CN109649633A - A kind of fixed wing aircraft shell that wing frame eyelid retractor is easy to assembly and stable - Google Patents
A kind of fixed wing aircraft shell that wing frame eyelid retractor is easy to assembly and stable Download PDFInfo
- Publication number
- CN109649633A CN109649633A CN201811652366.1A CN201811652366A CN109649633A CN 109649633 A CN109649633 A CN 109649633A CN 201811652366 A CN201811652366 A CN 201811652366A CN 109649633 A CN109649633 A CN 109649633A
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- wing
- airframe
- aircraft
- block
- stable
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- 210000000744 eyelid Anatomy 0.000 title claims abstract description 54
- 230000001681 protective effect Effects 0.000 claims abstract description 8
- 238000005286 illumination Methods 0.000 claims abstract description 6
- 239000002184 metal Substances 0.000 claims description 40
- 238000003466 welding Methods 0.000 claims description 25
- 230000003014 reinforcing effect Effects 0.000 claims description 8
- 230000000903 blocking effect Effects 0.000 claims description 4
- 230000002787 reinforcement Effects 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 7
- 238000010586 diagram Methods 0.000 description 5
- 239000007787 solid Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000024703 flight behavior Effects 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
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- 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
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
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- 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
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- 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
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/02—Tailplanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/06—Fins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/08—Stabilising surfaces mounted on, or supported by, wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/02—Mounting or supporting thereof
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of fixed wing aircraft shells that wing frame eyelid retractor is easy to assembly and stable, including properller and airframe, the properller is fixed on the front end middle position of airframe, the two sides of the properller, which are located on airframe, is provided with illumination protective cover, pass through side arc block, intermediate convex block, top planes block, wing frame eyelid retractor composed by inclined-plane support column and bottom holders is more convenient when connection, pass through the intermediate convex block on top planes block, allow to good grafting to live, to more convenient when fixed by screw, and the bottom holders of wing frame eyelid retractor are connected on airframe, and top planes block is fixed on aircraft flank by intermediate convex block, make inclined-plane support column that there is good pulling force and supporting role in this way, to pass through side The reinforcement of arc block is stablized, so that top junction forms stable triangle, thus more stable when high speed uses.
Description
Technical field
The invention belongs to related fixed wing aircraft technical fields, and in particular to a kind of wing frame eyelid retractor is easy to assembly and stablizes
Fixed wing aircraft shell.
Background technique
Fixed wing aircraft is referred to as aircraft, refers to and generates the thrust advanced or pulling force by power device, by the fixation of fuselage
Wing generates lift, in the aircraft for overweighting air of endoatmosphere flight.It is one kind of Fixed-Wing, and most often
The one kind seen, another Fixed-Wing are aerodones.The engine type that aircraft is used according to it can be divided into jet again
Aircraft and propeller aeroplane.The housing construction of aircraft generally includes wing, fuselage, empennage and undercarriage composition.If aircraft
Engine is not in fuselage, then engine nacelle also belongs to a part of housing construction.With the development of electronic technology, flight behaviour
The variation of essence also has occurred in the form of vertical device.In large aircraft, traditional mechanical manipulation system gradually by
Replaced more advanced fly-by-wire, computer system intervenes flight control system comprehensively, and the operation of driver is not
Again seem direct operating aircraft movement, and is more like and assigns movement instruction to aircraft.
Existing fixed wing aircraft wing frame eyelid retractor technology has the following problems: 1, existing fixed wing aircraft wing frame support
It is not very convenient when the wing of side that device is fixed on, and needs to buttress wing frame eyelid retractor on the other hand, another hand is fixed, in this way
It is easy to happen positional shift when fixed, so that being more troublesome when installing fixed.2, existing fixed-wing
Aircraft wing frame eyelid retractor support side edge wing carry out high-speed flight when be not it is stable, cannot support and fix well,
To not very convenient when high-speed flight operation, so that not being very safe when driving and using.
Summary of the invention
The purpose of the present invention is to provide a kind of fixed wing aircraft shells that wing frame eyelid retractor is easy to assembly and stable, with solution
Existing fixed wing aircraft wing frame eyelid retractor certainly mentioned above in the background art carries out high-speed flight in support side edge wing
When be not that stable and existing fixed wing aircraft wing frame eyelid retractor is fixed on problem not very convenient when the wing of side.
To achieve the above object, the invention provides the following technical scheme:
A kind of fixed wing aircraft shell that wing frame eyelid retractor is easy to assembly and stable, including properller and aircraft machine
Body, the properller are fixed on the front end middle position of airframe, and the two sides of the properller are located at
Illumination protective cover is provided on airframe, the illumination protective cover and airframe are fixedly connected by welding, the aircraft
It is provided with aircraft takeoffs and landings front-wheel in front of the lower end of body, the airframe and aircraft takeoffs and landings front-wheel are connected by internal component activity
It connects, the rear two sides of the aircraft takeoffs and landings front-wheel, which are located on the outside of airframe, is provided with aircraft takeoffs and landings rear-wheel, the aircraft takeoffs and landings
Rear-wheel and airframe are flexibly connected by internal component, are provided with front end observation window, institute among the front end of the airframe
It states airframe and front end observation window is fixed by cross fixed screw, the right side of the front end observation window is located on airframe
It is provided with right side cabin door, the right side cabin door is connected with airframe by articulate, a left side for the front end observation window
Side, which is located on airframe, is provided with left sides window, and the left sides window and airframe are solid by cross fixed screw
It is fixed, aircraft flank is provided on the outside of the upper end of the airframe, the aircraft flank and airframe pass through the company of being welded and fixed
It connects, the lower end of the aircraft flank is provided with wing frame eyelid retractor, and the lower end of the wing frame eyelid retractor is connected on airframe, institute
It states and is provided with flank aileron on rear side of aircraft flank, the aircraft flank and flank aileron are flexibly connected by internal component, institute
The inside for stating flank aileron, which is located on aircraft flank, is provided with flank wing flap, and the aircraft flank and flank wing flap pass through internal structure
Part is flexibly connected, and the horizontal stable wing is provided on the outside of the rear end of the airframe, and the horizontal stable wing and airframe are logical
It crosses and connection is welded and fixed, the vertically stable wing, the vertically stable wing and aircraft machine are provided with above the rear end of the airframe
Body is fixedly connected by welding, and metal rudder, the vertically stable wing and metal are provided on rear side of the vertically stable wing
Rudder is flexibly connected by component.
Preferably, the properller includes block and the bar that is screwed under vane fixator, metal vane, fixator,
The outside of the vane fixator is provided with metal vane for one week, and the metal vane and vane fixator pass through the company of being welded and fixed
It connects, the lower end of the vane fixator is provided with block under fixator, and block is solid by welding under the vane fixator and fixator
Fixed to connect, the lower end of block is provided with the bar that is screwed under the fixator, and block and the bar that is screwed pass through weldering under the fixator
It connects and is fixedly connected, the bar that is screwed is connected on airframe.
Preferably, the metal rudder includes fixing component, rudder shell and internal reinforcing webs, outside the rudder
The leading inside of shell is provided with fixing component, and the rudder shell is internally provided with internal reinforcing webs, outside the rudder
Shell is connected on the vertically stable wing by fixing component.
Preferably, the aircraft takeoffs and landings front-wheel includes connection fixing block, metal connecting column, bottom shell and aero tyre,
The lower end of the connection fixing block is provided with metal connecting column, and the connection fixing block and metal connecting column pass through the company of being welded and fixed
It connects, the lower end of the metal connecting column is provided with bottom shell, and block is internally provided with aero tyre under the fixator, described
Connection fixing block is connected on airframe.
Preferably, the wing frame eyelid retractor include side arc block, intermediate convex block, top planes block, inclined-plane support column and
Bottom holders, the lower end of the inclined-plane support column are provided with bottom holders, and the inclined-plane support column and bottom holders are logical
It crosses and connection is welded and fixed, the upper end of the inclined-plane support column is provided with top planes block, the inclined-plane support column and top planes
Block is fixedly connected by welding, and intermediate convex block, the intermediate convex block and top are provided among the upper end of the top planes block
Flat blocks are fixedly connected by welding, and facility has side arc block, the side arc on the outside of the upper end of the inclined-plane support column
Block, intermediate convex block and top planes block are connected on aircraft flank, and the bottom holders are connected on airframe.
Preferably, the horizontal stable wing includes determine wing shell, blocking outer ring block and connecting elements, described to determine wing shell
Lower end, which is provided with, stops outer ring block, and the lower end for stopping outer ring block is provided with connecting elements, and the blocking outer ring block passes through company
Connection member is connected on airframe.
Preferably, there are two the horizontal stable wing be arranged altogether, and it is described it is horizontal stabilize the wing be fixedly connected in parallel it is winged
In the rear end sides of machine body, the horizontal stable wing and airframe rear end horizontal vertical.
Preferably, there are two the wing frame eyelid retractor is arranged altogether, and the wing frame eyelid retractor is symmetrically fixed on aircraft machine
On the two sides of body, the wing frame eyelid retractor, aircraft flank and airframe constitute triangular shaped.
Preferably, the vertically stable wing rear end outer shape size and metal rudder leading inside shape size phase
Deng, and the vertically stable wing is vertically fixed on airframe.
Preferably, there are two the flank aileron is arranged altogether, and the flank aileron is symmetrically fixed on airframe two
It holds on the inside of aircraft flank, the outside of the airframe and aircraft flank is on same straight line.
Compared with prior art, the present invention provides a kind of fixed wing aircraft shells that wing frame eyelid retractor is easy to assembly and stable
Body, have it is following the utility model has the advantages that
1, fixed wing aircraft of the present invention passes through side arc block, intermediate convex block, top planes block, inclined-plane support column and bottom
Wing frame eyelid retractor composed by fixator is more convenient when connection, and the bottom holders of wing frame eyelid retractor are connected to aircraft
It on body, and is fixed by screw, so that fixed installation is stronger, and when connection and aircraft flank are mutually fixed
It waits, by the intermediate convex block on top planes block, allows to good grafting and live, thus when fixed by screw more
Add convenience, so that installation personnel is more convenient when assembling.
2, fixed wing aircraft of the present invention passes through side arc block, intermediate convex block, top planes block, inclined-plane support column and bottom
Wing frame eyelid retractor composed by fixator has the support pulling force effect reinforced, and the bottom holders of wing frame eyelid retractor are connected to winged
On machine body, and top planes block is fixed on aircraft flank by intermediate convex block, so that inclined-plane support column has fine
Pulling force and supporting role, to stablize by the reinforcement of side arc block so that top junction forms stable triangle,
To more stable when high speed uses, convenient for high-speed flight.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention, in the accompanying drawings:
Fig. 1 is a kind of fixed wing aircraft shell structure that wing frame eyelid retractor is easy to assembly and stable signal proposed by the present invention
Figure；
Fig. 2 is properller structural schematic diagram proposed by the present invention；
Fig. 3 is metal rudder structural schematic diagram proposed by the present invention；
Fig. 4 is aircraft takeoffs and landings fore wheel structure schematic diagram proposed by the present invention；
Fig. 5 is wing frame eyelid retractor structural schematic diagram proposed by the present invention；
Fig. 6 is horizontal stable wing structure schematic diagram proposed by the present invention；
In figure: 1, aircraft flank；2, flank aileron；3, flank wing flap；4, front end observation window；5, right side cabin door；6, left
Side observation window；7, the horizontal stable wing；71, determine wing shell；72, stop outer ring block；73, connecting elements；8, vertically stabilize the wing；9, golden
Belong to rudder；91, fixing component；92, rudder shell；93, internal reinforcing webs；10, wing frame eyelid retractor；101, side arc
Block；102, intermediate convex block；103, top planes block；104, inclined-plane support column；105, bottom holders；11, properller；
111, vane fixator；112, metal vane；113, block under fixator；114, be screwed bar；12, protective cover is illuminated；13, fly
Machine rises and falls front-wheel；131, connection fixing block；132, metal connecting column；133, bottom shell；134, aero tyre；14, aircraft machine
Body；15, aircraft takeoffs and landings rear-wheel.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-6 is please referred to, the present invention provides a kind of technical solution:
A kind of fixed wing aircraft shell that wing frame eyelid retractor is easy to assembly and stable, including properller 11 and aircraft machine
Body 14, properller 11 are fixed on the front end middle position of airframe 14, and the two sides of properller 11 are located at
It is provided with illumination protective cover 12 on airframe 14, illuminates protective cover 12 and airframe 14 is fixedly connected by welding, aircraft
It is living by internal component that aircraft takeoffs and landings front-wheel 13, airframe 14 and aircraft takeoffs and landings front-wheel 13 are provided in front of the lower end of body 14
Dynamic connection, the rear two sides of aircraft takeoffs and landings front-wheel 13, which are located on the outside of airframe 14, is provided with aircraft takeoffs and landings rear-wheel 15, and aircraft rises
Fall behind wheel 15 and airframe 14 to be flexibly connected by internal component, is provided with front end observation window among the front end of airframe 14
4, airframe 14 and front end observation window 4 are fixed by cross fixed screw, and the right side of front end observation window 4 is located at airframe 14
On be provided with right side cabin door 5, right side cabin door 5 connected with airframe 14 by articulate, the left side of front end observation window 4
It is solid by cross fixed screw that left sides window 6, left sides window 6 and airframe 14 are provided on airframe 14
It is fixed, it is provided with aircraft flank 1 on the outside of the upper end of airframe 14, aircraft flank 1 and airframe 14 are fixedly connected by welding,
The lower end of aircraft flank 1 is provided with wing frame eyelid retractor 10, and the lower end of wing frame eyelid retractor 10 is connected on airframe 14, aircraft side
The rear side of the wing 1 is provided with flank aileron 2, aircraft flank 1 and flank aileron 2 and is flexibly connected by internal component, flank aileron 2
Inside, which is located on aircraft flank 1, is provided with flank wing flap 3, and aircraft flank 1 and flank wing flap 3 are flexibly connected by internal component,
The horizontal stable wing 7 is provided on the outside of the rear end of airframe 14, the stable wing 7 of level and airframe 14 pass through the company of being welded and fixed
It connects, the vertically stable wing 8 is provided with above the rear end of airframe 14, vertically the stable wing 8 and airframe 14 are by being welded and fixed
The rear side of connection, the vertical stable wing 8 is provided with metal rudder 9, and vertically the stable wing 8 and metal rudder 9 pass through component activity
Connection.
Further, properller 11 includes block 113 and screw thread under vane fixator 111, metal vane 112, fixator
The outside of fixed link 114, vane fixator 111 is provided with metal vane 112, metal vane 112 and vane fixator 111 for one week
It is fixedly connected by welding, the lower end of vane fixator 111 is provided with block 113 under fixator, vane fixator 111 and fixator
It is fixedly connected by welding for lower piece 113, the lower end of block 113 is provided with the bar 114 that is screwed under fixator, block 113 under fixator
Bar 114 is fixedly connected by welding with being screwed, and the bar 114 that is screwed is connected on airframe 14, properller 11
The bar 114 that is screwed be connected on airframe 14, in this way when 14 internal motivation device of airframe rotate when, will
So that the bar 114 that is screwed is rotated, so that the bar 114 that is screwed just will drive block 113 and vane fixator under fixator
111 are rotated, and such rotation of vane fixator 111 will make metal vane 112 be rotated, and can thus provide air-flow
Carry out using.
Further, metal rudder 9 includes fixing component 91, rudder shell 92 and internal reinforcing webs 93, outside rudder
The leading inside of shell 92 is provided with fixing component 91, and rudder shell 92 is internally provided with internal reinforcing webs 93, outside rudder
Shell 92 is connected on the vertically stable wing 8 by fixing component 91, and the rudder shell 92 of metal rudder 9 passes through fixing component 91
It is connected on the vertically stable wing 8, so as to carry out control use well, so that it is more convenient when in use, and side
Have the function of reinforcing intensity to the internal reinforcing webs 93 inside rudder shell 92.
Further, aircraft takeoffs and landings front-wheel 13 includes connection fixing block 131, metal connecting column 132, bottom shell 133 and flies
Wheel tire 134, the lower end of connection fixing block 131 are provided with metal connecting column 132, connection fixing block 131 and metal connecting column 132
It is fixedly connected by welding, the lower end of metal connecting column 132 is provided with bottom shell 133, the inside setting of block 113 under fixator
There is aero tyre 134, connection fixing block 131 is connected on airframe 14, and the connection fixing block 131 of aircraft takeoffs and landings front-wheel 13 connects
It connects on airframe 14, so that it is more convenient when in use, and metal connecting column 132 has support well
Effect, and when sliding, it is more convenient when sliding by the aero tyre 134 of 133 lower end of bottom shell, thus
It is more convenient when in use.
Further, wing frame eyelid retractor 10 includes side arc block 101, intermediate convex block 102, top planes block 103, inclined-plane branch
Dagger 104 and bottom holders 105, the lower end of inclined-plane support column 104 are provided with bottom holders 105,104 He of inclined-plane support column
Bottom holders 105 are fixedly connected by welding, and the upper end of inclined-plane support column 104 is provided with top planes block 103, inclined-plane support
Column 104 and top planes block 103 are fixedly connected by welding, and intermediate convex block is provided among the upper end of top planes block 103
102, intermediate convex block 102 and top planes block 103 are fixedly connected by welding, and there is facility on the outside of the upper end of inclined-plane support column 104
Side arc block 101, side arc block 101, intermediate convex block 102 and top planes block 103 are connected on aircraft flank 1, bottom
Fixator 105 is connected on airframe 14, and the bottom holders 105 of wing frame eyelid retractor 10 are connected on airframe 14, this
Sample is more convenient when in use, and when connection, by the intermediate convex block 102 on top planes block 103, so that can
It is lived with good grafting, thus it is more convenient when fixed, and side arc block 101 has support degree, thus in height
Speed is more stable when use, consequently facilitating high-speed flight.
Further, the horizontal stable wing 7 includes determining wing shell 71, stopping outer ring block 72 and connecting elements 73, determines wing shell 71
Lower end be provided with and stop outer ring block 72, stop the lower end of outer ring block 72 to be provided with connecting elements 73, outer ring block 72 stopped to pass through
Connecting elements 73 is connected on airframe 14, and the blocking outer ring block 72 of the stable wing 7 of level is connected to winged by connecting elements 73
It is more convenient when connection in this way on machine body 14, depending on wing shell 71 play balanced action, thus when in use
It is more stable.
Further, there are two the horizontal stable wing 7 is arranged altogether, and the horizontal stable wing 7 is fixedly connected on airframe in parallel
In 14 rear end sides, the stable wing 7 of level and 14 rear end horizontal vertical of airframe stabilize the wing 7 by two levels in this way
Effect, thus more stable when in use.
Further, there are two wing frame eyelid retractor 10 is arranged altogether, and wing frame eyelid retractor 10 is symmetrically fixed on airframe 14
Two sides on, wing frame eyelid retractor 10, aircraft flank 1 and airframe 14 constitute it is triangular shaped, so when in use more
Add stabilization, thus more convenient when in use.
Further, vertically stable 8 rear end outer shape size of the wing is equal with 9 leading inside shape size of metal rudder,
And vertically the stable wing 8 is vertically fixed on airframe 14, thus it is more convenient when in use, it is easy to use personnel to carry out
It uses.
Further, there are two flank aileron 2 is arranged altogether, and flank aileron 2 is symmetrically fixed on 14 both ends of airframe and flies
In 1 inside of the pusher side wing, the outside of airframe 14 and aircraft flank 1 is on same straight line, so when in use more
Stablize, personnel convenient to use operate.
The working principle of the invention and process for using: fixed wing aircraft of the present invention when in use, is needed fixed-wing
The airframe 14 of aircraft adds fuel oil, to use being moved to the enterprising enforcement of designated runway.Driver opens aircraft in this way
The right side cabin door 5 of body 14, to be sitting in the operational window of airframe 14, cabin door 5 on the right side of closure later, to beat
Fly an airplanepilot an airplane body 14 power device switch.In this way when the power device of airframe 14 is opened, aircraft will be made
The properller 11 of 14 front end of body is rotated, to form reversed effect dynamics, such airframe 14 is by flying
Machine rises and falls front-wheel 13 and aircraft takeoffs and landings rear-wheel 15 can be very good to be moved.And work as the properller of 14 front end of airframe
After 11 revolving speeds reach certain takeoff speed, by the operating stick in 14 operational window of airframe, so that fixed wing aircraft front end is lifted
It rises, and passes through aircraft flank 1, flank aileron 2, flank wing flap 3, the horizontal stable wing 7, the vertically stable wing on airframe 14
8 and metal rudder 9 effect so that properller 11, which forms air-flow and ground generation, acts on dynamics so that
Fixed wing aircraft takes off, to pack up front and back wheel.And when fixed wing aircraft flight in the sky, by airframe 14
Left sides window 6 and front end observation window 4, so as to observe outside well, consequently facilitating carrying out control use.And in height
When fast flight, fixed wing aircraft passes through the wing frame eyelid retractor 10 below aircraft flank 1, so that when flight more
Add stabilization, and wing frame eyelid retractor 10 is by side arc block 101, intermediate convex block 102, top planes block 103, inclined-plane support column
104 and bottom holders 105 formed.And the bottom holders 105 of wing frame eyelid retractor 10 are connected on airframe 14, in this way
It is more convenient when in use, and when connection, by the intermediate convex block 102 on top planes block 103, allow to
Good grafting is lived, thus it is more convenient when fixed, and side arc block 101 has support degree, so that upper rectangular
At stable triangular state, thus it is more stable when high speed uses, consequently facilitating high-speed flight.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (10)
1. a kind of fixed wing aircraft shell that wing frame eyelid retractor is easy to assembly and stable, including properller (11) and aircraft machine
Body (14), it is characterised in that: the properller (11) is fixed on the front end middle position of airframe (14), institute
The two sides for stating properller (11), which are located on airframe (14), is provided with illumination protective cover (12), the illumination protective cover
(12) it is fixedly connected by welding with airframe (14), before being provided with aircraft takeoffs and landings in front of the lower end of the airframe (14)
It takes turns (13), the airframe (14) and aircraft takeoffs and landings front-wheel (13) are flexibly connected by internal component, before the aircraft takeoffs and landings
The rear two sides of wheel (13), which are located on the outside of airframe (14), to be provided with aircraft takeoffs and landings rear-wheel (15), the aircraft takeoffs and landings rear-wheel
(15) it is flexibly connected with airframe (14) by internal component, front end sight is provided among the front end of the airframe (14)
It examines window (4), the airframe (14) and front end observation window (4) are fixed by cross fixed screw, the front end observation window (4)
Right side be located on airframe (14) and be provided with right side cabin door (5), the right side cabin door (5) and airframe (14) lead to
Articulate connection is crossed, the left side of the front end observation window (4), which is located on airframe (14), is provided with left sides window (6),
The left sides window (6) and airframe (14) are fixed by cross fixed screw, outside the upper end of the airframe (14)
Side is provided with aircraft flank (1), and the aircraft flank (1) and airframe (14) are fixedly connected by welding, the aircraft side
The lower end of the wing (1) is provided with wing frame eyelid retractor (10), and the lower end of the wing frame eyelid retractor (10) is connected on airframe (14),
It is provided with flank aileron (2) on rear side of the aircraft flank (1), the aircraft flank (1) and flank aileron (2) pass through internal structure
Part is flexibly connected, and the inside of the flank aileron (2), which is located on aircraft flank (1), is provided with flank wing flap (3), the aircraft side
The wing (1) and flank wing flap (3) are flexibly connected by internal component, are provided with horizontal peace on the outside of the rear end of the airframe (14)
Determine the wing (7), horizontal stable the wing (7) and airframe (14) are fixedly connected by welding, after the airframe (14)
End top is provided with vertically stable the wing (8), and vertically stable the wing (8) and airframe (14) are fixedly connected by welding, institute
It states and is provided with metal rudder (9) on rear side of vertically stable the wing (8), vertically stable the wing (8) and metal rudder (9) pass through
Component is flexibly connected.
2. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: the properller (11) includes block (113) and spiral shell under vane fixator (111), metal vane (112), fixator
The outside of line fixed link (114), the vane fixator (111) is provided with metal vane (112) for one week, the metal vane
(112) it is fixedly connected by welding with vane fixator (111), the lower end of the vane fixator (111) is provided with fixator
Lower piece (113), block (113) is fixedly connected by welding under the vane fixator (111) and fixator, block under the fixator
(113) lower end is provided with the bar that is screwed (114), and block (113) and the bar (114) that is screwed pass through welding under the fixator
It is fixedly connected, the bar that is screwed (114) is connected on airframe (14).
3. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: the metal rudder (9) includes fixing component (91), rudder shell (92) and internal reinforcing webs (93), the side
It is provided with fixing component (91) to the leading inside of rudder shell (92), the rudder shell (92) is internally provided with internal add
Strong net (93), the rudder shell (92) are connected on vertically stable the wing (8) by fixing component (91).
4. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: the aircraft takeoffs and landings front-wheel (13) include connection fixing block (131), metal connecting column (132), bottom shell (133) and
The lower end of aero tyre (134), the connection fixing block (131) is provided with metal connecting column (132), the connection fixing block
(131) it is fixedly connected by welding with metal connecting column (132), the lower end of the metal connecting column (132) is provided with outside bottom
Shell (133), block (113) is internally provided with aero tyre (134) under the fixator, connection fixing block (131) connection
On airframe (14).
5. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: the wing frame eyelid retractor (10) includes side arc block (101), intermediate convex block (102), top planes block (103), inclined-plane
The lower end of support column (104) and bottom holders (105), the inclined-plane support column (104) is provided with bottom holders (105),
The inclined-plane support column (104) and bottom holders (105) are fixedly connected by welding, the inclined-plane support column (104) it is upper
End is provided with top planes block (103), and the inclined-plane support column (104) and top planes block (103) are fixedly connected by welding,
It is provided with intermediate convex block (102) among the upper end of the top planes block (103), the intermediate convex block (102) and top planes
Block (103) is fixedly connected by welding, and facility has side arc block (101), institute on the outside of the upper end of the inclined-plane support column (104)
It states side arc block (101), intermediate convex block (102) and top planes block (103) to be connected on aircraft flank (1), the bottom
Fixator (105) is connected on airframe (14).
6. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: described horizontal stable the wing (7) include determining wing shell (71), stopping outer ring block (72) and connecting elements (73), described to determine the wing
The lower end of shell (71), which is provided with, stops outer ring block (72), and the lower end for stopping outer ring block (72) is provided with connecting elements
(73), the blocking outer ring block (72) is connected on airframe (14) by connecting elements (73).
7. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: there are two horizontal stable the wing (7) are arranged altogether, and horizontal stable the wing (7) are fixedly connected on aircraft machine in parallel
In the rear end sides of body (14), horizontal stable the wing (7) and airframe (14) rear end horizontal vertical.
8. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: there are two the wing frame eyelid retractor (10) is arranged altogether, and the wing frame eyelid retractor (10) is symmetrically fixed on airframe
(14) on two sides, the wing frame eyelid retractor (10), aircraft flank (1) and airframe (14) constitute triangular shaped.
9. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: the vertically stable wing (8) rear end outer shape size is equal with metal rudder (9) leading inside shape size, and
Vertically stable the wing (8) are vertically fixed on airframe (14).
10. a kind of wing frame eyelid retractor according to claim 1 fixed wing aircraft shell easy to assembly and stable, feature
Be: there are two the flank aileron (2) is arranged altogether, and the flank aileron (2) is symmetrically fixed on airframe (14) two
It holds on the inside of aircraft flank (1), the outside of the airframe (14) and aircraft flank (1) is on same straight line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811652366.1A CN109649633B (en) | 2018-12-31 | 2018-12-31 | Fixed wing aircraft casing of easy to assemble and stable of wing frame support ware |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811652366.1A CN109649633B (en) | 2018-12-31 | 2018-12-31 | Fixed wing aircraft casing of easy to assemble and stable of wing frame support ware |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109649633A true CN109649633A (en) | 2019-04-19 |
| CN109649633B CN109649633B (en) | 2023-10-03 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811652366.1A Active CN109649633B (en) | 2018-12-31 | 2018-12-31 | Fixed wing aircraft casing of easy to assemble and stable of wing frame support ware |
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| CN (1) | CN109649633B (en) |
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| US4121791A (en) * | 1977-07-27 | 1978-10-24 | Taylor Bruce G | Aircraft built up from individual readily assembled and disassembled segments or components |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN109649633B (en) | 2023-10-03 |
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