANGSU) Co.,Ltd. Country or region before: China |