CN110254745A - A kind of modularization flying wing type multimachine body aircraft joining method - Google Patents
A kind of modularization flying wing type multimachine body aircraft joining method Download PDFInfo
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- CN110254745A CN110254745A CN201910478940.4A CN201910478940A CN110254745A CN 110254745 A CN110254745 A CN 110254745A CN 201910478940 A CN201910478940 A CN 201910478940A CN 110254745 A CN110254745 A CN 110254745A
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- parting surface
- wing
- joint structure
- abutting joint
- rapid abutting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- Manufacturing & Machinery (AREA)
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The invention discloses a kind of modularization flying wing type multimachine body aircraft joining methods, it is characterised in that comprises the following processes: establishing fuselage, wing parting surface in flying wing complete machine theory shape first, forms fuselage wing basic unit；Then rapid abutting joint structure is set on parting surface；Multimachine body is spliced and combined finally by rapid abutting joint structure.This method establishes a kind of modularization flying wing type multimachine body aircraft using pectinate texture realization quickly splicing by establishing the case unit and wing element of modular flying wing on the basis of traditional flying wing.
Description
Technical field
The invention belongs to aircraft digital design fields, are related to a kind of modularization flying wing type multimachine body aircraft joining method.
Background technique
Traditional flying wing is the aircraft that fuselage and wing combine together, and has lightweight construction, efficient loading
Greatly, the features such as flight resistance is small, and lift resistance ratio is high, and Stealth Fighter is good.But traditional flying wing due to aircaft configuration form from
It is just fixed up at the beginning of design, the maximum take-off weight of aircraft, farthest voyage, the parameters such as maximum loading capacity and weapon loading
Also it is just fixed up therewith, the cargo more than dead weight cannot be delivered, it cannot be according to the type sum number of the cargo delivered
Amount carries out flexibly adjustment, meets the multiple-task demand of the low high transport capacity of oil consumption.Meanwhile traditional flying wing is restricted
In the limitation that voyage and weapon load, airborne combat performance cannot be substantially improved by rapid refit, meet the farther cruise of army
With the mission requirements of stronger firepower.Since traditional flying wing mechanism is limited, it is not able to satisfy same airplane investigation, rescues
The demand of more role transformings and efficient task and the rapid structural replacement and maintenance of breakdown plane such as help, transport.
Summary of the invention
To solve the above-mentioned problems, the present invention provides a kind of modularization flying wing type multimachine body aircraft joining method, pass through
The case unit and wing element that modular flying wing is established on the basis of traditional flying wing, utilize pectination knot
Structure realizes quickly splicing, establishes a kind of modularization flying wing type multimachine body aircraft.
A kind of modularization flying wing type multimachine body aircraft joining method, includes the following steps:
Step 1 establishes fuselage, wing parting surface in flying wing complete machine theory shape, and it is substantially single to form fuselage wing
Member；
1 is respectively parallel to the aircraft plane of symmetry and builds in the theoretical shape position that two lateral extent of the plane of symmetry is 1/6 span of boarding a plane
Vertical fuselage, wing parting surface；
2 will be located at the part on the inside of parting surface as the case unit of modularization flying wing；
3 will be located at the part on the outside of parting surface as the wing element of modularization flying wing.
Rapid abutting joint structure is arranged in step 2 on parting surface, and detailed process is as follows:
1 case unit along on parting surface on the left of course be arranged rapid abutting joint structure；Rapid abutting joint structure, in fuselage list
The evagination pectination connector worked in coordination and indent pectination connector are provided on member and wing element parting surface.
2 case unit along on the right side of course be arranged with left side match and rapid abutting joint structure；
3 are arranged rapid abutting joint structure on along wing element on the left of course；
4 are arranged rapid abutting joint structure on along wing element on the right side of course.
Step 3 is spliced and combined multimachine body by rapid abutting joint structure, and detailed process is as follows:
1 splices multiple case units using the mutually matched rapid abutting joint structure on case unit parting surface,
Form case unit group.
2, by the rapid abutting joint structure on wing element parting surface, carry out quick with the case unit group spliced
Splicing, forms complete multimachine body flying wing, wherein splicing is as follows:
2-1 is by first case unit along the rapid abutting joint structure and second fuselage being arranged on parting surface on the right side of course
Unit is spliced along mutually matched rapid abutting joint structure is arranged on parting surface on the left of course；
2-1 is completed splicing part when needing the fuselage of the modular flying wing of more than two to dock by 2-2
It is fast along being arranged on parting surface on the left of course with third case unit along the rapid abutting joint structure being arranged on parting surface on the right side of course
Fast docking structure carries out pairing connection, and so on complete case unit group；
2-3 is by the rapid abutting joint structure being arranged on parting surface on the left of the suitable course of the case unit group of completion and along course
The rapid abutting joint structure being arranged on the parting surface of left side wing basic unit is spliced；
2-4 by the rapid abutting joint structure being arranged on parting surface on the right side of the suitable course of the part of the 2-3 splicing completed with it is suitable
Rapid structural on the right side of course on the parting surface of wing basic unit carries out quick pairing splicing, completes modularization flying wing type multimachine
The quick splicing of body aircraft.
The application is the utility model has the advantages that this patent proposes one kind by establishing modularization on the basis of traditional flying wing
Flying wing case unit and wing element, using pectinate texture realize quickly splicing, establish a kind of modularization all-wing aircraft
Formula multimachine body aircraft.Flying wing type multimachine body splices aircraft compared with traditional flying wing, has bigger loading capacity, bigger
Voyage, lower oil consumption, less aircrew, configuration flexibly, the features such as expansion is strong, maintenance is quick, meet investigation, rescue,
The efficient demands of different fields multitask such as transport.
Detailed description of the invention
The fuselage of Fig. 1 modularization flying wing, wing element structural exploded view.
Fig. 2 modularization flying wing multimachine body splices aircraft exploded view.
Fig. 3 modularization flying wing multimachine body splices aircraft constitutional diagram.
Explanation: 1, case unit is numbered in figure；2, wing element；3, indent pectination connector；4, evagination pectination connector；5, machine
Body unit group
Specific embodiment
As shown in Figure 1-3, a kind of modularization flying wing type multimachine body aircraft joining method, includes the following steps:
Step 1 establishes fuselage, wing parting surface in flying wing complete machine theory shape, and it is substantially single to form fuselage wing
Member；
1 is respectively parallel to the aircraft plane of symmetry and builds in the theoretical shape position that two lateral extent of the plane of symmetry is 1/6 span of boarding a plane
Vertical fuselage, wing parting surface；
2 will be located at the part on the inside of parting surface as the case unit 1 of modularization flying wing；
3 will be located at the part on the outside of parting surface as the wing element 2 of modularization flying wing.
Rapid abutting joint structure is arranged in step 2 on parting surface, and detailed process is as follows:
1 case unit 1 along on parting surface on the left of course be arranged rapid abutting joint structure；Rapid abutting joint structure, in fuselage
The evagination pectination connector 4 and indent pectination connector 3 worked in coordination are provided on 2 parting surface of unit 1 and wing element.
2 case unit 1 along on the right side of course be arranged with left side match and rapid abutting joint structure；
3 are arranged rapid abutting joint structure on along wing element 2 on the left of course；
4 are arranged rapid abutting joint structure on along wing element 2 on the right side of course.
Step 3 is spliced and combined multimachine body by rapid abutting joint structure, and detailed process is as follows:
1 splices multiple case units 1 using the mutually matched rapid abutting joint structure on case unit parting surface,
Form case unit group 5.
2, by the rapid abutting joint structure on wing element parting surface, carry out quickly with the case unit group 5 spliced
Splicing, forms complete multimachine body flying wing, wherein splicing is as follows:
2-1 is by first case unit 1 along the 3 rapid abutting joint knot of indent pectination connector being arranged on parting surface on the right side of course
Structure and second case unit 1 are along being arranged mutually matched 4 rapid abutting joint structure of evagination pectination connector on parting surface on the left of course
Spliced；
2-1 is completed splicing part when needing the fuselage of the modular flying wing of more than two to dock by 2-2
It is outer along what is be arranged on parting surface on the left of course along the indent pectination connector 3 and third case unit being arranged on parting surface on the right side of course
Convex pectination connector 4 carries out pairing connection, and so on complete the splicing of case unit group 5；
2-3 is by the evagination pectination connector 4 being arranged on parting surface on the left of the suitable course of the case unit group 5 of completion and along boat
The indent pectination connector 3 being arranged on the parting surface of wing basic unit to the left is spliced；
2-4 by the indent pectination connector 3 being arranged on parting surface on the right side of the suitable course of the part of the 2-3 splicing completed with it is suitable
Evagination pectination connector 4 on the right side of course on the parting surface of wing basic unit carries out quick pairing splicing, completes modularization all-wing aircraft
The quick splicing of formula multimachine body aircraft.
Claims (6)
1. a kind of modularization flying wing type multimachine body aircraft joining method, it is characterised in that include the following steps:
Step 1 establishes fuselage, wing parting surface in flying wing complete machine theory shape, forms fuselage wing basic unit；
Rapid abutting joint structure is arranged in step 2 on parting surface；
Step 3 is spliced and combined multimachine body by rapid abutting joint structure.
2. a kind of modularization flying wing type multimachine body aircraft joining method according to claim 1, it is characterised in that described
Step 1 comprises the following processes:
2-1 theoretical shape board a plane two lateral extent of the plane of symmetry be 1/6 span position be respectively parallel to the aircraft plane of symmetry establish
Fuselage, wing parting surface；
2-2 will be located at the part on the inside of parting surface as the case unit of modularization flying wing；
2-3 will be located at the part on the outside of parting surface as the wing element of modularization flying wing.
3. a kind of modularization flying wing type multimachine body aircraft joining method according to claim 1, it is characterised in that described
Step 2 comprises the following processes:
3-1 is in case unit along setting rapid abutting joint structure on parting surface on the left of course；
3-2 case unit along on the right side of course be arranged with left side match and rapid abutting joint structure；
Rapid abutting joint structure is arranged in 3-3 on along wing element on the left of course；
Rapid abutting joint structure is arranged in 3-4 on along wing element on the right side of course.
4. a kind of modularization flying wing type multimachine body aircraft joining method according to claim 1, it is characterised in that step 3 packet
Include following process:
4-1 splices multiple case units using the mutually matched rapid abutting joint structure on case unit parting surface, shape
At case unit group；
4-2 carries out fast Speed Pinyin by the rapid abutting joint structure on wing element parting surface, with the case unit group spliced
It connects, forms complete multimachine body flying wing.
5. a kind of modularization flying wing type multimachine body aircraft joining method according to claim 4, it is characterised in that described
Rapid abutting joint structure is provided with the evagination pectination connector worked in coordination and indent comb on case unit and wing element parting surface
Straight coupling.
6. a kind of modularization flying wing type multimachine body aircraft joining method according to claim 4, it is characterised in that described
Quick splicing is as follows in 4-2:
6-1 is by first case unit along the rapid abutting joint structure and second case unit being arranged on parting surface on the right side of course
Spliced along mutually matched rapid abutting joint structure is arranged on parting surface on the left of course；
6-1 is completed the suitable boat of splicing part when needing the fuselage of the modular flying wing of more than two to dock by 6-2
The rapid abutting joint structure being arranged on parting surface to the right is quick right along being arranged on parting surface on the left of course with third case unit
Binding structure carry out pairing connection, and so on complete case unit group splicing；
6-3 is by the rapid abutting joint structure being arranged on parting surface on the left of the suitable course of the case unit group of completion and along on the left of course
The rapid abutting joint structure being arranged on the parting surface of wing basic unit is spliced；
6-4 is by the rapid abutting joint structure being arranged on parting surface on the right side of the suitable course of the part of the 6-3 splicing completed and along course
Rapid structural on the parting surface of right side wing basic unit carries out quick pairing splicing, completes modularization flying wing type multimachine body and flies
The quick splicing of machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910478940.4A CN110254745A (en) | 2019-06-03 | 2019-06-03 | A kind of modularization flying wing type multimachine body aircraft joining method |
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| CN201910478940.4A CN110254745A (en) | 2019-06-03 | 2019-06-03 | A kind of modularization flying wing type multimachine body aircraft joining method |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110745232A (en) * | 2019-11-18 | 2020-02-04 | 西安爱生技术集团公司 | Modularization unmanned aerial vehicle fuselage butt-joint structural |
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| CN101384481A (en) * | 2005-07-07 | 2009-03-11 | 杰弗里·S·索姆 | Modular articulated-wing aircraft |
| US8292220B1 (en) * | 2009-03-19 | 2012-10-23 | Northrop Grumman Corporation | Flying wing aircraft with modular missionized elements |
| JP2012245831A (en) * | 2011-05-26 | 2012-12-13 | Kawada Kogyo Kk | Assembly structure of small unmanned aircraft |
| CN202686762U (en) * | 2012-05-25 | 2013-01-23 | 辽宁通用航空研究院 | Axisymmetric conjoined airplane of unit airplanes with flying wings |
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| CN110745232A (en) * | 2019-11-18 | 2020-02-04 | 西安爱生技术集团公司 | Modularization unmanned aerial vehicle fuselage butt-joint structural |
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Application publication date: 20190920 |