CN205221111U

CN205221111U - Modularization aircraft

Info

Publication number: CN205221111U
Application number: CN201520640957.2U
Authority: CN
Inventors: 田悦丰
Original assignee: Individual
Current assignee: Individual
Priority date: 2015-08-21
Filing date: 2015-08-21
Publication date: 2016-05-11
Anticipated expiration: 2025-08-21

Abstract

The utility model provides a modularization aircraft, includes drive arrangement module 1, linking module 2, bears module 3 and auxiliary module 4, drive arrangement module 1 with bear module 3 and make up into aircraft constitutional unit through linking module 2, bear module 3 and bearing the energy and load simultaneously, also regard as the fuselage structure of aircraft, alternative additional auxiliary module 4 among the constitutional unit for fill the not enough of above -mentioned module. This modularization aircraft has redistributed the energy and load, has changed the structure and has passed the power route, has optimized distributing of stress between the structure to solved that traditional aircraft mechanical structure is complicated, the problem is concentrated to load, makeed the unlimited benign expansion as required of this aircraft structure. Furthermore, the utility model discloses a modularization integrated configuration for universalization, standardization are realized to spare part in the aircraft.

Description

A kind of modular aircraft

Technical field

The utility model belongs to field of flight vehicle design, particularly relates to a kind of brand new of modular aircraft.

Background technology

Fuselage, the i.e. carrying platform of aircraft.Widely used is at present the aircraft with multiple stage actuating device, the composition of its fuselage is similar, primarily of " center loading plate ", horn and alighting gear composition, " center loading plate " and horn form the radial structure dispersed to periphery by a center-point, and this structure possesses the advantages such as structure is simple, lightweight when aircraft size is relatively little.Along with future is to the continuous demand of aircraft load capacity, the problem that this structure is brought is that actuating device is more, propellerpiston or the space occupied by actuating device larger, the size of fuselage must increase thereupon, development like this is gone down, and boat material, structural stress concentration problem can be more serious, need extra " weightening finish reinforcement " to make up the problems referred to above, in addition, the increase of airframe structure " deadweight " also can cut down the limited propulsive effort of actuating device, increase energy resource consumption.Assuming that ignore these, infinitely expand aircraft size, will inevitably cause because of propulsive effort by structural weight excessive loss, part-structure yield stress the chain reaction that brings, final structure is collapsed.

Utility model content

For solving the problem, the utility model provides a kind of modular aircraft, comprises actuating device module, link block, carrier module and supplementary module, and actuating device module and carrier module are combined into Flight Vehicle Structure unit by link block; Carrier module in the carrying energy and load simultaneously, also as the airframe structure of aircraft; Carrier module is provided with bearing space and the connection location with other modules or device; Link block is provided with the connection location with other modules or device.

Alternative additional supplementary module in Flight Vehicle Structure unit, supplementary module form is not fixed, and extensively, for filling up the deficiency of above-mentioned module, in whole Flight Vehicle Structure, part supplementary module even can play the effect replacing above-mentioned certain module in effect.Such as: when aircraft needs to carry the functional load such as imaging equipment, armament systems, radio system, namely supplementary module serves as connection hanger, is responsible for the attaching parts between said system and aircraft; When aircraft needs to carry large scale, irregularly shaped load, namely supplementary module serves as the attaching parts between load and aircraft.When carrier module place carrying battery and (or) other load weight larger time, supplementary module can be installed additional at structural unit place to increase the integrally-built Joint strenght of aircraft; When aircraft do not need carrying heavier load or carry more multiple-energy-source time, also can serve as connecting device between actuating device module with supplementary module, namely in aircraft, airframe structure is jointly arranged in pairs or groups by carrier module and supplementary module and is formed.

The modules quantity of composition Flight Vehicle Structure unit is N, N >=0.According to actual needs, each structural unit can have difference, and module number not etc., can matched combined arbitrarily between module.Owing to having redistributed the energy and load in structure, each structural unit all can provide separately power and bear load, makes this aircraft structurally can the unlimited optimum expansion of cumulative sum as required, and then improves continuation of the journey and load capacity.Can carry in carrier module but be not limited to actuating device module and produce the energy of propulsive effort, other load and auxiliary device.Described actuating device module, link block, carrier module and supplementary module all can be used as carrying or the carry region of other load.

On aircraft, actuating device module produces the energy needed for propulsive effort can be battery, fuel and other energy.If actuating device module is electric drive, its cell shapes and battery pack connection line can be arranged as required, can be arc surfaceds, circle, square etc.; If actuating device module is fuel driven, carrier module place can carry the fuel energies such as fuel oil.Can as required, battery (group) or fuel can be placed in carrier module outside face, also can partially or completely be placed in carrier module inner space.Battery (group) can also directly and actuating device model calling form aircraft fuselage framework, namely battery (group) is both for aircraft provides power source, again can directly as the attaching parts of vehicle airframe.

Carry-on link block and the relation between actuating device module and bogey module can be integral structure, movable structure, also can be assembled structures; The outer shape of carrier module does not limit, and as required, can be circular tube shaped, square tube type, half-round tubular, I shape, irregularly shaped etc.; Can be fixedly connected with between carry-on modules, also can be flexibly connected.

In sum, this modular aircraft has redistributed the energy and load, change structure load path, optimize distribution of stress between structure, thus solve that conventional aircraft mechanical structure is complicated, load concentration problem, make this Flight Vehicle Structure can unlimited optimum expansion as required.In addition, the utility model adopts modularization composite structure, makes parts in aircraft realize universalization, normalisation.

Accompanying drawing explanation

Fig. 1 a is the schematic diagram of modules in the utility model;

Fig. 1 b, 1c, 1d, 1e, 1f are structural unit schematic diagrams of the present utility model;

Fig. 2 a, 2b, 2c, 2d and 2e are the birds-eye vieies of the different embodiment of modularization of the present utility model;

Fig. 3 a and 3b is the birds-eye view of the utility model modularization specific embodiments;

Fig. 4 a and 4b is the modular embodiment birds-eye view of the utility model and partial side view;

Fig. 5 is the schematic diagram of the modular expansion embodiment of the utility model;

Fig. 6 is that modular one of the utility model expands embodiment schematic diagram;

Fig. 7 is that modular one of the utility model expands embodiment schematic diagram

Wherein, other load 7-screw propeller 8-center link block of 1-actuating device module 2-link block 3-carrier module 4-supplementary module 5-propellerpiston 6-

Detailed description of the invention

Be the schematic diagram of modules in the utility model as shown in Figure 1a, 1 is actuating device module, and 2 is link block, and 3 is carrier module, and 4 is supplementary module.

Being described in further details structural unit of the present utility model below, according to the configuration of existing aircraft, is all the energy with battery in present embodiment, and it is example that actuating device connects screw propeller.In Fig. 1 b, actuating device module 1 connects to form a structural unit with one end of carrier module 3 by link block 2, and link block 2 connects to form a structural unit with another carrier module 3 again simultaneously, by that analogy, can infinitely expand.In Fig. 1 c, the X-direction two ends of link block 2 connect carrier module 3 separately, and Y direction two ends separately connecting drive device module 1 form a structural unit, and actuating device module 1 is connected to form engine power group with screw propeller 7 again, by that analogy, can infinitely expand.In Fig. 1 d, carrier module 3 two ends are installed actuating device module 1 through link block 2 respectively and are formed a structural unit, and actuating device module 1 is connected with screw propeller 7, by that analogy, can infinitely expand.Fig. 1 f, actuating device module 1 is installed through link block 2 respectively in carrier module 3 two ends, simultaneously, a supplementary module 4 composition structural unit is jointly provided with below two link block 2 places, carrier module 3, each actuating device module 1 is connected with screw propeller 7 respectively, if the effect of the supplementary module in the present embodiment 4 is when bearing load weight is larger in carrier module 3, the Joint strenght between carrier module 3 and actuating device module 1 in structural unit can be increased.Fig. 1 e, actuating device module 1 connects to form a structural unit with one end of carrier module 3 by link block 2, can be connected with other load 6 below carrier module 3 by supplementary module 4.

About the modularization detailed description of the invention of aircraft, see Fig. 2 to Fig. 7.

Fig. 2 a, 2b, 2c, 2d and 2e are the birds-eye vieies of the different embodiment of modularization of the present utility model.Be respectively in figure and carry out modular combination with one end of carrier module 3 by the structural unit that link block 2 connects to form by actuating device module 1 and form.In figure, 5 is propellerpiston.Wherein, in Fig. 2 e, actuating device module 1 forms a structural unit by link block 2 and carrier module 3, actuating device module 1 forms a structural unit by link block 2 and supplementary module 4, all structural units are fixed on center link block 8 comprising modules aircraft in " annular " successively, what this figure showed is when needed for aircraft, load capacity is less, when all carrying battery or load without the need to all carrier modules 3, part carrier module 3 can be replaced by supplementary module 4, to alleviate aircraft weight.

As Fig. 3 a, link block 2 and carrier module 3 form structural unit, and multiple structural unit carries out combination centered by link block 2 to be fixed, and link block about 2 installs actuating device module 1 respectively, and actuating device module 1 is provided with screw propeller 7.

As Fig. 3 b, actuating device module 1, link block 2 and carrier module 3 form structural unit, and N number of structural unit " head and the tail connect " is combined into the modular aircraft of " annular " structure.Wherein, each actuating device module 1 is separately installed with screw propeller 7,5 is propellerpiston.

As Fig. 4 a, actuating device module 1, link block 2 and carrier module 3 form structural unit, and four structural units become modular aircraft according to rhombus framework combinations, are equipped with supplementary module 4 below aircraft, for carry load.Wherein, each actuating device module 1 is separately installed with screw propeller 7,5 is propellerpiston.Fig. 4 b is partial side view, is equipped with other load 6 below supplementary module 4.

Fig. 5, Fig. 6 and Fig. 7 are all schematic diagrams of the modular expansion embodiment of the utility model aircraft.Wherein, Fig. 5 is the unlimited expansion schematic diagram of Fig. 4 a, and Fig. 6 is the unlimited expansion schematic diagram of Fig. 2 e, and Fig. 7 is the unlimited expansion schematic diagram of Fig. 2 c.

Should be noted that, except above-mentioned embodiment, the utility model also has other embodiment a lot of certainly, such as, also can select in actuating device module with the driving engine of fuel driven or with the driving engine of other driven by energy, the equivalence made according to the utility model like this changes and amendment, and still belong to scope of the present utility model, former capital should be considered as further embodiment of the present utility model.

Claims

1. a modular aircraft, comprises actuating device module, link block, carrier module and supplementary module, it is characterized in that:

A. actuating device module and carrier module are combined into Flight Vehicle Structure unit by link block;

B. carrier module is the carrying energy and load while, also as the airframe structure of aircraft;

C. carrier module is provided with bearing space and the connection location with other modules or device;

D. link block is provided with the connection location with other modules or device;

E. in Flight Vehicle Structure unit, alternative is added with supplementary module, and supplementary module form is not fixed, and extensively, for filling up the deficiency of above-mentioned module, in whole Flight Vehicle Structure, part supplementary module even can play the effect replacing above-mentioned certain module in effect;

F. described Flight Vehicle Structure can the unlimited cumulative sum expansion of modularization.

2. a kind of modular aircraft according to claim 1, is characterized in that: the modules quantity of composition Flight Vehicle Structure unit is N, N >=0, matched combined arbitrarily as required between each module.

3. modular aircraft according to any one of claim 1 to 2, is characterized in that: the connecting device between the actuating device module of described aircraft can all be made up of carrier module as required, also jointly can be made up of supplementary module and carrier module.

4. modular aircraft according to claim 1, is characterized in that: described carrier module place can carry but be not limited to actuating device module and produce the energy of propulsive effort, load and other auxiliary device.

5. modular aircraft according to claim 1, is characterized in that: described actuating device module, link block, carrier module and supplementary module all can be used as carrying or the carry region of other load.

6. modular aircraft according to claim 1, is characterized in that: if the actuating device module of described aircraft is electric drive, its cell shapes can be arranged as required.

7. modular aircraft according to claim 1, is characterized in that: can be fixedly connected with between described carry-on modules, also can be to be flexibly connected.