CN106275361A - A kind of dirigible abnormity layout empennage operating mechanism - Google Patents
A kind of dirigible abnormity layout empennage operating mechanism Download PDFInfo
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- CN106275361A CN106275361A CN201610753633.9A CN201610753633A CN106275361A CN 106275361 A CN106275361 A CN 106275361A CN 201610753633 A CN201610753633 A CN 201610753633A CN 106275361 A CN106275361 A CN 106275361A
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- empennage
- dirigible
- operating mechanism
- manipulated variable
- abnormity
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/12—Movable control surfaces
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
Abstract
The invention discloses a kind of dirigible abnormity layout empennage operating mechanism, including the manipulated variable changeover panel being arranged within dirigible and operating mechanism, by handling, bindiny mechanism is fixing with manipulated variable changeover panel to be connected operating mechanism, and operating mechanism drives manipulated variable changeover panel synchronous axial system；Dirigible afterbody is provided with and holds centrosymmetric abnormity layout empennage no less than 3, and each empennage all includes that rudder face and connecting rod, rudder face and connecting rod are vertical and fixing and connects；Connecting rod two ends are connected with manipulated variable changeover panel by Duo Liang bindiny mechanism, and manipulated variable changeover panel drives rudder face synchronous axial system by Duo Liang bindiny mechanism.Present invention reduces abnormity layout empennage operating mechanism design difficulty and implementation cost, enable abnormity layout empennage to be used more widely.
Description
Technical field
The present invention relates to dirigible empennage manipulation device technical field, particularly relate to a kind of dirigible abnormity layout empennage and handle machine
Structure.
Background technology
Dirigible abnormity empennage layout refers to the many tails being different from the X-shaped of cross-shape layout, Y shape even empennage quantity more than 4
Wing layout, abnormity layout empennage, according to the difference of distribution form, is each provided with the technical characterstic of uniqueness, such as X-shaped layout empennage
Can be substantially reduced dirigible height and width dimensions, working service is convenient.But the rudder face action of abnormity layout empennage and people
The direction of member, lifting are handled the most corresponding, it is impossible to directly handled by stick.At present, steerable system design needs to introduce electricity
Ore-controlling Role, is converted to the manipulated variable handling dirigible direction and lifting the rudder amount of each rudder face, and relies on automatically controlled steering wheel to tail
Wing rudder face is implemented to handle, and steerable system technical difficulty and implementation cost are higher, limits being widely used of abnormity layout.
Summary of the invention
The technical problem to be solved in the present invention is to control, for abnormity layout empennage in prior art, the defect that difficulty is big,
A kind of rudder face rudder amount that the direction of dirigible and lifting manipulated variable can be converted to abnormity layout empennage is provided, and drives rudder face to move
The dirigible abnormity layout empennage operating mechanism made.
The technical solution adopted for the present invention to solve the technical problems is:
The present invention provides a kind of dirigible abnormity layout empennage operating mechanism, including the manipulated variable conversion being arranged within dirigible
Dish and operating mechanism, by handling, bindiny mechanism is fixing with manipulated variable changeover panel to be connected operating mechanism, and operating mechanism drives to be handled
Amount changeover panel synchronous axial system；
Dirigible afterbody be provided with hold no less than 3 centrosymmetric abnormity layout empennage, each empennage all include rudder face and
Connecting rod, rudder face and connecting rod are vertical and fixing to be connected；Connecting rod two ends are connected with manipulated variable changeover panel by Duo Liang bindiny mechanism, handle
Amount changeover panel drives rudder face synchronous axial system by Duo Liang bindiny mechanism.
Further, the operating mechanism of the present invention includes the foot-driven lever of vertical manual joystick and level, manually handles
Bar and the fixing connection of foot-driven lever.
Further, the present invention handles the manipulating wire rope that bindiny mechanism is tensioning state, and manipulating wire rope is provided with
At least 4.
Further, the rudder dimension cord that Duo Liang bindiny mechanism is tensioning state of the present invention.
Further, the empennage of the present invention also includes hinge, and rudder face is fixed on the stabilization of empennage by hinge.
Further, the manipulated variable changeover panel of the present invention being additionally provided with two-freedom hinge, Duo Liang bindiny mechanism passes through
Two-freedom hinge is connected with manipulated variable changeover panel.
Further, the manual joystick of the operating mechanism of the present invention and the point of intersection of foot-driven lever, by hinge and dirigible
Connect.
Further, the Duo Liang bindiny mechanism that each rudder face of the present invention is corresponding changes in manipulated variable with two-freedom hinge
Intersecting at two junction points on dish, the line of two junction points is through the hinge centres of manipulated variable changeover panel, and this line hangs down
Straight in the median plane of this empennage stabilization；The amount of spin of each rudder face is identical at the component of this angle with pilot guidance amount.
Further, the dirigible afterbody of the present invention is provided with 4 and holds centrosymmetric empennage, forms X-shaped between empennage.
Further, the dirigible afterbody of the present invention is provided with 3 and holds centrosymmetric empennage, forms Y shape between empennage.
The beneficial effect comprise that: the dirigible abnormity layout empennage operating mechanism of the present invention, by by dirigible
Direction and lifting manipulated variable are converted to the rudder face rudder amount of abnormity layout empennage, and drive rudder face action, it is possible to use simple machine
Tool structure completes the manipulation work of the empennage to abnormity layout；Present invention reduces abnormity layout empennage operating mechanism design difficulty
And implementation cost, enable abnormity layout empennage to be used more widely；And this apparatus structure is simple, volume is little, lightweight,
Will not increase the extra heavy burden of dirigible, implementation cost is relatively low.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described, in accompanying drawing:
Fig. 1 is the overall structure schematic diagram of the embodiment of the present invention；
Fig. 2 is the manipulated variable input end structure schematic diagram of the dirigible abnormity layout empennage operating mechanism of the embodiment of the present invention；
Fig. 3 is the structural representation of the dirigible empennage of the embodiment of the present invention；
Fig. 4 is the rudder amount output end structure schematic diagram of the dirigible X-shaped layout empennage operating mechanism of the embodiment of the present invention；
Fig. 5 is the rudder amount output end structure schematic diagram of the dirigible Y shape layout empennage operating mechanism of the embodiment of the present invention；
In figure, 1-manipulated variable changeover panel, 2-two-freedom hinge, 3-operating mechanism, 4-handles bindiny mechanism, and 5-rudder amount is even
Connection mechanism, 6-rudder face, 7-hinge, 8-connecting rod, 9-stabilization.
Detailed description of the invention
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with drawings and Examples, right
The present invention is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the present invention, not
For limiting the present invention.
As it is shown in figure 1, the dirigible abnormity layout empennage operating mechanism of the embodiment of the present invention, including being arranged within dirigible
Manipulated variable changeover panel 1 and operating mechanism 3, by handling, bindiny mechanism 4 is fixing with manipulated variable changeover panel 1 to be connected operating mechanism 3, behaviour
Vertical mechanism 3 drives manipulated variable changeover panel 1 synchronous axial system；
Dirigible afterbody is provided with and holds centrosymmetric abnormity layout empennage no less than 3, and each empennage all includes rudder face 6 He
Connecting rod 8, rudder face 6 and connecting rod 8 are vertical and fixing to be connected；Duo Liang bindiny mechanism 5 and manipulated variable changeover panel 1 phase are passed through in connecting rod 8 two ends
Even, manipulated variable changeover panel 1 drives rudder face 6 synchronous axial system by Duo Liang bindiny mechanism 5.
As in figure 2 it is shown, operating mechanism 3 includes the foot-driven lever of vertical manual joystick and level, manual joystick and foot
Treadle is fixing to be connected.Handling the manipulating wire rope that bindiny mechanism 4 is tensioning state, manipulating wire rope is provided with at least 4.Rudder amount
Bindiny mechanism 5 is the rudder dimension cord of tensioning state.
As it is shown on figure 3, empennage also includes that hinge 7, rudder face 6 are fixed on the stabilization 9 of empennage by hinge 7.Manipulated variable
Being additionally provided with two-freedom hinge 2 on changeover panel 1, Duo Liang bindiny mechanism 5 is by two-freedom hinge 2 and manipulated variable changeover panel 1
It is connected.The manual joystick of operating mechanism 3 and the point of intersection of foot-driven lever, be connected with dirigible by hinge.
Duo Liang bindiny mechanism 5 and the two-freedom hinge 2 of each rudder face 6 correspondence intersect at two on manipulated variable changeover panel 1
Individual junction point, the line of two junction points is through the hinge centres of manipulated variable changeover panel 1, and this line is perpendicular to this empennage peace
Determine the median plane in face；The amount of spin of each rudder face 6 is identical at the component of this angle with pilot guidance amount.
Dirigible afterbody is provided with 4 and holds centrosymmetric empennage, forms X-shaped between empennage.Dirigible afterbody is provided with 3 and holds
Centrosymmetric empennage, forms Y shape between empennage.
In another specific embodiment of the present invention, the manipulated variable changeover panel 1 of abnormity layout empennage operating mechanism and behaviour
Vertical mechanism 3 is arranged in airship gondola by two-freedom hinge, by four between operating mechanism and manipulated variable changeover panel
Tight manipulating wire rope connects.When operating mechanism 3 rotates under the manipulation of pilot, manipulated variable changeover panel 1 is at manipulating wire
Synchronous axial system under the effect of rope.
The single empennage of dirigible is made up of stabilization 9 and rudder face 6, and rudder face 6 is fixed on stabilization 9 by hinge 7, rudder face
Connecting rod 8 it is fixed with on 6.
The described connecting rod 8 being fixed together with rudder face 6 is connected with manipulated variable changeover panel 1 by rudder dimension cord, rudder amount
Steel wire rope remains tensioning state by adjustment, makes rudder face 6 and manipulated variable changeover panel 1 synchronous axial system.
Rudder face 6 and manipulated variable changeover panel 1 connect with this empennage on ship capsule residing for established angle relevant, such as Fig. 4 and Fig. 5
Shown in, when manipulated variable changeover panel is in the centre position without handling, each rudder face 6 junction point on manipulated variable changeover panel 1
Being 2, the line of 2 junction points is through the hinge centres of manipulated variable changeover panel 1, and this line is perpendicular to this empennage stabilization
Median plane.Now, the amount of spin of the rudder face of each established angle is identical at the component of this angle with pilot guidance amount, therefore,
Under each rudder face mating reaction, the produced turning efficiency of making a concerted effort of all rudder face aerodynamic force i.e. may conform to the manipulation meaning of pilot
Figure, makes dirigible complete to turn to according to the requirement of pilot.
Operating mechanism contains a manipulated variable changeover panel, and changeover panel is arranged on a two degrees of freedom turning joint, energy
Enough two degrees of freedom rotates.Former and later two faces of control handwheel are connected with pilot stick and rudder face respectively by steel wire rope, make respectively
For manipulated variable input and rudder amount outfan.Input connects pilot's lift control lever and direction joystick, rudder by steel wire
Amount outfan connects empennage rudder face by steel wire.The installation on changeover panel of the outfan steel wire rope is changed according to empennage distribution form
Relative angle, it is possible to by the lifting of pilot and directional control amount by the rudder amount that the method migration of machinery is abnormity empennage, right
Abnormity empennage realizes directly controlling.For using motor-driven empennage, sensor installed by the outfan of changeover panel mechanism, moreover it is possible to
Enough replace control system, pilot guidance amount is directly changed into abnormity empennage control the rudder amount signal of telecommunication, simplified control system,
Improve system reliability.
It should be appreciated that for those of ordinary skills, can be improved according to the above description or be converted,
And all these modifications and variations all should belong to the protection domain of claims of the present invention.
Claims (10)
1. a dirigible abnormity layout empennage operating mechanism, it is characterised in that include the manipulated variable conversion being arranged within dirigible
Dish (1) and operating mechanism (3), by handling, bindiny mechanism (4) is fixing with manipulated variable changeover panel (1) to be connected operating mechanism (3), behaviour
Vertical mechanism (3) drives manipulated variable changeover panel (1) synchronous axial system；
Dirigible afterbody is provided with and holds centrosymmetric abnormity layout empennage no less than 3, and each empennage all includes rudder face (6) and connects
Bar (8), rudder face (6) and connecting rod (8) are vertical and fixing to be connected；Connecting rod (8) two ends are turned with manipulated variable by Duo Liang bindiny mechanism (5)
Changing dish (1) to be connected, manipulated variable changeover panel (1) drives rudder face (6) synchronous axial system by Duo Liang bindiny mechanism (5).
Dirigible abnormity layout empennage operating mechanism the most according to claim 1, it is characterised in that operating mechanism (3) includes
Vertical manual joystick and the fixing connection of the foot-driven lever of level, manual joystick and foot-driven lever.
Dirigible abnormity layout empennage operating mechanism the most according to claim 1, it is characterised in that handle bindiny mechanism (4)
For the manipulating wire rope of tensioning state, manipulating wire rope is provided with at least 4.
Dirigible abnormity layout empennage operating mechanism the most according to claim 1, it is characterised in that Duo Liang bindiny mechanism (5)
Rudder dimension cord for tensioning state.
Dirigible abnormity layout empennage operating mechanism the most according to claim 1, it is characterised in that empennage also includes hinge
(7), rudder face (6) is fixed on the stabilization (9) of empennage by hinge (7).
Dirigible abnormity layout empennage operating mechanism the most according to claim 1, it is characterised in that manipulated variable changeover panel (1)
On be additionally provided with two-freedom hinge (2), Duo Liang bindiny mechanism (5) is by two-freedom hinge (2) and manipulated variable changeover panel (1)
It is connected.
Dirigible abnormity layout empennage operating mechanism the most according to claim 2, it is characterised in that the hands of operating mechanism (3)
Dynamic stick and the point of intersection of foot-driven lever, be connected with dirigible by hinge.
Dirigible abnormity layout empennage operating mechanism the most according to claim 6, it is characterised in that each rudder face (6) is corresponding
Duo Liang bindiny mechanism (5) and two-freedom hinge (2) on manipulated variable changeover panel (1), intersect at two junction points, two companies
The line of contact is through the hinge centres of manipulated variable changeover panel (1), and this line is perpendicular to the median plane of this empennage stabilization；
The amount of spin of each rudder face (6) is identical at the component of this angle with pilot guidance amount.
Dirigible abnormity layout empennage operating mechanism the most according to claim 1, it is characterised in that dirigible afterbody is provided with 4
Individual hold centrosymmetric empennage, between empennage, form X-shaped.
Dirigible abnormity layout empennage operating mechanism the most according to claim 1, it is characterised in that dirigible afterbody is provided with 3
Individual hold centrosymmetric empennage, between empennage, form Y shape.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610753633.9A CN106275361B (en) | 2016-08-29 | 2016-08-29 | A kind of dirigible abnormity layout empennage operating mechanism |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610753633.9A CN106275361B (en) | 2016-08-29 | 2016-08-29 | A kind of dirigible abnormity layout empennage operating mechanism |
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| Publication Number | Publication Date |
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| CN106275361A true CN106275361A (en) | 2017-01-04 |
| CN106275361B CN106275361B (en) | 2019-05-24 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610753633.9A Active CN106275361B (en) | 2016-08-29 | 2016-08-29 | A kind of dirigible abnormity layout empennage operating mechanism |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106910386A (en) * | 2017-04-18 | 2017-06-30 | 河北天启通宇航空器材科技发展有限公司 | Manipulation device link gear is used in gyroplane teaching |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1602545A (en) * | 1967-10-31 | 1970-12-21 | ||
| CN201254293Y (en) * | 2008-08-26 | 2009-06-10 | 安徽省华云高科技有限责任公司 | Novel power airship |
| CN104309795A (en) * | 2014-10-22 | 2015-01-28 | 襄阳宏伟航空器有限责任公司 | Low-altitude detection floating platform |
| CN205239897U (en) * | 2015-11-18 | 2016-05-18 | 广州广鸿航空科技有限公司 | Mechanism is controlled in step to unmanned aerial vehicle tailwheel and rudder |
| CN205998111U (en) * | 2016-08-29 | 2017-03-08 | 航宇救生装备有限公司 | A kind of dirigible abnormity layout empennage operating mechanism |
-
2016
- 2016-08-29 CN CN201610753633.9A patent/CN106275361B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1602545A (en) * | 1967-10-31 | 1970-12-21 | ||
| CN201254293Y (en) * | 2008-08-26 | 2009-06-10 | 安徽省华云高科技有限责任公司 | Novel power airship |
| CN104309795A (en) * | 2014-10-22 | 2015-01-28 | 襄阳宏伟航空器有限责任公司 | Low-altitude detection floating platform |
| CN205239897U (en) * | 2015-11-18 | 2016-05-18 | 广州广鸿航空科技有限公司 | Mechanism is controlled in step to unmanned aerial vehicle tailwheel and rudder |
| CN205998111U (en) * | 2016-08-29 | 2017-03-08 | 航宇救生装备有限公司 | A kind of dirigible abnormity layout empennage operating mechanism |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106910386A (en) * | 2017-04-18 | 2017-06-30 | 河北天启通宇航空器材科技发展有限公司 | Manipulation device link gear is used in gyroplane teaching |
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| Publication number | Publication date |
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| CN106275361B (en) | 2019-05-24 |
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