CN208412092U - A kind of more power fixed wing aircrafts - Google Patents
A kind of more power fixed wing aircrafts Download PDFInfo
- Publication number
- CN208412092U CN208412092U CN201821069979.8U CN201821069979U CN208412092U CN 208412092 U CN208412092 U CN 208412092U CN 201821069979 U CN201821069979 U CN 201821069979U CN 208412092 U CN208412092 U CN 208412092U
- Authority
- CN
- China
- Prior art keywords
- fixed
- vertical pusher
- aileron
- mounting hole
- aircraft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of more power fixed wing aircrafts, fuselage two sides are symmetrically arranged with fixed aileron, and in fixed aileron up to being set less there are two vertical pusher mounting hole, vertical pusher, which is arranged in vertical pusher mounting hole, pushes aircraft vertical lifting；On the outside of fixed aileron, horizontal propeller setting pushes aircraft cruising flight in afterbody for the fixed main wing setting；Door apparatus is equipped in the position of upper of vertical pusher mounting hole or/and the position Xia Kou.Vertical pusher, which is mounted in fixed aileron, can lead to the problem of one, it is exactly that vertical pusher installation position vertical pusher mounting hole is unable to convection current above and below air in aircraft cruise, otherwise it will affect the balance of aircraft, in order to solve this problem, the utility model is equipped with door apparatus in the position of upper of vertical pusher mounting hole or/and the position Xia Kou, vertical pusher mounting hole can be closed when aircraft cruises by door apparatus, vertical pusher is hidden in fixed aileron.
Description
Technical field
The utility model relates to airplane equipment technical fields, and in particular to a kind of more power fixed wing aircrafts.
Background technique
More rotors (vertical pusher) vertical take-off and landing drone or helicopter almost all common at present concentrates on consuming
Field, more rotor vertical take-off and landing drone professions are sorted out and are known as consumer level unmanned plane.Its payload only has several hectograms to several
Kilogram, it is limited by industrial chain and self-technique condition, domestic plurality of unmanned plane R & D Enterprises are not yet developed greatly so far
The multi-rotor unmanned aerial vehicle of load, their product more be used to take photo by plane, entertain or complete minimal amount of technical grade flight and appoint
Business.
Traditional fixed wing aircraft advantage is that flying speed is fast, and voyage and cruise time are long, the disadvantage is that landing distance,
Seek the runway of high quality.The advantages of multi-rotor unmanned aerial vehicle is lesser landing site, energy VTOL, hovering, the disadvantage is that
Power consumption is big, speed is slow, cruise duration is short.
The unmanned plane that more rotors (vertical pusher) are arranged on fixed wing aircraft (with horizontal propeller) at present has been opened
Hair application, with the continuous innovation of technology, in order to adapt to the needs of various industries, there is the load-carrying and flying speed of aircraft
The requirement of update, as shown in Figure 1, this more power fixed-wings that multiple vertical pushers are arranged in fixed wing aircraft two sides fly
Machine, since vertical pusher is by connecting rod or directly plug-in setting at fuselage position, thus when loading capacity is larger, it is this
Setting structure is just unbearable, and will lead to connecting portion fracture leads to the generation of safety accident, in addition, this external hanging type is vertical
Propeller setting structure can generate larger resistance in aircraft high speed cruise flight, to influence the flight efficiency of aircraft.Also
It is exactly that the vertical pusher setting structure of this external hanging type is needed more multi-thread due to the promotion of the structural behaviour of vertical pusher
Road also will affect the reasonable setting of vertical pusher in conjunction with fuselage.
Utility model content
The purpose of this utility model is to overcome the shortage of prior art, and provides a kind of more power fixed wing aircrafts, solves
The unreasonable set-up mode of existing more power fixed wing aircraft external hanging type vertical pushers, when loading capacity is larger, this set
Structure is just unbearable, and will lead to connecting portion fracture leads to the generation of safety accident, in addition, the vertical thrust of this external hanging type
Device setting structure can generate larger resistance in aircraft high speed cruise flight, to influence the flight efficiency of aircraft.There are also be exactly
The vertical pusher setting structure of this external hanging type, due to the promotion of the structural behaviour of vertical pusher, need more multi-line with
Fuselage combines, and also will affect the rational setting problem of vertical pusher.
The utility model is achieved through the following technical solutions:
A kind of more power fixed wing aircrafts, including fuselage, fixed main wing, horizontal propeller and vertical pusher, the machine
Body two sides are symmetrically arranged with fixed aileron, and in fixed aileron, up to setting less, there are two vertical pusher mounting hole, the vertical thrusts
Device, which is arranged in vertical pusher mounting hole, pushes aircraft vertical lifting；The fixed main wing setting is on the outside of fixed aileron, institute
It states horizontal propeller setting and pushes aircraft cruising flight in afterbody；Vertical pusher mounting hole position of upper or/and
The position Xia Kou is equipped with door apparatus.
A kind of more power fixed wing aircrafts of the utility model, by the way that fixed aileron is arranged, fixed aileron is set using streamlined
Meter, fixed aileron are the extensions of fuselage two sides, and fixed main wing setting is on the outside of fixed aileron, and by the way that fixed aileron is arranged, one can
To effectively reduce the length of fixed main wing, in the case where guaranteeing the same aircraft degree of balance, to reduce the space of integrated airplane
Size, two can be used to install vertical pusher, because the width of fixed joint chord is basic and fuselage is suitable, connecting portion
Area is big, is connected firmly, and vertical pusher is mounted in fixed aileron, can effectively improve the installation strength of vertical pusher,
So as to promote bigger loading capacity, in addition, vertical pusher is to be hidden in installation in fixed aileron, thus vertical pusher
Resistance will not be generated when aircraft cruises；
Vertical pusher, which is mounted in fixed aileron, can lead to the problem of one, be exactly that vertical pusher installation position vertically pushes away
It is unable to convection current above and below air when aircraft cruises into device mounting hole, otherwise will affect the balance of aircraft, in order to solve this problem, this
Utility model is equipped with door apparatus in the position of upper of vertical pusher mounting hole or/and the position Xia Kou, is filled by shield door
Vertical pusher mounting hole can be closed when aircraft cruises by setting, and vertical pusher is hidden in fixed aileron.
Further, the door apparatus includes the two semi-circular shield doors of fan, and every semi-circular shield door of fan, which is connected with, to be turned
Dynamic connecting rod, pivot link are set in shaft by rotational sleeve, the rotational sleeve equipped with fan type tooth, two fan type teeth it
Between be equipped with movable block, movable block two sides be equipped with intermeshing tooth of fan type tooth, the movable block outer end is connected with electricity
Dynamic push rod pushes movable block when the elongation of the screw rod of electric pushrod, and the movable block drives pivot link rotation by fan type tooth,
Pivot link rotates around the shaft opens the semi-circular shield door of two fans, otherwise makes the semi-circular shield door closure of two fans.
Further, when door apparatus is opened, the two semi-circular shield doors of fan are stored up in fixed aileron.
Further, two vertical pusher mounting holes, each vertical pusher mounting hole are equipped in every fixed aileron
It is interior to be equipped with a set of vertical pusher.
Further, the door apparatus includes a round flexible shield door of fan, is connected on every round flexible shield door of fan
It is connected to telescopic screw rod, the telescopic screw rod that the correspondence two on a fixed aileron fans round flexible shield door connects by adjusting sleeve
It connects, sleeve umbrella tooth is equipped in the middle part of the adjusting sleeve, corresponding sleeve umbrella tooth passes through rotation axis and rotation on the fixed aileron of two pieces
The rotation axis end umbrella tooth of axis both ends setting connects transmission, and rotation axis umbrella tooth, the rotation axis umbrella tooth are equipped in the middle part of rotation axis
It is meshed and is equipped with motor umbrella tooth, the motor umbrella tooth is mounted on the machine shaft of motor, is fanned and is justified by motor synchronous drive four
The flexible shield door of type turns off or on.
Further, the round flexible shield door when opening, store up in fixed aileron by round flexible shield door.
Further, the fixed aileron uses airflow design.
Further, the fuselage bottom is equipped with support frame.
The utility model compared with prior art, has the following advantages and benefits:
1, a kind of more power fixed wing aircrafts of the utility model, by the way that fixed aileron is arranged, fixed aileron is using streamlined
The extension that aileron is fuselage two sides is fixed in design, and fixed main wing setting fixes aileron on the outside of fixed aileron, by being arranged, and one
The length that fixed main wing can be effectively reduced, in the case where guaranteeing the same aircraft degree of balance, to reduce the sky of integrated airplane
Between size, two can be used to install vertical pusher, because the width of fixed joint chord is basic and fuselage is suitable, interconnecting piece
Plane product is big, is connected firmly, vertical pusher is mounted in fixed aileron, and the installation that can effectively improve vertical pusher is strong
Degree, so as to promote bigger loading capacity, in addition, vertical pusher is to be hidden in installation in fixed aileron, to vertically push away
Into device resistance will not be generated when aircraft cruises；
2, a kind of more power fixed wing aircrafts of the utility model, vertical pusher, which is mounted in fixed aileron, can generate one
Problem is exactly that vertical pusher installation position vertical pusher mounting hole is unable to convection current above and below air in aircraft cruise, otherwise
Will affect the balance of aircraft, in order to solve this problem, the utility model vertical pusher mounting hole position of upper or/and under
Mouth position is equipped with door apparatus, can be closed vertical pusher mounting hole when aircraft cruises by door apparatus, will
Vertical pusher is hidden in fixed aileron.
3, a kind of more power fixed wing aircrafts of the utility model pass through the setting vertical pusher installation on fixed aileron
Hole, and the position of upper of vertical pusher mounting hole or/and the position Xia Kou are equipped with door apparatus and pass through in aircraft landing
The resistance that vertical pusher mounting hole is opened when can effectively reduce aircraft landing, this, can be quick when emergency occurs
Complete aircraft landing；
4, a kind of more power fixed wing aircrafts of the utility model, the utility model devise two kinds of door apparatus structure shapes
Formula, embodiment 1 individually can control closure or openness to each vertical pusher mounting hole respectively, it is possible to implement targetedly
Operation, embodiment 2, so door apparatus synchronously control, convenient for operation.The utility model can be by door apparatus
Unlatching control, to control the balance of fuselage, thus for aircraft safety fly one of guarantee is provided.Solve existing more power
The unreasonable set-up mode of fixed wing aircraft external hanging type vertical pusher, when loading capacity is larger, this set structure just can not
It bears, will lead to connecting portion fracture leads to the generation of safety accident, in addition, knot is arranged in the vertical pusher of this external hanging type
Structure can generate larger resistance in aircraft high speed cruise flight, to influence the flight efficiency of aircraft.There are also be exactly this plug-in
The vertical pusher setting structure of formula needs more multi-line in conjunction with fuselage due to the promotion of the structural behaviour of vertical pusher,
Also it will affect the rational setting problem of vertical pusher.
Detailed description of the invention
Attached drawing described herein is used to provide to further understand the utility model embodiment, constitutes the one of the application
Part does not constitute the restriction to the utility model embodiment.In the accompanying drawings:
Fig. 1 is the structural schematic diagram of existing more power fixed wing aircrafts；
Fig. 2 is a kind of schematic perspective view of more power fixed wing aircrafts of the utility model；
Fig. 3 is a kind of schematic view of the front view of more power fixed wing aircrafts of the utility model；
Fig. 4 is a kind of side structure schematic view of more power fixed wing aircrafts of the utility model；
Fig. 5 is a kind of overlooking structure diagram of more power fixed wing aircrafts of the utility model；
Fig. 6 is a kind of door apparatus closed state structural schematic diagram of more power fixed wing aircrafts of the utility model；
Fig. 7 is that the utility model implements 1 door apparatus closed state structural schematic diagram；
Fig. 8 is that the utility model implements 1 door apparatus open state structural schematic diagram；
Fig. 9 is that the utility model implements 2 door apparatus closed state structural schematic diagrams；
Figure 10 is that the utility model implements 3 door apparatus open state structural schematic diagrams；
Label and corresponding parts title in attached drawing:
1- fuselage, the fixed main wing of 2-, 3- horizontal propeller, 4- vertical pusher, the fixed aileron of 5-, 6- vertical pusher peace
Fill hole, the semi-circular shield door of 7-, 8- pivot link, 9- rotational sleeve, 10- shaft, 11- fan type tooth, 12- movable block, 13- item
Tooth, 14- electric pushrod, 15- screw rod, the round flexible shield door of 16-, 17- telescopic screw rod, 18- adjusting sleeve, 19- sleeve umbrella tooth,
20- rotation axis, 21- rotation axis end umbrella tooth, 22- rotation axis umbrella tooth, 23- motor umbrella tooth, 24- motor, 25- machine shaft, 26-
Support frame.
Specific embodiment
For the purpose of this utility model, technical solution and advantage is more clearly understood, below with reference to embodiment and attached drawing,
The utility model is described in further detail, and the exemplary embodiment and its explanation of the utility model are only used for explaining this
Utility model is not intended to limit the scope of the present invention.
Embodiment 1
As illustrated in figs. 2 through 8, a kind of more power fixed wing aircrafts of the utility model, including fuselage 1, fixed main wing 2, level push away
Into device 3 and vertical pusher 4, horizontal propeller 3 can use existing propeller structure, and such as turbojet can also
To use turbo oar engine, turbo oar engine is constituted using aviation kerosine engine and propeller type propeller, vertical pusher 4
Rotor mechanism can be used, such as ducted fan, fuselage 1 is identical with existing unmanned plane or helicopter structure, 1 two sides of fuselage
It is symmetrically arranged with fixed aileron 5, at least provided with two vertical pusher mounting holes 6, the vertical pusher 4 on fixed aileron 5
It is arranged in vertical pusher mounting hole 6 and pushes aircraft vertical lifting；The setting of fixed main wing 2 is in fixed 5 outside of aileron, institute
It states the setting of horizontal propeller 3 and pushes aircraft cruising flight in 1 tail portion of fuselage；Vertical pusher mounting hole 6 position of upper or/
Door apparatus is equipped with the position Xia Kou.Door apparatus can be set in position of upper, screen can also be equipped in the position Xia Kou
Door gear is covered, or is equipped with door apparatus in position of upper and the position Xia Kou simultaneously.
Door apparatus includes the two semi-circular shield doors 7 of fan, and every semi-circular shield door 7 of fan is connected with pivot link 8, rotates
Connecting rod 8 is set in shaft 10 by rotational sleeve 9, and the rotational sleeve 9 is equipped with fan type tooth 11, between two fan type teeth 11
Equipped with movable block 12, it is equipped with and 11 intermeshing teeth of fan type tooth 13,12 outer end of movable block in 12 two sides of movable block
It is connected with electric pushrod 14, movable block 12 is pushed when the screw rod 15 of electric pushrod 14 extends, the movable block 12 passes through fan type
Tooth 11 drives pivot link 8 to rotate, and 10 rotations open the semi-circular shield door 7 of two fans to pivot link 8 around the shaft, otherwise make two fans
Semi-circular shield door 7 is closed.When door apparatus is opened, the two semi-circular shield doors 7 of fan are stored up in fixed aileron 5.It is electronic
Push rod 14 can also be changed to cylinder or hydraulic cylinder according to actual needs.
A kind of more power fixed wing aircrafts of the utility model, by the way that fixed aileron is arranged, fixed aileron is set using streamlined
Meter, fixed aileron are the extensions of fuselage two sides, and fixed main wing setting is on the outside of fixed aileron, and by the way that fixed aileron is arranged, one can
To effectively reduce the length of fixed main wing, in the case where guaranteeing the same aircraft degree of balance, to reduce the space of integrated airplane
Size, two can be used to install vertical pusher, because the width of fixed joint chord is basic and fuselage is suitable, connecting portion
Area is big, is connected firmly, and vertical pusher is mounted in fixed aileron, can effectively improve the installation strength of vertical pusher,
So as to promote bigger loading capacity, in addition, vertical pusher is to be hidden in installation in fixed aileron, thus vertical pusher
Resistance will not be generated when aircraft cruises；
Vertical pusher, which is mounted in fixed aileron, can lead to the problem of one, be exactly that vertical pusher installation position vertically pushes away
It is unable to convection current above and below air when aircraft cruises into device mounting hole, otherwise will affect the balance of aircraft, in order to solve this problem, this
Utility model is equipped with door apparatus in the position of upper of vertical pusher mounting hole or/and the position Xia Kou, is filled by shield door
Vertical pusher mounting hole can be closed when aircraft cruises by setting, and vertical pusher is hidden in fixed aileron.
By being arranged vertical pusher mounting hole on fixed aileron, and the position of upper of vertical pusher mounting hole or/
It is equipped with door apparatus with the position Xia Kou, in aircraft landing, can be effectively reduced by unlatching vertical pusher mounting hole winged
Resistance when machine lands, aircraft landing can be rapidly completed when emergency occurs in this；
Embodiment 1 individually can control closure or openness to each vertical pusher mounting hole respectively, it is possible to implement have needle
Operation to property.
Embodiment 2
As shown in Fig. 2-6,9 and 10, a kind of more power fixed wing aircrafts of the utility model on the basis of embodiment 1 will
Door apparatus replaces with the mechanism form of the present embodiment, sets in every fixed aileron 5 there are two vertical pusher mounting hole 6,
A set of vertical pusher 4 is equipped in each vertical pusher mounting hole 6.
The door apparatus includes a round flexible shield door 16 of fan, is connected with and stretches on every round flexible shield door 16 of fan
Contracting screw rod 17, the correspondence two on a fixed aileron 5 fan the telescopic screw rod 17 of round flexible shield door 16 by adjusting sleeve 18
Connection adjusts the both ends screw thread of sleeve 18 on the contrary, the telescopic screw rod 17 that both ends can be made to connect is synchronous to be shortened or stretch when rotating
It is long, sleeve umbrella tooth 19 is equipped in the middle part of the adjusting sleeve 18, corresponding sleeve umbrella tooth 19 passes through rotation axis on the fixed aileron 5 of two pieces
20 and 20 both ends of rotation axis setting rotation axis end umbrella tooth 21 connect transmission, in the middle part of rotation axis 20 be equipped with rotation axis umbrella tooth
22, the rotation axis umbrella tooth 22 is meshed equipped with motor umbrella tooth 23, and the motor umbrella tooth 23 is mounted on the machine shaft of motor 24
On 25, round flexible shield door 16 is fanned by 24 synchronous drive four of motor and is turned off or on.
Motor 24 starts, and motor 24 passes sequentially through machine shaft 25, motor umbrella tooth 23, rotation axis umbrella tooth 22 and drives rotation axis
20 rotations, rotation axis 20 report the adjusting sleeve 18 for driving both ends connection to rotate, when adjusting the rotation of sleeve 18, can make both ends same
The telescopic screw rod 17 of connection is synchronous to be shortened or extends.
The round flexible shield door 16 when opening, store up in fixed aileron 5 by round flexible shield door 16.It is described solid
5 wings of fixed pair use airflow design.Airflow design is 20 th century America 30 or 40 years for a kind of most popular design style, with
The fairing of round and smooth smoothness is principal mode, is initially mainly used in automobile, on the train vehicles, was widely current later, several
Feed through to all product shapes.Development in science and technology and consumerism facilitate the generation and prevalence of streamlined style.Science and technology hair
Exhibition often to modern designs provide with inspiration, streamlined is originally a term in aerodynamics, for describe surface it is round and smooth,
The object form that the lines flow smoothly.This threadiness is applied to friendship because windage of the object in high-speed motion can be reduced
In the design of logical tool.1 bottom of fuselage is equipped with support frame 26.Support frame 26 can support aircraft in aircraft landing.
A kind of more power fixed wing aircrafts of the utility model, by the way that fixed aileron is arranged, fixed aileron is set using streamlined
Meter, fixed aileron are the extensions of fuselage two sides, and fixed main wing setting is on the outside of fixed aileron, and by the way that fixed aileron is arranged, one can
To effectively reduce the length of fixed main wing, in the case where guaranteeing the same aircraft degree of balance, to reduce the space of integrated airplane
Size, two can be used to install vertical pusher, because the width of fixed joint chord is basic and fuselage is suitable, connecting portion
Area is big, is connected firmly, and vertical pusher is mounted in fixed aileron, can effectively improve the installation strength of vertical pusher,
So as to promote bigger loading capacity, in addition, vertical pusher is to be hidden in installation in fixed aileron, thus vertical pusher
Resistance will not be generated when aircraft cruises；
Vertical pusher, which is mounted in fixed aileron, can lead to the problem of one, be exactly that vertical pusher installation position vertically pushes away
It is unable to convection current above and below air when aircraft cruises into device mounting hole, otherwise will affect the balance of aircraft, in order to solve this problem, this
Utility model is equipped with door apparatus in the position of upper of vertical pusher mounting hole or/and the position Xia Kou, is filled by shield door
Vertical pusher mounting hole can be closed when aircraft cruises by setting, and vertical pusher is hidden in fixed aileron.
By being arranged vertical pusher mounting hole on fixed aileron, and the position of upper of vertical pusher mounting hole or/
It is equipped with door apparatus with the position Xia Kou, in aircraft landing, can be effectively reduced by unlatching vertical pusher mounting hole winged
Resistance when machine lands, aircraft landing can be rapidly completed when emergency occurs in this.
Embodiment 2, thus door apparatus synchronously control, convenient for operation.The utility model can be by shield door
The unlatching of device controls, to control the balance of fuselage, to provide one of guarantee for aircraft safety flight.Awing by two
A semi-circular flexible shielding door closure, which lives propeller or Ducted propeller, makes wing keep complete smooth appearance, does not produce awing
Raw nest gas rotation, aircraft vertical landing lift are provided by the multiple Ducted propellers being arranged in wing, aircraft is flat fly during,
Ducted propeller duct mouth in wing will be closed by closing means, and aircraft is made to keep good aerodynamic configuration.
Aircraft is gone up and down by multiple propellers or Ducted propeller in fixed aileron 5, awing by round flexible shield door
Covering propeller or Ducted propeller makes wing keep complete smooth appearance, does not generate the rotation of nest gas awing, aircraft hangs down
Straight landing lift is provided by the multiple Ducted propellers being arranged in wing, aircraft is flat fly during, the duct in wing promotes
Device duct mouth will be closed by closing means, and aircraft is made to keep good aerodynamic configuration.
Above-described specific embodiment, to the purpose of this utility model, technical scheme and beneficial effects carried out into
One step is described in detail, it should be understood that being not used to limit the foregoing is merely specific embodiment of the present utility model
Determine the protection scope of the utility model, within the spirit and principle of the utility model, any modification for being made equally is replaced
It changes, improve, should be included within the scope of protection of this utility model.
Claims (8)
1. a kind of more power fixed wing aircrafts, including fuselage (1), fixed main wing (2), horizontal propeller (3) and vertical pusher
(4), it is characterised in that: fuselage (1) two sides are symmetrically arranged with fixed aileron (5), at least provided with two on fixed aileron (5)
Vertical pusher mounting hole (6), vertical pusher (4) setting push aircraft vertical in vertical pusher mounting hole (6)
Lifting；On the outside of fixed aileron (5), the horizontal propeller (3) is arranged in fuselage (1) tail portion for fixed main wing (2) setting
Push aircraft cruising flight；Door apparatus is equipped in the position of upper of vertical pusher mounting hole (6) or/and the position Xia Kou.
2. a kind of more power fixed wing aircrafts according to claim 1, it is characterised in that: the door apparatus includes two
It fans semi-circular shield door (7), every semi-circular shield door (7) of fan is connected with pivot link (8), and pivot link (8) passes through turning set
Cylinder (9) is set on shaft (10), and the rotational sleeve (9) is equipped with fan type tooth (11), is equipped between two fan type teeth (11)
Movable block (12) is equipped with and intermeshing tooth (13) of fan type tooth (11), the movable block in movable block (12) two sides
(12) outer end is connected with electric pushrod (14), pushes movable block (12) when the elongation of the screw rod (15) of electric pushrod (14), described
Movable block (12) drives pivot link (8) rotation by fan type tooth (11), and (10) rotation makes two fans half to pivot link (8) around the shaft
Round shield door (7) is opened, otherwise is closed the semi-circular shield door of two fans (7).
3. a kind of more power fixed wing aircrafts according to claim 2, it is characterised in that: when door apparatus is opened,
The two semi-circular shield doors (7) of fan are stored up in fixed aileron (5).
4. a kind of more power fixed wing aircrafts according to claim 1, it is characterised in that: set in every fixed aileron (5)
There are two vertical pusher mounting hole (6), a set of vertical pusher (4) are equipped in each vertical pusher mounting hole (6).
5. a kind of more power fixed wing aircrafts according to claim 4, it is characterised in that: the door apparatus includes one
Round flexible shield door (16) is fanned, is connected with telescopic screw rod (17) on every round flexible shield door (16) of fan, a fixed aileron
(5) correspondence two on fans the telescopic screw rod (17) of round flexible shield door (16) by adjusting sleeve (18) connection, the adjusting
Sleeve umbrella tooth (19) are equipped in the middle part of sleeve (18), corresponding sleeve umbrella tooth (19) passes through rotation axis in two pieces fixed aileron (5)
(20) and the rotation axis end umbrella tooth (21) of rotation axis (20) both ends setting connects transmission, and rotation is equipped in the middle part of rotation axis (20)
Axis umbrella tooth (22), the rotation axis umbrella tooth (22) are meshed equipped with motor umbrella tooth (23), and the motor umbrella tooth (23) is mounted on electricity
On the machine shaft (25) of machine (24), round flexible shield door (16) is fanned by motor (24) synchronous drive four and is turned off or on.
6. a kind of more power fixed wing aircrafts according to claim 5, it is characterised in that: the round flexible shield door
(16) when opening, round flexible shield door (16) is stored up in fixed aileron (5).
7. a kind of more power fixed wing aircrafts according to claim 1, it is characterised in that: the fixed aileron (5) uses
Airflow design.
8. a kind of more power fixed wing aircrafts according to claim 1, it is characterised in that: fuselage (1) bottom is equipped with
Support frame (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821069979.8U CN208412092U (en) | 2018-07-06 | 2018-07-06 | A kind of more power fixed wing aircrafts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821069979.8U CN208412092U (en) | 2018-07-06 | 2018-07-06 | A kind of more power fixed wing aircrafts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208412092U true CN208412092U (en) | 2019-01-22 |
Family
ID=65125750
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821069979.8U Expired - Fee Related CN208412092U (en) | 2018-07-06 | 2018-07-06 | A kind of more power fixed wing aircrafts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208412092U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639333A (en) * | 2018-07-06 | 2018-10-12 | 成都军融项目管理有限公司 | A kind of more power fixed wing aircrafts with vertical lift function |
| CN111017205A (en) * | 2019-12-24 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Vertical take-off and landing conveyor |
| CN114235025A (en) * | 2021-11-23 | 2022-03-25 | 佛山市川东磁电股份有限公司 | Building health state monitoring system |
-
2018
- 2018-07-06 CN CN201821069979.8U patent/CN208412092U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108639333A (en) * | 2018-07-06 | 2018-10-12 | 成都军融项目管理有限公司 | A kind of more power fixed wing aircrafts with vertical lift function |
| CN111017205A (en) * | 2019-12-24 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Vertical take-off and landing conveyor |
| CN114235025A (en) * | 2021-11-23 | 2022-03-25 | 佛山市川东磁电股份有限公司 | Building health state monitoring system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106428547B (en) | Vertical take-off and landing fixed-wing aircraft with multiple rotors capable of being automatically retracted and extended | |
| CN208412092U (en) | A kind of more power fixed wing aircrafts | |
| CN1978277A (en) | Combined rotor aircraft | |
| CN109760832A (en) | A kind of VTOL fixed-wing unmanned vehicle | |
| CN108639333B (en) | Multi-power fixed wing aircraft with vertical lifting function | |
| CN209176908U (en) | A kind of rotor fixed-wing unmanned plane of composite drive | |
| CN114560084A (en) | Self-unfolding deformation wing of bionic flapping wing flying robot | |
| CN200970477Y (en) | Artificial plane model | |
| CN104443353A (en) | Wing-changeable airplane | |
| CN203845012U (en) | Rotary flapping wing type driving airplane | |
| CN109911185A (en) | A kind of high speed single rotor helicopter without tail surface | |
| CN108382578A (en) | A kind of mixed at high speed layout vertically taking off and landing flyer | |
| CN211281472U (en) | Duct tail sitting posture VTOL unmanned aerial vehicle | |
| CN117566089A (en) | Fixed wing aircraft capable of changing sweepback wing to vertically take off and land | |
| CN110641694A (en) | Automatic VTOL fixed wing unmanned aerial vehicle of folding rotor | |
| CN207346096U (en) | Vertical take-off and landing fixed wing aircraft with rear-mounted propeller | |
| CN213649894U (en) | Thrust vector tail sitting type vertical take-off and landing unmanned aerial vehicle | |
| CN111137446B (en) | Pneumatic layout of multi-rotor vertical take-off and landing unmanned aerial vehicle with stalling function | |
| CN211076356U (en) | Commuting type electric airplane system | |
| CN208134610U (en) | A kind of mixed at high speed layout vertically taking off and landing flyer | |
| CN208134600U (en) | A kind of aircraft with stretching, extension function | |
| CN208760900U (en) | A kind of annular wing unmanned vehicle | |
| CN209336997U (en) | Unmanned plane | |
| CN113002770A (en) | Rotor craft capable of attaching wings to fuselage | |
| CN103991542A (en) | Rotary flapping wing driving airplane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190122 Termination date: 20200706 |