CN208683094U - A kind of novel rudder face connection structure - Google Patents

A kind of novel rudder face connection structure Download PDF

Info

Publication number
CN208683094U
CN208683094U CN201820582662.8U CN201820582662U CN208683094U CN 208683094 U CN208683094 U CN 208683094U CN 201820582662 U CN201820582662 U CN 201820582662U CN 208683094 U CN208683094 U CN 208683094U
Authority
CN
China
Prior art keywords
rudder face
fin
blade unit
unit
end rib
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.)
Active
Application number
CN201820582662.8U
Other languages
Chinese (zh)
Inventor
苏扬
刘德山
赵安民
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wing Wing Flying (tianjin) Technology Co Ltd
Original Assignee
Wing Wing Flying (tianjin) Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Wing Wing Flying (tianjin) Technology Co Ltd filed Critical Wing Wing Flying (tianjin) Technology Co Ltd
Priority to CN201820582662.8U priority Critical patent/CN208683094U/en
Application granted granted Critical
Publication of CN208683094U publication Critical patent/CN208683094U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

The utility model proposes a kind of novel rudder face connection structures, comprising: wingtip fin unit, rudder face end rib blade unit, rotary shaft, stringer and wing;Described rudder face end rib blade unit one end is connect with stringer, and the other end is connect with wingtip fin unit;The rotary shaft passes through rudder face end rib blade unit, and both ends are fixedly connected with wing;The wingtip fin unit is made of N1 layers of fin, N1 >=3;The rudder face end rib blade unit is made of N2 layers of fin, N2 >=3.The utility model proposes a kind of novel rudder face connection structure, to relatively simple articulated connection is optimized on the market at present, the face contact stress of the point contact stress of script or small area is changed to the face contact stress of larger area, improve stress condition, endurance is improved, the probability of damage is reduced.

Description

A kind of novel rudder face connection structure
Technical field
The utility model belongs to aeronautical product technical field, especially a kind of novel rudder face connection structure.
Background technique
At this stage, the rudder face connection type on fixed-wing unmanned plane is mostly simple hinge connection, and such connection type is held Power ability is poor, and larger stress is generated easily at hinge shaft, and then destroys hinge connection, if during unmanned plane during flying The connection damage of rudder face hinge occurs, can also jeopardize flight safety.
Utility model content
To solve the above-mentioned problems, the utility model provides a kind of novel rudder face connection structure.
Specific technical solution is as follows:
A kind of novel rudder face connection structure, comprising: wingtip fin unit, rudder face end rib blade unit, rotary shaft, stringer and Wing;Described rudder face end rib blade unit one end is connect with stringer, and the other end is connect with wingtip fin unit;The rotary shaft is worn Rudder face end rib blade unit is crossed, both ends are fixedly connected with wing;The wingtip fin unit is made of N1 layers of fin, and the N1 >= 3;The rudder face end rib blade unit is made of N2 layers of fin, N2 >=3.
It preferably, further include mask.
Preferably, the outer surface of rudder face end rib blade unit is arranged in the mask.
Preferably, the fin number of the wingtip fin unit is equal to the fin number of rudder face end rib blade unit.
Preferably, the connection type between the fin of the wingtip fin unit be it is cementing, be bolted in magnetic It is one or more.
Preferably, the connection type between the fin of the rudder face end rib blade unit be it is cementing, be bolted in magnetic It is one or more.
Preferably, the connection type between rudder face end rib blade unit and wing is cementing, bolt to the rotary shaft respectively One of connection and magnetic are a variety of.
Preferably, the material of the wingtip fin unit is cork wood, aluminium alloy, steel, copper, carbon fiber, glass fibre, gathers One of ethylene and polylactic acid are a variety of.
Preferably, the material of the rudder face end rib blade unit is cork wood, aluminium alloy, steel, copper, carbon fiber, glass fibre, gathers One of ethylene and polylactic acid are a variety of.
Preferably, the material of the rotary shaft is cork wood, aluminium alloy, steel, copper, carbon fiber, glass fibre, polyethylene and gathers One of lactic acid is a variety of.
Compared with the existing technology, a kind of novel rudder face connection structure described in the utility model has the advantage that
The utility model proposes a kind of novel rudder face connection structure, at present on the market relatively simple articulated connection into It has gone optimization, the face contact stress of the point contact stress of script or small area is changed to the face contact stress of larger area, is changed Stress condition has been apt to it, has improved endurance, has reduced the probability of damage.
Detailed description of the invention
Fig. 1 be the utility model proposes a kind of novel rudder face connection structure schematic diagram;
Fig. 2 be the utility model proposes a kind of novel rudder face connection structure specific embodiment one schematic diagram;
Fig. 3 be the utility model proposes a kind of novel rudder face connection structure have mask schematic diagram.
Description of symbols:
1 wingtip fin unit, 24 stringer of rudder face end rib 3 rotary shaft of blade unit, 5 mask
11 fin A1,12 fin B1,13 fin A1 '
21 fin A2,22 fin B2,23 fin A2 '
Specific embodiment
The technical solution of the utility model is further described below in conjunction with specific embodiment.It should be appreciated that herein The specific embodiment of description is only used to explain the utility model, is not used to limit the utility model.
In the description of the present invention, it should be understood that term " center ", " longitudinal direction ", " transverse direction ", "upper", "lower", The orientation or positional relationship of the instructions such as "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of describing the present invention and simplifying the description, rather than indicate Or imply that signified device or element there must be specific side, be constructed and operated in a specific orientation, therefore should not be understood as Limitations of the present invention.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified Dress ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integrally Connection;It can be mechanical connection, be also possible to be electrically connected;Can be and be directly connected to, can also indirectly connected through an intermediary, It can be the connection inside two elements.For the ordinary skill in the art, on being understood by concrete condition State the concrete meaning of term in the present invention.
The utility model will be described in detail below with reference to the accompanying drawings and embodiments.
Fig. 1 be the utility model proposes a kind of novel rudder face connection structure schematic diagram, comprising: wingtip fin unit (1), rudder face end rib blade unit (2), rotary shaft (3), stringer (4) and wing;The rudder face end rib blade unit (2) one end and stringer (4) it connects, the other end is connect with wingtip fin unit (1);The rotary shaft (3) passes through rudder face end rib blade unit (2), both ends It is fixedly connected with wing, the connection type between rudder face end rib blade unit (2) and wing is glue to the rotary shaft (3) respectively It ties, be bolted and one of magnetic or a variety of;The wingtip fin unit (1) is made of N1 layers of fin, and the N1 >= 3, the connection type between the fin of the wingtip fin unit (1) be it is cementing, be bolted and one of magnetic or more Kind;The rudder face end rib blade unit (2) is made of N2 layers of fin, N2 >=3, the fin of the rudder face end rib blade unit (2) Between connection type be it is cementing, be bolted and one of magnetic or a variety of, the fin of the wingtip fin unit (1) Number is equal to the fin number of rudder face end rib blade unit (2).
The material of the wingtip fin unit (1) and rudder face end rib blade unit (2) is cork wood, aluminium alloy, steel, copper, carbon One of fiber, glass fibre, polyethylene and polylactic acid are a variety of.
The material of the rotary shaft (3) is cork wood, aluminium alloy, steel, copper, carbon fiber, glass fibre, polyethylene and polylactic acid One of or it is a variety of.
The utility model proposes a kind of novel rudder face connection structure further include mask (5), the mask (5) is arranged in rudder The outer surface of face end rib blade unit (2) makes entire wing more as shown in figure 3, the setting of mask (5) can reduce air drag Add smooth.
Specific embodiment one
Fig. 2 be the utility model proposes a kind of novel rudder face connection structure specific embodiment one schematic diagram, this is practical A kind of novel rudder face connection structure of novel proposition, including wingtip fin unit (1), rudder face end rib blade unit (2), rotary shaft (3), stringer (4) and mask (5);
The wingtip fin unit (1) is made of N1 layers of fin, mainly by fin A1 (11), fin A1 ' (13) and Fin B1 (12) composition, fin A1 (11) are identical with fin A1 ' (13) material;
The rudder face end rib blade unit (2) is made of N2 layers of fin, mainly by fin A2 (21), fin A2 ' (23) and Fin B2 (22) composition, fin A2 (21) are identical with fin A2 ' (23) material;
The rudder face end rib blade unit (2) one end is connect with stringer (4), and one end is connect with wingtip fin unit (1);
It is reserved on the A2 (21) and fin A2 ' (23) of the rudder face end rib blade unit (2) and rotary shaft (3) cross section The identical hole of size, the rotary shaft (3) pass through the hole;
The both ends of the rotary shaft (3) are fixed on the wing in addition to rudder face;
Upper and lower surface of the mask (5) in rudder face end rib blade unit (2).
The wingtip fin unit (1) is identical with rudder face end rib blade unit (2) fin element number, and element number can root It is arranged according to concrete condition;
Between the N1 layer fin of the wingtip fin unit (1) by it is cementing, be bolted, the modes such as magnetic connect.
Between the N2 layer fin of the rudder face end rib blade unit (2) by it is cementing, be bolted, the modes such as magnetic connect.
The fixed form of the rotary shaft (3) can for it is cementing, be bolted, magnetic etc.;
The fin material of the wingtip fin unit (1) and rudder face end rib blade unit (2) can for cork wood, aluminium alloy, Steel, copper, carbon fiber, glass fibre, polyethylene, polylactic acid etc.;
Rotary shaft (3) material can be cork wood, aluminium alloy, steel, copper, carbon fiber, glass fibre, polyethylene, poly- cream Acid etc..
In conclusion the utility model proposes a kind of novel rudder face connection structure, to relatively simple on the market at present Articulated connection is optimized, and the face that the face contact stress of the point contact stress of script or small area is changed to larger area is connect Stress is touched, stress condition is improved, improves endurance, reduce the probability of damage.
Above embodiment is preferred embodiments of the present invention, is not intended to limit the special of the utility model Sharp protection scope.Those skilled in the art belonging to any the utility model, it is disclosed in the utility model not departing from Under the premise of spirit and scope, the transformation of the equivalent structure and equivalent steps that done to the content of the utility model each falls within this reality Within novel claimed the scope of the patents.

Claims (7)

1. a kind of novel rudder face connection structure characterized by comprising wingtip fin unit (1), rudder face end rib blade unit (2), rotary shaft (3), stringer (4) and wing;
The rudder face end rib blade unit (2) one end is connect with stringer (4), and the other end is connect with wingtip fin unit (1);
The rotary shaft (3) passes through rudder face end rib blade unit (2), and both ends are fixedly connected with wing;
The wingtip fin unit (1) is made of N1 layers of fin, N1 >=3;
The rudder face end rib blade unit (2) is made of N2 layers of fin, N2 >=3.
2. a kind of novel rudder face connection structure according to claim 1, which is characterized in that further include mask (5).
3. a kind of novel rudder face connection structure according to claim 2, which is characterized in that the mask (5) is arranged in rudder The outer surface of face end rib blade unit (2).
4. a kind of novel rudder face connection structure according to claim 1, which is characterized in that the wingtip fin unit (1) fin number is equal to the fin number of rudder face end rib blade unit (2).
5. a kind of novel rudder face connection structure according to claim 1, which is characterized in that the wingtip fin unit (1) the connection type between fin be it is cementing, be bolted and one of magnetic or a variety of.
6. a kind of novel rudder face connection structure according to claim 1, which is characterized in that the rudder face end rib blade unit (2) the connection type between fin be it is cementing, be bolted and one of magnetic or a variety of.
7. a kind of novel rudder face connection structure according to claim 1, which is characterized in that the rotary shaft (3) respectively with Connection type between rudder face end rib blade unit (2) and wing be it is cementing, be bolted and one of magnetic or a variety of.
CN201820582662.8U 2018-04-23 2018-04-23 A kind of novel rudder face connection structure Active CN208683094U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820582662.8U CN208683094U (en) 2018-04-23 2018-04-23 A kind of novel rudder face connection structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820582662.8U CN208683094U (en) 2018-04-23 2018-04-23 A kind of novel rudder face connection structure

Publications (1)

Publication Number Publication Date
CN208683094U true CN208683094U (en) 2019-04-02

Family

ID=65876546

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820582662.8U Active CN208683094U (en) 2018-04-23 2018-04-23 A kind of novel rudder face connection structure

Country Status (1)

Country Link
CN (1) CN208683094U (en)

Similar Documents

Publication Publication Date Title
CN103552682B (en) A kind of all-wing aircraft and buzzard-type wing connection wing airplane
CN205440869U (en) Fixed chord flight time aircraft of canard configuration of VTOL
CN103192990A (en) Vertical/short take-off and landing flying wing layout aircraft
CN205633042U (en) Unmanned aerial vehicle
CN105129090A (en) Low resistance and low sonic boom layout supersonic aircraft
WO2017000156A1 (en) Double-blade tandem helicopter
CN107187599A (en) A kind of HAE aerodynamic configuration of aircraft of use two-shipper height rear wing Three-wing-surface
CN201633921U (en) Helicopter with empennage
CN105346720B (en) Blade, propeller and unmanned vehicle
CN206434864U (en) A kind of aircraft of VTOL
CN208683094U (en) A kind of novel rudder face connection structure
CN108100233B (en) Flaperon
CN111017185B (en) Laminar flow technology verification machine
CN103171758A (en) Lift-rising method of flying wing type airplane
CN108372926A (en) A kind of novel rudder face connection structure
CN108974361A (en) Canard and the hybrid layout unmanned plane of all-wing aircraft
CN203958600U (en) A kind of unmanned plane
CN106828911A (en) String wing unmanned plane
CN110550203A (en) Supersonic aircraft
CN201647122U (en) Pneumatic distribution of aircraft
CN216580979U (en) L-shaped structure vertical take-off and landing flight mechanism and aircraft
CN202541831U (en) Small wing of airplane
CN104015916A (en) Unmanned plane
CN205098475U (en) Vertical take -off and landing aircraft
CN203681870U (en) Vertical take-off and landing aircraft

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant