CN207917157U - A kind of tiltrotor separate type shipping gondola - Google Patents

A kind of tiltrotor separate type shipping gondola Download PDF

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Publication number
CN207917157U
CN207917157U CN201721915721.0U CN201721915721U CN207917157U CN 207917157 U CN207917157 U CN 207917157U CN 201721915721 U CN201721915721 U CN 201721915721U CN 207917157 U CN207917157 U CN 207917157U
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China
Prior art keywords
tiltrotor
cabin
cabin ontology
undercarriage
gondola
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CN201721915721.0U
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Chinese (zh)
Inventor
王勇
王飞羽
王牧天
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Muyutian Aviation Technology Jiangsu Co ltd
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Mu Yu Aviation Technology (jiangsu) Co Ltd
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Abstract

A kind of tiltrotor disclosed by the utility model separate type shipping gondola, it include the cabin ontology on the lower front of the fuselage by being removably mounted tiltrotor, being constituted in the cabin ontology has a cabin for loading cargo, the bottom of the cabin ontology is provided with an Aircraft landing gear system, undercarriage of the Aircraft landing gear system one side as the tiltrotor when taking off or landing, is on the other hand used for the cabin ontology in ground moving.The separate type shipping gondola of the utility model is mounted on by dismountable mode on the lower front of the fuselage of tiltrotor, it 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

A kind of tiltrotor separate type shipping gondola
Technical field
The utility model is related to tiltrotor technical fields more particularly to a kind of tiltrotor to be hung with separate type shipping Cabin.
Background technology
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 separate type shipping gondola 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 separate type shipping gondola, includes the machine by being removably mounted tiltrotor Cabin ontology on the lower front of body, interior constitute of the cabin ontology have a cabin for loading cargo, the cabin sheet The bottom of body is provided with an Aircraft landing gear system, on the one hand the Aircraft landing gear system is rising as the tiltrotor On the other hand undercarriage when flying or landing is used for the cabin ontology 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 cabin ontology, the left rear side undercarriage, right lateral side undercarriage are separately positioned on the cabin The both sides at the bottom surface rear portion of ontology.
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 cabin for detecting it in real time A control processor is provided in ontology, the control processor is connect with each pressure sensor respectively, every for receiving One collected pressure signal of pressure sensor, and the cabin ontology is obtained to the progress calculation processing of these pressure signals and is existed Load the position of centre of gravity after cargo.
In a preferred embodiment of the utility model, one and the control process are additionally provided in the cabin ontology The alarm of device connection, when position of centre of gravity of the cabin ontology that the control processor calculation processing obtains after loading cargo is inclined When from normal range (NR), the control processor generates an alarm signal and the alarm signal is sent to the alarm, The alarm generates alarm after receiving the alarm signal, and notice loading personnel readjust the intrinsic cargo position of cabin It sets.
In a preferred embodiment of the utility model, the cabin ontology is additionally provided with one and the control processor The trim indicator of the position of centre of gravity for cabin ontology described in real-time display of connection.
As a result of technical solution as above, the beneficial effects of the utility model are:The separate type of the utility model Shipping gondola is mounted on by dismountable mode on the lower front of the fuselage of tiltrotor, can be filled on the ground in advance Loading object, then the separate type shipping gondola for being mounted with cargo is connect with the fuselage of idle tiltrotor, rotation of verting at this time Wing machine can loading flight, save load cargo the time it takes, improve the turnaround speed and conevying efficiency of cargo.This Outside, since the separate type shipping gondola of the utility model and the fuselage of tiltrotor use separation design, when separate type goods After fortune gondola is damaged, it is only necessary to be overhauled to the separate type shipping gondola of damage, the fuselage of tiltrotor can It carries other good separate type shipping gondolas to fly, efficiently solves existing tiltrotor flower in terms of maintenance The problem of taking the plenty of time 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 separate type shipping gondola of the utility model.
Fig. 2 is the front view of the separate type shipping gondola of the utility model.
Fig. 3 is the vertical view of the separate type shipping gondola of the utility model.
Fig. 4 is the upward view of the utility model.
Fig. 5 is the left view of the utility model.
Fig. 6 is the three dimensional structure diagram of the fuselage mating connection of the utility model and tiltrotor.
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 Fig. 1 to Fig. 5 and Fig. 6 is combined, what is provided in figure is a kind of tiltrotor separate type shipping gondola, including Pass through the cabin ontology 100 on the lower front for the fuselage 200 for being removably mounted tiltrotor, cabin ontology 100 Interior composition has a cabin for loading cargo.
The top of cabin ontology 100 is a plane 101, and peripheral region has been provided at circumferentially spaced several quick locking components (not shown), cabin ontology 100 are detachably connected by the main part of several quick locking components and fuselage 100 It connects.The bottom of cabin ontology 100 is provided with an Aircraft landing gear system, on the one hand which is used as tilting rotor On the other hand undercarriage of the machine when taking off or landing is used for cabin ontology 100 in ground moving, i.e., is hung as separate type shipping Movable pulley of the cabin in ground moving.Specifically, Aircraft landing gear system includes front left side undercarriage 110, forward right side undercarriage 120, left rear side undercarriage 130 and right lateral side undercarriage 140, front left side undercarriage 110 and forward right side undercarriage 120 are set respectively The bottom surface front part sides in cabin ontology 100 are set, left rear side undercarriage 130 and right lateral side undercarriage 140 are separately positioned on cabin The both sides at the bottom surface rear portion of ontology 100.
On front left side undercarriage 110, forward right side undercarriage 120, left rear side undercarriage 130 and right lateral side undercarriage 140 It is separately installed with pressure sensor 111,121,131,141, pressure sensor 111,121,131,141 is left front for detecting in real time The pressure that side undercarriage 110, forward right side undercarriage 120, left rear side undercarriage 130 and right lateral side undercarriage 140 are born.
Be provided with a control processor 150 in cabin ontology 100, control processor 150 respectively with pressure sensor 111, 121,131,141 connection, for receiving pressure sensor 111,121,131,141 collected pressure signals, and to these pressures Force signal carries out calculation processing and obtains position of centre of gravity of the cabin ontology 100 after loading cargo.
An alarm 160 being connect with control processor 150 is additionally provided in separate type shipping gondola 110, at control The cabin ontology 100 that reason 150 calculation processing of device obtains is when the position of centre of gravity after loading cargo deviates normal range (NR), control process Device 150 generates an alarm signal and the alarm signal is sent to alarm 160, and alarm 160 receives the alarm signal Alarm is generated afterwards, and notice loading personnel readjust the cargo location in cabin ontology 100.
Separate type shipping gondola 110 be additionally provided with one connect with control processor 150 be used for real-time display cabin ontology The trim indicator 170 of 100 position of centre of gravity, the personnel of loading can be according to the cabin ontology 100 shown by trim indicator 170 Position of centre of gravity, position of the adjustment cargo in cabin ontology 100, so that the position of centre of gravity symbol of the cabin ontology 100 after loading It closes and is required as defined in flight airmanship, ensure flight safety.
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 (5)

1. a kind of tiltrotor separate type shipping gondola, which is characterized in that including being verted by being removably mounted Cabin ontology on the lower front of the fuselage of gyroplane, interior constitute of the cabin ontology have a cabin for loading cargo, The bottom of the cabin ontology is provided with an Aircraft landing gear system, verts described in the Aircraft landing gear system one side conduct On the other hand undercarriage of the gyroplane when taking off or landing is used for the cabin ontology in ground moving.
2. tiltrotor as described in claim 1 separate type shipping gondola, which is characterized in that the undercarriage system System includes front left side undercarriage, forward right side undercarriage, left rear side undercarriage and right lateral side undercarriage, and the front left side is risen and fallen Frame, forward right side undercarriage are separately positioned on the bottom surface front part sides of the cabin ontology, and the left rear side undercarriage, right lateral side rise Fall the both sides that frame is separately positioned on the bottom surface rear portion of the cabin ontology.
3. tiltrotor as claimed in claim 2 separate type shipping gondola, which is characterized in that rise and fall in the front left side One is separately installed on frame, forward right side undercarriage, left rear side undercarriage and right lateral side undercarriage for detecting its carrying pressure in real time The pressure sensor of power, a control processor is provided in the cabin ontology, and the control processor is pressed with each respectively Force snesor connects, and is counted for receiving the collected pressure signal of each pressure sensor, and to these pressure signals Calculation handles to obtain position of centre of gravity of the cabin ontology after loading cargo.
4. tiltrotor as claimed in claim 3 separate type shipping gondola, which is characterized in that in the cabin ontology also It is provided with an alarm being connect with the control processor, when the cabin ontology that the control processor calculation processing obtains exists When loading the position of centre of gravity after cargo and deviateing normal range (NR), the control processor generates an alarm signal and by the alarm Signal is sent to the alarm, and the alarm generates alarm after receiving the alarm signal, and notice loading personnel are again Adjust the intrinsic cargo location of cabin.
5. tiltrotor as claimed in claim 3 separate type shipping gondola, which is characterized in that the cabin ontology is also set It is equipped with the trim indicator for the position of centre of gravity for cabin ontology described in real-time display that one connect with the control processor.
CN201721915721.0U 2017-12-31 2017-12-31 A kind of tiltrotor separate type shipping gondola Active CN207917157U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721915721.0U CN207917157U (en) 2017-12-31 2017-12-31 A kind of tiltrotor separate type shipping gondola

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721915721.0U CN207917157U (en) 2017-12-31 2017-12-31 A kind of tiltrotor separate type shipping gondola

Publications (1)

Publication Number Publication Date
CN207917157U true CN207917157U (en) 2018-09-28

Family

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CN201721915721.0U Active CN207917157U (en) 2017-12-31 2017-12-31 A kind of tiltrotor separate type shipping gondola

Country Status (1)

Country Link
CN (1) CN207917157U (en)

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GR01 Patent grant
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TR01 Transfer of patent right

Effective date of registration: 20240414

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

TR01 Transfer of patent right