CN208217008U - A kind of aircraft suspention cabin system - Google Patents
A kind of aircraft suspention cabin system Download PDFInfo
- Publication number
- CN208217008U CN208217008U CN201820473964.1U CN201820473964U CN208217008U CN 208217008 U CN208217008 U CN 208217008U CN 201820473964 U CN201820473964 U CN 201820473964U CN 208217008 U CN208217008 U CN 208217008U
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- CN
- China
- Prior art keywords
- aircraft
- gondola
- cabin
- lifting rope
- midair
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- Expired - Fee Related
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Abstract
The utility model relates to aircraft applications technical field, specifically a kind of aircraft suspends cabin system in midair.It includes aircraft and gondola, and the gondola includes cabin and hatch door, and cabin is equipped with the accommodating space for accommodating passenger；At least one lifting rope is connected at the top of the gondola, one end of lifting rope is connect with aircraft；The maximum weight bearing of aircraft is less than or equal to the weight of gondola.The technical program is connect by lifting rope with gondola by design aircraft, and the weight bearing of aircraft is not more than gondola weight, so that aircraft is only capable of dragging gondola movement, driving safety.
Description
Technical field
The utility model relates to aircraft applications technical field, specifically a kind of aircraft suspends cabin system in midair.
Background technique
With the continuous development of aircraft, aircraft using more and more extensive, especially unmanned plane；Unmanned plane is being applied
In be generally used for investigating, take pictures and transporting cargo etc. in the air；And unmanned plane transport passenger is used seldom to see, mainly pacify
Total factor is difficult to ensure.
Summary of the invention
Utility model aims to solve in the prior art, unmanned plane transports the problem of the safety deficiency of passenger,
A kind of aircraft suspention cabin system is provided, which can transport passenger safely.
A kind of aircraft suspention cabin system comprising aircraft and gondola, the gondola include cabin and hatch door, and cabin is set
There is the accommodating space for accommodating passenger；At least one lifting rope, one end of lifting rope and aircraft are connected at the top of the gondola
Connection；The maximum weight bearing of aircraft is less than or equal to the weight of gondola.
Further, the aircraft includes a base, and base is equipped with equally distributed multiple rotor assemblies.
Further, the aircraft is unmanned plane.
The beneficial effect of the technical program, the technical program is connect by lifting rope with gondola by design aircraft, and is flown
The weight bearing of row device is not more than gondola weight, so that aircraft is only capable of dragging gondola movement, and aircraft is separated with gondola, guarantees row
Safety is sailed, aircraft does not influence the safe handling of gondola, efficiently solves the manned safety issue of prior art unmanned plane.
The aircraft suspention cabin system of the utility model can be applied to the entertainment selection on the water surface or land.
Detailed description of the invention
Fig. 1 is a kind of schematic diagram of the utility model.
Appended drawing reference:
1 --- gondola；11 --- cabin；12 --- hatch door；2 --- lifting rope；3 --- base；4 --- rotor assemblies；
5 --- attachment base.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Referring to Fig. 1: a kind of aircraft suspention cabin system comprising aircraft and gondola 1, the aircraft are unmanned plane,
The gondola 1 includes cabin 11 and hatch door 12, and cabin 11 is equipped with the accommodating space for accommodating passenger；The top of the gondola 1
It is connected at least one lifting rope 2, one end of lifting rope 2 is connect with aircraft；The maximum weight bearing of aircraft is less than or equal to gondola 1
Weight.
In the technical program, using gondola 1 for accommodating passenger, hatch door 12 is for being sealed gondola 1.Aircraft
Weight bearing is not more than the weight of gondola 1, and within this range, aircraft can pull the movement of gondola 1 and the use of gondola 1 peace
Quan Xing.When the utility model is applied to amusement on water project, when gondola 1 is affixed on hydroplaning, high and low fall can be manually manufactured
Waterfall is hanging, can also manually manufacture water wave height fluctuating movement, can also increase inertia with movement speed and realize that great-jump-forward sky flies.When
Gondola 1 be equipped with lifting rope crispatura disk when, it can be achieved that various hanging fly or jump.
Preferably, seat is equipped in gondola 1；To facilitate passenger to take.To guarantee reliability of operation, lifting rope 2 be can be used
It more, when avoiding gondola 1 hanging suddenly, rotates.
Aircraft and gondola 1 are connected by lifting rope 2 in the technical program so that aircraft and gondola 1 be separated by it is certain away from
From the issuable noise of aircraft, vibration and fire etc. keep the passenger safety for riding on gondola 1 comfortable all far from gondola 1.
Simultaneously as the use of lifting rope 2, so that the distance between aircraft and gondola 1 have certain retractility, to realize practical
Novel flexibility and navigability.When gondola 1 lifting, slide with transverse shifting when, due to the presence of lifting rope 2 play it is certain
Buffer function can also make passenger increase comfort.
Aircraft is equipped with aircraft operation system, and gondola 1 is equipped with gondola operating system, aircraft operation system and gondola behaviour
It is independent mutually to make system, gondola operating system autonomous operation, safety flexibly, does not interfere with aircraft.Gondola 1 above and below passenger
When, it shuts down lower progress completely without aircraft, aircraft can be hovered over to the top of gondola 1, be not necessarily to aircraft gate.
Further, the aircraft includes a base 3, and base 3 is equipped with equally distributed multiple rotor assemblies 4.
Aircraft controls multiple rotor assemblies 4 by computer to provide lift, while the lift difference of different rotor assemblies 4 is given
Aircraft provides steering etc., and manipulation is convenient.
The top of cabin 11 is equipped with the attachment base 5 for connecting lifting rope 2.
Attachment base 5 is set at the top of cabin 11, can facilitate and be connect with lifting rope 2；It avoids not fixing.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
Claims (4)
1. a kind of aircraft suspends cabin system in midair, it is characterised in that: it includes aircraft and gondola, and the gondola includes cabin and cabin
Door, cabin are equipped with the accommodating space for accommodating passenger；At least one lifting rope, one end of lifting rope are connected at the top of the gondola
It is connect with aircraft；The maximum weight bearing of aircraft is less than or equal to the weight of gondola.
2. a kind of aircraft according to claim 1 suspends cabin system in midair, it is characterised in that: the aircraft includes a machine
Seat, base are equipped with equally distributed multiple rotor assemblies.
3. a kind of aircraft according to claim 2 suspends cabin system in midair, it is characterised in that: the top of cabin is equipped with for connecting
Connect the attachment base of lifting rope.
4. a kind of aircraft according to claim 1 suspends cabin system in midair, it is characterised in that: the aircraft is unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820473964.1U CN208217008U (en) | 2018-04-04 | 2018-04-04 | A kind of aircraft suspention cabin system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820473964.1U CN208217008U (en) | 2018-04-04 | 2018-04-04 | A kind of aircraft suspention cabin system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208217008U true CN208217008U (en) | 2018-12-11 |
Family
ID=64504502
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820473964.1U Expired - Fee Related CN208217008U (en) | 2018-04-04 | 2018-04-04 | A kind of aircraft suspention cabin system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208217008U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920897A (en) * | 2019-12-14 | 2020-03-27 | 赵海荣 | Aircraft rescue nacelle and control method |
-
2018
- 2018-04-04 CN CN201820473964.1U patent/CN208217008U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110920897A (en) * | 2019-12-14 | 2020-03-27 | 赵海荣 | Aircraft rescue nacelle and control method |
| CN110920897B (en) * | 2019-12-14 | 2021-09-03 | 赵海荣 | Aircraft rescue nacelle and control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181211 Termination date: 20210404 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |