CN108357673A - A kind of unmanned plane including modular extendable load cabin and function module - Google Patents
A kind of unmanned plane including modular extendable load cabin and function module Download PDFInfo
- Publication number
- CN108357673A CN108357673A CN201810322402.1A CN201810322402A CN108357673A CN 108357673 A CN108357673 A CN 108357673A CN 201810322402 A CN201810322402 A CN 201810322402A CN 108357673 A CN108357673 A CN 108357673A
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- Prior art keywords
- function module
- load cabin
- modular extendable
- extendable load
- unmanned plane
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- 230000003287 optical effect Effects 0.000 claims description 11
- 230000005484 gravity Effects 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 6
- 230000006870 function Effects 0.000 description 73
- 238000013461 design Methods 0.000 description 4
- 238000004891 communication Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 3
- 238000005070 sampling Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- KVCQTKNUUQOELD-UHFFFAOYSA-N 4-amino-n-[1-(3-chloro-2-fluoroanilino)-6-methylisoquinolin-5-yl]thieno[3,2-d]pyrimidine-7-carboxamide Chemical class N=1C=CC2=C(NC(=O)C=3C4=NC=NC(N)=C4SC=3)C(C)=CC=C2C=1NC1=CC=CC(Cl)=C1F KVCQTKNUUQOELD-UHFFFAOYSA-N 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007634 remodeling Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- 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
Abstract
The invention discloses a kind of unmanned planes including modular extendable load cabin and function module, including modular extendable load cabin and function module；The width of the modular extendable load cabin and the high width for being suitble to the function module and high size；The horizontal length of the function module be a datum length or be the datum length integral multiple, the horizontal length of the modular extendable load cabin is the integral multiple of the datum length；The cabin side wall of the modular extendable load cabin is provided with guide rail, for the sliding slot or bearing fit that are arranged in the function module, so that the track that the function module is limited along the guide rail is slid in or out the modular extendable load cabin；The inside of the modular extendable load cabin has multiple fixed grafting slot structures, for supporting multiple function module grafting；The bulkhead of the modular extendable load cabin is threaded hole, coordinates with the screw in the function module, for fastening the function module.
Description
Technical field
The present invention relates to air vehicle technique fields, include modular extendable load cabin and work(more particularly to one kind
The unmanned plane of energy module.
Background technology
Unmanned plane application at present includes mainly consumer level and industry-level.The unmanned plane of different purposes is in the gentle dynamic shape of appearance
Upper difference is apparent, and it is apparent by aircraft configuration to be influenced difference for space in corresponding fuselage, this cause various avionics in current aircraft,
The function modules installation site difference such as power, application load is very big, even same aerodynamic configuration unmanned plane is based on, for difference
Using to each function module shape, in cabin, position, power supply and data transmission will also carry out layout, cloth in special fuselage
Line, structure design and special counterweight setting etc..Such case greatly reduces unmanned aerial vehicle body space service efficiency, improves
Unmanned plane manufacturing cost and maintenance cost, limit unmanned plane Function Extension ability.Therefore, it urgently needs to unmanned aerial vehicle body
Inner space is standardized modularized design, effectively to promote unmanned aerial vehicle body inner space service efficiency and improve unmanned plane
The extended capability of application reduces the manufacturing cost and use cost of unmanned plane.
Thus, there is a need in the art for a kind of unmanned plane modular extendable load cabin structure and function modules：It can be solved
Some or all of certainly or at least mitigate in the presence of the above-mentioned prior art disadvantage.
Invention content
A kind of modular extendable load cabin of present invention offer is designed with functional module structure, is made especially suitable for unmanned plane
Fuselage extends load cabin and functional module structure design.
The technical solution adopted in the present invention is as described below.
According to the first aspect of the invention, it provides a kind of including nobody of modular extendable load cabin and function module
Machine, which is characterized in that the unmanned plane includes modular extendable load cabin and function module；
The width of the modular extendable load cabin and the high width for being suitble to the function module and high size；The function mould
The horizontal length of block be a datum length or be the datum length integral multiple, the water of the modular extendable load cabin
Flat length is the integral multiple of the datum length, preferably greater than 3 times, more preferably greater than 5 times, most preferably greater than 10 times；
The cabin side wall of the modular extendable load cabin is provided with guide rail, for the cunning that is arranged in the function module
Slot or bearing fit make the track that the function module is limited along the guide rail slide in or out the modular extendable load
Cabin；
The inside of the modular extendable load cabin has multiple fixed grafting slot structures, for supporting multiple work(
It can module grafting；
The bulkhead of the modular extendable load cabin is threaded hole, coordinates with the screw in the function module, uses
In the fastening function module.
Preferably, handle ring is arranged in the upper surface of the function module, for taking out function module from load cabin.
Preferably, the power supply interface of bottom surface or side the setting unified specification of the modular extendable load cabin, it is described
The grafting of supply line is completed when function module is inserted into the modular extendable load cabin.
Preferably, the data bus interface of ground or side the setting unified specification of the modular extendable load cabin,
The grafting of data/address bus is completed while the function module is inserted into the modular extendable load cabin.
Preferably, the screw in the function module is normal screws or hand the turn of the screw.
Preferably, the function module includes siding.
Preferably, tenon is arranged in the bulkhead of the modular extendable load cabin, with the function module edge mate.It is excellent
Selection of land, the tenon are the stress sections of one kind or nacelle itself in spring leaf or spring catch.
Preferably, the large-scale trepanning of below the bulkhead of the modular extendable load cabin or side setting, with it is described nobody
The trepanning cooperation being arranged on the shell of machine, completes optical imagery, or be easily installed holder convenient for the function module with optical lens
Gondola etc. need to run through the plug-in device of bulkhead.
Preferably, the function module can configure multiple functions, such as one-shot battery module, battery module, fuel electricity
Pond module, camera model, holder gondola module, avionic device module, communication module, radar module, atmospheric sampling module,
Throw module, storage and transportation module etc..
According to the second aspect of the invention, provide the first aspect of the present invention include modular extendable load cabin and
The unmanned plane assembly method of function module, which is characterized in that
Choose the function module that total length is equal to or less than the horizontal length of the modular extendable load cabin；
The quality and position of centre of gravity for obtaining each function module, the work(is determined according to the quality and position of centre of gravity
The erection sequence of energy module；
The function module slides into the modular extendable load cabin along the track that the guide rail limits；
Multiple function modules are fixed with multiple fixed grafting slot structures inside the modular extendable load cabin；
The bulkhead of the modular extendable load cabin is threaded hole with the screw in the function module to coordinate, is used
In the fastening function module.
Preferably, the grafting of supply line is completed when the function module is inserted into the modular extendable load cabin.
Preferably, the grafting of data/address bus is completed when the function module is inserted into the modular extendable load cabin.
Preferably, the screw in the function module is normal screws or hand the turn of the screw.
Preferably, the bulkhead setting tenon of the modular extendable load cabin and the function module edge mate, will
It is fixed.Preferably, the tenon is the stress section of one kind or nacelle itself in spring leaf or spring catch.
Preferably, the large-scale trepanning of below the bulkhead of the modular extendable load cabin or side setting, with it is described nobody
The trepanning cooperation being arranged on the shell of machine, the function module with optical lens completes optical imagery, or is easily installed holder
Gondola etc. need to run through the plug-in device of bulkhead.
Preferably, the function module can configure multiple functions, such as one-shot battery module, battery module, fuel electricity
Pond module, camera model, holder gondola module, avionic device module, communication module, radar module, atmospheric sampling module,
Throw module, storage and transportation module etc..
Modular extendable load cabin and the functional module structure design of the present invention, greatly improves unmanned plane application
Quick Extended ability improves the versatility of unmanned plane, saves unmanned plane application cost, improves being applicable in for unmanned plane
Property.
Description of the drawings
It with reference to the accompanying drawings will be to the feature, advantage of invention and the technical of illustrative embodiments and industrial meaning
Justice is described, and in the accompanying drawings, identical reference numeral indicates identical element, and wherein：
Fig. 1 shows that the unmanned plane according to exemplary embodiment of the invention, load cabin coordinate installation diagram with function module；
Fig. 2A-C show the modularization load cabin nacelle shape graphics of Fig. 1；
Fig. 3 shows the trepanning of load cabin large size and function module optical lens cooperation figure and B load cabins and the work(of A Fig. 1
It can module guide rail sliding slot engagement figure；
Fig. 4 show Fig. 1 A modularizations load cabin nacelle bottom and B nacelle internal-internals space divide figure (including
Grafting slot structure, guide rail, power supply interface, data bus interface, threaded hole, tenon, large-scale trepanning)；
Fig. 5 shows A load cabins and function module inserting groove engagement figure；B load cabins and function module for electrically engage figure and
Data sum total figure；C load cabins are schemed with the cooperation of function module threaded hole；D load cabins are closed with function module card shooting to be schemed.
Specific implementation mode
In the present invention, datum length is a length, is not some regular length, is in order to express easily to introduce
A kind of saying, this length can by those skilled in the art or by designer according to actual conditions oneself define.It is described
The length of function module is the integral multiple of the datum length or the datum length, such as 2 times, 3 times, 4 times or 5 times
More than.Such as the datum length is 1U, i.e. 70mm.
Exemplary embodiment of the invention is described in detail with reference to the accompanying drawings.Description to illustrative embodiments
Merely for the sake of demonstration purpose, and it is definitely not to the present invention and its application or the limitation of usage.Moreover, in figure each component size
Also it is only schematical with ratio, does not exactly correspond to actual product.
Fig. 1 shows the unmanned plane 1 according to exemplary embodiment of the invention, and load cabin 11 is matched with function module 12 to be attached together
Figure.The unmanned plane 1 includes a kind of modular extendable load cabin 11 and corresponding function module 12 for unmanned plane, real
It is as follows to apply mode：
1. modular functionality extends load cabin 11
1.1. there is the load nacelle that the normal width high thickness adapted to 1 size of unmanned plane is scaling up
11, the 9U modular functionalities that such as wide x high x thickness in an inner space is 126mm x100mm x630mm extend load cabin, such as Fig. 1
Shown in 2.
1.2. 11 inner space of nacelle is divided into the space that plurality of specifications complies with standard the integral multiple that width is U, has time
Between width summation be no more than nacelle 11 support total U numbers, to accommodate the module 12 of different in width U.If this example is 9U load cabins
11,11 space of nacelle is divided into the subspace of 3 specifications including 2U, 3U, 4U, the summation of three sub-spaces is 9U, is used for
Placement size is respectively that total U numbers of 12,3 function modules 12 of 2U, 3U, 4U specification function module are 9U, and 12 total U numbers of module are little
In the U numbers that module bay 11 is supported.As shown in Figure 2.Due to realizing fixation between module bay 11 and function module 12, module 12 is total
U numbers can be less than the U numbers that module bay 11 is supported.
1.4. 11 cabin side wall of load cabin is provided with guide rail 111, for in function module 12 sliding slot or bearing 121 match
It closes, function module 12 is made to slide in or out load cabin 11 along particular track.As shown in figure 3, the sliding slot of the big little modules of a 3u 12
121 and load cabin 11 guide rail 111 cooperation skid off load cabin 11.
1.5. multiple standard compliant fixed grafting slot structures 112 are arranged in the inside of nacelle 11, multiple meet mark for fixing
Accurate function module 12 (notice inserting column 122), supports unmanned plane flight that can be performed simultaneously multiple-task.Such as this example one
A example is the 9U modular functionalities load cabin 11 that the wide x high x thickness in inner space is 126mm x100mm x630mm, is provided with 9
The grafting simultaneously of standard 1U modules 12 that wide x high x thickness is 126mm x100mm x70mm, as shown in figure 4, supporting multiple integers simultaneously
The grafting simultaneously of the module 12 of times U sizes, such as supports 1U, 2U, 3U, as shown in Figure 5A.
1.6. the power supply interface 113 of 11 bottom surface of load cabin or side setting unified specification, module 12 are inserted into load cabin 11
The grafting of supply line is completed simultaneously.The power supply interface 113 of one XT60 is such as set in 11 side of 9U load cabins, and module 12 is inserted
After entering load cabin, power interface is connect with power supply interface, as shown in Figure 5 B.Power supply interface 113 is used for setting inside module 12
It is standby to be powered, to make it possible to play its function.
1.7. the data bus interface 114 of 11 bottom surface of load cabin or side setting unified specification, module 12 are inserted into load cabin
The grafting of data/address bus is completed while 11.The data bus interface of one RS232 is such as set in 11 side of 9U load cabins
114, after module 12 is inserted into load cabin, data-interface is connect with data bus interface, as shown in Figure 5 B.Data bus interface 114
It is communicated with the equipment inside module 12, such as the data transmission that inside modules equipment such as camera is collected is to load cabin
Memory on；Or the equipment into module 12 sends instruction.Data bus interface can also be passed through between disparate modules 12
114 carry out information exchange.
1.8. 11 bulkhead of load cabin is threaded hole 115, coordinates with the screw 125 in function module 12, for fastening work(
It can module 12.Screw is normal screws or hand the turn of the screw.As shown in Figure 5 C.
1.9. tenon 116 is arranged in 11 bulkhead of load cabin, and with 12 edge mate of function module, work(is quickly fixed for no tool
It can module 12.The mode of tenon 116 is one kind in spring leaf or spring catch.As used spring catch and bulkhead tenon in this example
116 cooperations, fixed function module 12, as shown in Figure 5 D.
1.10. the large-scale trepanning 117 of below 11 bulkhead of load cabin or side setting, coordinates with the trepanning on unmanned plane shell,
Optical imagery is completed convenient for the function module with optical lens, or be easily installed holder gondola etc. to hang through the outer of bulkhead
It is standby.Circular hole as opened a radius 30-60mm in this example below bulkhead carries out optical imagery operation for optical lens.Such as Fig. 3
It is shown.
2. the structure of function module 12
2.1. there are 1U, 2U, 3U, 4U until 8U specifications, can be adapted to and be fixed in modular functionality load cabin 11.Such as this reality
Example includes four function modules 12, and respectively wide x high x thickness is 1 piece of the 1U function modules of 126mm x100mm x70mm, wide x
High x thickness is 1 piece of the 2U function modules of 126mm x100mm x140mm, and wide x high x thickness is the 3U work(of 126mm x100mm x210mm
It can 2 pieces of module.The module for analogizing dimensions can be designed according to actual needs.As shown in Figure 2.
2.2. the quality of each function module 12 is measured, position of centre of gravity measures in advance and is labeled in 12 exposed table of module
Face, such as upper surface, using 12 center of gravity of module, in addition the center of aircraft itself, quickly calculates center of gravity of airplane Calculation of stowage on board tune
It is whole, see Fig. 5 D (128 mark).
2.3. 12 side wall of function module setting sliding slot or bearing 121, for matching with the guide rail 111 on 11 bulkhead of load cabin
It closes, function module 12 is made to slide in or out load cabin 11 along particular track.As in this example in 12 side wall sliding slot 121 of module and load
The guide rail 111 of 11 wall of cabin coordinates, and slides into load cabin 11.As shown in Figure 3.
2.4. 12 side wall of function module is threaded hole 125, and by normal screws or hand the turn of the screw and load cabin 11
Threaded hole 115 coordinate, be used for fastening function module 12.As used hand the turn of the screw by module threaded hole 125 and bulkhead in this example
Threaded hole 115 coordinates fixed module 12, as shown in Figure 5 C.
2.5. tenon 126 is arranged in 12 side wall of function module, with 11 edge mate of load cabin, is used for fixed function module 12.
The mode of tenon 126 can be spring leaf or spring catch.As used spring catch to be closed with 116 with bulkhead tenon in this example, fixed work(
Energy module 12, as shown in Figure 5 D.
2.6. 12 upper surface of function module setting handle ring 129, for taking out function module 12 from load cabin 11, such as
Shown in Fig. 5 D.For ease of use, one or more can be arranged in handle ring 129.
2.7. function module 12 can be according to being configured to multiple functions.Such as one-shot battery module, battery module, fuel cell
Module, holder gondola module, avionic device module, communication module, radar module, atmospheric sampling module, is thrown camera model
Throw module, storage and transportation module etc..The basic avionics module of 1U in such as this example, single electric camera model, the slr camera module of 2U or
The high capacity cell module or professional aviation measuring camera of photoelectric nacelle module and 3U.
Above embodiment example is only used for that the present invention is further explained, and is not used as limitation of the invention, practical
The limitation of the embodiment of attached drawing description is not limited in, such as the size of modular functionality load cabin 11 is not limited to 9U, and
It is the integral multiple of U, is determined according to 1 fuselage size of unmanned plane, as long as the integral multiple of 12 U of function module, and ensure to use
It is no more than space U numbers in cabin in the U number summations for being installed on all modules 12 in the same modular functionality load cabin 11.Only
Will be in the spirit of the present invention, the change and modification to embodiment described above are in claims of the present invention
In the range of.
In the present specification, whenever referring to " illustrative embodiments ", " preferred embodiment ", " embodiment " etc.
When mean for the embodiment description specific feature, structure or feature be included in the present invention at least one embodiment party
In formula.The appearance of these words different places in the present specification is not necessarily all referring to same embodiment.In addition, appointing when being directed to
When one embodiment/embodiment describes specific feature, structure or feature, it will be understood that those skilled in the art also can be
This feature, structure or feature are realized in other embodiment in all embodiments.
Embodiments of the present invention described in detail above.However, the aspect of the present invention is not limited to the above embodiment.
Without departing from the scope of the invention, various remodeling and replacement can be applied in the above embodiment.
Claims (10)
1. a kind of unmanned plane including modular extendable load cabin and function module, which is characterized in that described includes modularization
The unmanned plane of expansible load cabin and function module includes modular extendable load cabin and function module；
The width of the modular extendable load cabin and the high width for being suitble to the function module and high size；The function module
Horizontal length be a datum length or be the datum length integral multiple, the level of the modular extendable load cabin is long
Degree is the integral multiple of the datum length, preferably greater than 3 times, more preferably greater than 5 times, most preferably greater than 10 times；
The cabin side wall of the modular extendable load cabin is provided with guide rail, for the sliding slot being arranged in the function module or
Bearing fit makes the track that the function module is limited along the guide rail slide in or out the modular extendable load cabin；
The inside of the modular extendable load cabin has multiple fixed grafting slot structures, for supporting multiple function moulds
Block grafting；
The bulkhead of the modular extendable load cabin is threaded hole, coordinates with the screw in the function module, for tight
Gu the function module.
2. the unmanned plane according to claim 1 for including modular extendable load cabin and function module, which is characterized in that
Handle ring is arranged in the upper surface of the function module, for taking out function module from load cabin.
3. the unmanned plane according to claim 1 or 2 for including modular extendable load cabin and function module, feature exist
In the power supply interface of the bottom surface of the modular extendable load cabin or side setting unified specification, the function module is inserted into
The grafting of supply line is completed when the modular extendable load cabin.
4. the unmanned plane according to claim 1 or 2 for including modular extendable load cabin and function module, feature exist
In, the data bus interface of the ground of the modular extendable load cabin or side setting unified specification, the function module
The grafting of data/address bus is completed while being inserted into the modular extendable load cabin.
5. the unmanned plane according to claim 1 or 2 for including modular extendable load cabin and function module, feature exist
In tenon is arranged in the bulkhead of the modular extendable load cabin, with the function module edge mate.
6. the unmanned plane according to claim 1 or 2 for including modular extendable load cabin and function module, feature exist
In setting large-scale trepanning in below the bulkhead of the modular extendable load cabin or side is set on the shell of the unmanned plane
The trepanning cooperation set, completes optical imagery, or be easily installed holder gondola etc. to run through convenient for the function module with optical lens
The plug-in device of bulkhead.
7. a kind of unmanned plane assembly method including modular extendable load cabin and function module, which is characterized in that
Choose the function module that total length is equal to or less than the horizontal length of the modular extendable load cabin；
The quality and position of centre of gravity for obtaining each function module, the function mould is determined according to the quality and position of centre of gravity
The erection sequence of block；
The function module slides into the modular extendable load cabin along the track that the guide rail limits；
With multiple fixed multiple function module grafting of grafting slot structure inside the modular extendable load cabin；
The bulkhead of the modular extendable load cabin is threaded hole with the screw in the function module to coordinate, for tight
Gu the function module.
8. the unmanned plane assembly method according to claim 7 for including modular extendable load cabin and function module,
It is characterized in that, the grafting of supply line is completed when the function module is inserted into the modular extendable load cabin.
9. the unmanned plane assembly method according to claim 7 or 8 for including modular extendable load cabin and function module,
It is characterized in that, the function module completes the grafting of data/address bus when being inserted into the modular extendable load cabin.
10. the unmanned plane assembly side according to claim 7 or 8 for including modular extendable load cabin and function module
Method, which is characterized in that bulkhead setting tenon and the function module edge mate of the modular extendable load cabin, by it
It is fixed.
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| CN201810322402.1A CN108357673A (en) | 2018-04-11 | 2018-04-11 | A kind of unmanned plane including modular extendable load cabin and function module |
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| EP3854677A1 (en) * | 2020-01-23 | 2021-07-28 | BAE SYSTEMS plc | Airframe and method of assembling an airframe |
| EP3854678A1 (en) * | 2020-01-23 | 2021-07-28 | BAE SYSTEMS plc | Airframe and method of manufacturing an airframe |
| WO2021148775A1 (en) * | 2020-01-23 | 2021-07-29 | Bae Systems Plc | Airframe and method for assembling an airframe |
| WO2021148774A1 (en) * | 2020-01-23 | 2021-07-29 | Bae Systems Plc | Airframe and method of manufacturing an airframe |
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