CN108045549A - A kind of tiltrotor with separable function pod - Google Patents
A kind of tiltrotor with separable function pod Download PDFInfo
- Publication number
- CN108045549A CN108045549A CN201711495836.3A CN201711495836A CN108045549A CN 108045549 A CN108045549 A CN 108045549A CN 201711495836 A CN201711495836 A CN 201711495836A CN 108045549 A CN108045549 A CN 108045549A
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- gondola
- separate type
- tiltrotor
- undercarriage
- type shipping
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- 230000005484 gravity Effects 0.000 claims description 10
- 238000012545 processing Methods 0.000 claims description 6
- 230000032258 transport Effects 0.000 description 7
- 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
- 238000013461 design Methods 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
- 230000008859 change Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Tires In General (AREA)
Abstract
A kind of tiltrotor with separable function pod disclosed by the invention, including：One fuselage；It is horizontally installed on the left and right wing of the waist both sides；The left and right rotor for being separately positioned on the end of the left and right wing and being rotated respectively around the left and right wing；And one be arranged on empennage on the afterbody；The lower lateral front of the fuselage is a dismountable separate type shipping gondola for being used to load cargo.The present invention 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 connected 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 present invention relates to tiltrotor technical field more particularly to a kind of tilting rotors with separable function pod
Machine.
Background technology
Tiltrotor is a kind of course of new aircraft that fixed wing aircraft and helicopter feature combine together, and someone is vivid
It is called aerial " half-breed " on ground.Tiltrotor had not only had the ability of 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 level and upright position
Turn system component.The operation principle of tiltrotor is：When rotor vert system component it is in vertical position when, tiltrotor
It similar to DCB Specimen side-by-side helicopter, can hover, side flies, flies afterwards, 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, increase 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 so reduce the turnaround speed and conevying efficiency of cargo.In addition, it is used in tiltrotor
The cabin for loading cargo is normally located at fuselage interior, easily the cabin for being used to load cargo is caused to damage when loading cargo
Bad (fuselage is usually less likely to be damaged), once cabin is damaged, tiltrotor just can not fly, it is necessary to be carried out to the cabin of damage
On-call maintenance just allows to fly again, so can undoubtedly spend the substantial amounts of repair time, causes turnaround speed and the transport of cargo
Efficiency further reduces.For this purpose, applicant carried out beneficial explorations and trial, result of the above problems is had found, under
The technical solution that face will be introduced generates in this background.
The content of the invention
The technical problems to be solved by the invention：A kind of quickening cargo week rotating speed is provided in view of the deficiencies of the prior art
Degree, the tiltrotor with separable function pod for improving conevying efficiency.
Following technical scheme may be employed to realize in technical problem solved by the invention：
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；
The left and right rotation for being separately positioned on the end of the left and right wing and being rotated respectively around the left and right wing
The wing；And
One is arranged on 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 being used to load cargo.
In a preferred embodiment of the invention, the bottom of the separate type shipping gondola is provided with a undercarriage
System, undercarriage of the Aircraft landing gear system one side as the tiltrotor when taking off or landing, the opposing party
Face is for the separate type shipping gondola in ground moving.
In a preferred embodiment of the invention, the Aircraft landing gear system includes front left side undercarriage, forward right side
Undercarriage, left rear side undercarriage and right lateral side undercarriage, the front left side undercarriage, forward right side undercarriage are separately positioned on institute
The bottom surface front part sides of separate type shipping gondola are stated, the left rear side undercarriage, right lateral side undercarriage are separately positioned on described point
The both sides at the bottom surface rear portion from formula shipping gondola.
In a preferred embodiment of the invention, rise and fall in the front left side undercarriage, forward right side undercarriage, left rear side
One is separately installed on frame and right lateral side undercarriage and carries the pressure sensor of pressure, the separate type goods for detecting it in real time
A control processor is provided in fortune gondola, the control processor is connected respectively with each pressure sensor, for receiving
The pressure signal that each pressure sensor collects, and calculating processing is carried out to these pressure signals and obtains the separate type goods
Transport position of centre of gravity of the gondola after cargo is loaded.
In a preferred embodiment of the invention, it is additionally provided in the separate type shipping gondola at one and the control
Manage the alarm of device connection, the weight after separate type shipping gondola that the control processor calculating processing obtains is loading cargo
When normal range (NR) is deviateed in heart position, the control processor generates an alarm signal and is sent to the alarm signal described
Alarm, the alarm generate alarm after receiving the alarm signal, and notice loading personnel readjust separate type shipping
Cargo location in gondola.
In a preferred embodiment of the invention, the separate type shipping gondola is additionally provided with one and the control process
The trim indicator for the position of centre of gravity of separate type shipping gondola described in real-time display of device connection.
In a preferred embodiment of the invention, an aircraft support system is further included, the aircraft support system includes
First, second, third support undercarriage and first, second, third wheel-retracting gear being connected with aircraft control system,
The first support undercarriage is mounted on that one end of the left-handed wing away from its propeller by the first wheel-retracting gear
End in, it is described second support undercarriage by the second wheel-retracting gear be mounted on the dextrorotation wing away from its propeller
That one end end in, the 3rd support undercarriage is arranged on the bottom of the fuselage by the 3rd wheel-retracting gear
In rear side and positioned at the rear of the separate type shipping gondola.
In a preferred embodiment of the invention, the tiltrotor is unmanned tiltrotor.
As a result of technical solution as above, the beneficial effects of the present invention are：The present invention is by by the downside of fuselage
Forepart is arranged to a dismountable separate type shipping gondola, and separate type shipping gondola can load cargo on the ground in advance, then
The separate type shipping gondola for being mounted with cargo is connected with the fuselage of idle tiltrotor, tiltrotor can carry at this time
Object flies, and saves and loads cargo the time it takes, improves the turnaround speed and conevying efficiency of cargo.Further, since point
Separation design is used from formula shipping gondola and the fuselage of tiltrotor, after a certain separate type shipping gondola is damaged,
It only needs to overhaul the separate type shipping gondola of damage, the fuselage of tiltrotor can carry other good separation
Formula shipping gondola flies, and efficiently solves the problems, such as that existing tiltrotor is time-consuming in terms of maintenance,
Further improve conevying efficiency.
Description of the drawings
It in order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is attached drawing needed in technology description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of invention, for those of ordinary skill in the art, without creative efforts, can be with
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is the three dimensional structure diagram of the present invention.
Fig. 2 is the top view of the present invention.
Fig. 3 is the bottom view of the present invention.
Fig. 4 is the front view of the present invention.
Fig. 5 is the left view of the present invention.
Fig. 6 is the three dimensional structure diagram after present invention removal separate type shipping gondola.
Fig. 7 is the front view after present invention removal separate type shipping gondola.
Fig. 8 is the three dimensional structure diagram of the separate type shipping gondola of the present invention.
Fig. 9 is the front view of the separate type shipping gondola of the present invention.
Figure 10 is the top view of the separate type shipping gondola of the present invention.
Specific embodiment
In order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
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 afterbody of fuselage 100.In the present embodiment, originally
The tiltrotor of invention is unmanned tiltrotor.
The separate type shipping gondola 110 that the lower lateral front of fuselage 100 is removably used to load cargo for one, separate type goods
The top of gondola 110 is transported as 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, then the separate type shipping that will be mounted with cargo on the ground in advance
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
For undercarriage of the tiltrotor when taking off or landing, on the other hand for separate type shipping gondola 110 in ground moving, i.e.,
As movable pulley of the separate type shipping gondola in ground moving.Before Aircraft landing gear system includes front left side undercarriage 121, the right side
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
A control processor (not shown) is inside provided with, which is connected with each pressure sensor, is used for respectively
The pressure signal that each pressure sensor collects is received, and calculating processing is carried out to these pressure signals and obtains separate type goods
Transport position of centre of gravity of the gondola 110 after cargo is loaded.
An alarm (not shown) being connected 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 calculating processing obtains after cargo is loaded 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 be connected 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 requirement as defined in flight airmanship, ensures flight safety.
The tiltrotor with separable function pod of the present invention further includes an aircraft support system, aircraft support system
System include support undercarriage 500a, 500b, 500c and be connected with aircraft control system wheel-retracting gear 600a,
600b, 600c, support undercarriage 500a are mounted on left-handed wing 300a away from its propeller by wheel-retracting gear 600a
In the end of that one end, support undercarriage 500b is mounted on dextrorotation wing 300b away from its spiral by wheel-retracting gear 600b
In the end of that one end of paddle, after support undercarriage 500c is arranged on the bottom of fuselage 100 by wheel-retracting gear 600c
In side and positioned at the rear of separate type shipping gondola 110.(left and right rotor 300a, 300b are rotated after tiltrotor is landed
To plumbness), the separate type shipping that the tiltrotor of the present invention is placed in using the means of transport similar to ground ox trailer is hung
The lower section in cabin 110, and by tiltrotor integral jacking certain altitude, the flight control system of tiltrotor controls at this time
Fall frame jack 600a, 600b, 600c action so that support undercarriage 500a, 500b, 500c put down and be supported in ground
On, then the quick-locking mechanism between separate type shipping gondola 110 and fuselage 100 is unlocked so that separate type shipping
It separates and falls on means of transport between gondola 110 and fuselage 100, the haulagman of separate type shipping gondola 110 is carried in control
Tool declines certain altitude, and then separate type shipping gondola 110 leaves means of transport in tow, at this point, tiltrotor is (without separation
Formula 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 basic principles, main features and the advantages of the invention have been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the above embodiments and description only describe this
The principle of invention, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these changes
Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended 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；
The left and right rotor for being separately positioned on the end of the left and right wing and being rotated respectively around the left and right wing；With
And
One is arranged on 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 being used to load 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
Undercarriage when taking off or landing, on the other hand 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 connected with each pressure sensor, for receiving the pressure signal that each pressure sensor collects, and to these pressure
Signal carries out calculating processing and obtains position of centre of gravity of the separate type shipping gondola after cargo is loaded.
5. the tiltrotor with separable function pod as claimed in claim 4, which is characterized in that the separate type goods
An alarm being connected with the control processor is additionally provided in fortune gondola, is obtained when the control processor calculating 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 connected with the control processor
The trim indicator put.
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 first, second, third support undercarriage and are connected 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 away 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 away from its propeller, the 3rd support undercarriage passes through the 3rd 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 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 |
|---|---|---|---|
| CN201711495836.3A CN108045549A (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 |
|---|---|---|---|
| CN201711495836.3A CN108045549A (en) | 2017-12-31 | 2017-12-31 | A kind of tiltrotor with separable function pod |
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| Publication Number | Publication Date |
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| CN108045549A true CN108045549A (en) | 2018-05-18 |
Family
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| Application Number | Title | Priority Date | Filing Date |
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| CN201711495836.3A Pending CN108045549A (en) | 2017-12-31 | 2017-12-31 | A kind of tiltrotor with separable function pod |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108583890A (en) * | 2018-06-20 | 2018-09-28 | 滨州学院 | A kind of agriculture unmanned plane that can uniformly sow seeds |
| CN109878725A (en) * | 2019-03-31 | 2019-06-14 | 拓攻（南京）机器人有限公司 | A kind of fixed-wing logistics unmanned plane |
| CN111591440A (en) * | 2020-05-27 | 2020-08-28 | 湖南省仙鸟科技有限公司 | Sickle wing vertical take-off and landing aircraft |
| CN113753217A (en) * | 2021-09-19 | 2021-12-07 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft configuration with mission cabin |
| CN114043831A (en) * | 2021-11-01 | 2022-02-15 | 广东汇天航空航天科技有限公司 | Flying car |
| CN114212235A (en) * | 2021-12-30 | 2022-03-22 | 西安京东天鸿科技有限公司 | Aircraft, cargo carrying system, aircraft dismounting method and aircraft mounting method |
| CN116062205A (en) * | 2023-03-07 | 2023-05-05 | 四川腾盾科技有限公司 | Unmanned aerial vehicle with integral fuselage cargo hold throwing and recycling device and throwing method |
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