CN106564580A - Airship - Google Patents
Airship Download PDFInfo
- Publication number
- CN106564580A CN106564580A CN201610913828.5A CN201610913828A CN106564580A CN 106564580 A CN106564580 A CN 106564580A CN 201610913828 A CN201610913828 A CN 201610913828A CN 106564580 A CN106564580 A CN 106564580A
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- China
- Prior art keywords
- center
- pole
- dirigible
- connecting rod
- skeleton
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- 239000002775 capsule Substances 0.000 claims abstract description 118
- 239000004744 fabric Substances 0.000 claims description 18
- 230000002459 sustained effect Effects 0.000 claims description 3
- 230000008901 benefit Effects 0.000 abstract description 6
- 238000012423 maintenance Methods 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 10
- 238000000034 method Methods 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000007789 sealing Methods 0.000 description 5
- 238000009432 framing Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 210000000988 bone and bone Anatomy 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- 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
- B64B1/08—Framework construction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Actuator (AREA)
- Toys (AREA)
Abstract
The invention relates to an airship comprising a framework and an airship capsule, wherein the framework is arranged in the airship capsule to support the airship capsule; horizontal empennages are arranged on the rear part of both sides of the airship capsule; one or more perpendicular empennages are arranged on the rear part of the top of the airship capsule; the horizontal empennages and the perpendicular empennages are all provided with control surfaces; the control surfaces are rotationally connected to the horizontal empennages and the perpendicular empennages; the number of the perpendicular empennages is adjusted according to the width of the airship capsule; the framework includes a plurality of center rods which are arranged along the direction of the body of the airship, and the center rods are connected by connecting rods; and the rear parts of the center rods are equipped with one or more rear propeller devices which are provided with driving devices. Being equipped with the structure, the airship effectively solves the technical problems that a traditional non-rigid airship is low in strength, limited in size and high in air pressure maintenance, and the auxiliary facilities of the traditional non-rigid airship capsule affect the strength of the same and causes the deformation of the same. The airship has the advantages of being simple in structure, great in rigidity, high in strength, free from limitation by the size of the airship and light in structure.
Description
Technical field
The present invention relates to aircraft field, more particularly to a kind of dirigible.
Background technology
Modern dirigible is typically all blimp, to keep their profile, can only be by helium pressure in air bag come
Realize.Blimp is typically small, and in below 30m, its low intensity, air pressure remains big to general length, and affiliated facility is to ship capsule
Tension intensity is big so that the deformation of ship capsule is big.
Therefore, gently, rigidly the big dirigible of good, length length, load-carrying seems particularly necessary to study a kind of structure.
The content of the invention
The technical problem to be solved in the present invention is the big dirigible of a kind of light structure of design, good, the length length of rigidity, load-carrying, solution
Certainly existing technical problem.
To solve above-mentioned technical problem, the dirigible of the present invention includes skeleton and ship capsule, and the skeleton is placed in the intracapsular support of ship
Ship capsule, the ship capsule both sides are provided with tailplane, and tailplane is arranged on ship capsule sidepiece rear, and the ship capsule top is provided with vertical
Empennage, vertical tail is arranged on ship capsule top rear, and the tailplane and vertical tail are equipped with rudder face, the rudder face and water
The horizontal tail wing rotates connection, and the rudder face is rotated with vertical tail and is connected；The number of vertical tail is suitably adjusted according to ship bag beam degree；
The skeleton includes many center-poles, and the center-pole is arranged along dirigible kayak body direction, and connecting rod is passed through between the center-pole
Connection, the center-pole afterbody is provided with rear screw shaft device, and the rear screw shaft device is provided with driving means.
Further, the rotational angle of the rudder face is -90 °～90 °, i.e., clockwise around tailplane or vertical tail
The angular range of rotation is 0～90 °, and the angular range of rotate counterclockwise is 0～90 °, and the power for turning to is provided to dirigible.
Further, the connection pole length is more than the Breadth Maximum between center-pole.
Further, the ship capsule is provided with hollow cavity, and the center-pole and connecting rod are placed in the hollow cavity, institute
Center-pole and ship capsule inner wall are stated by pulling rope and drawing cloth connection, described pulling rope one end is connected with center-pole, the other end and
Drawing cloth connection, described drawing cloth one end is connected with pulling rope, and the other end is connected with ship capsule inner wall.The design of hollow cavity is just
The center-pole or connecting rod of skeleton can be accommodated, can be processed with it goes without doing air-tightness while structural strength is ensured.Certainly, bone
The junction of frame and ship capsule can also adopt conventional seals structure, and in the junction of skeleton and ship capsule sealing structure is provided with.Dirigible
Bottom hung weight（Such as gondola）, the effect for pulling structure is that the weight average of weight is distributed to into dirigible ship capsule surface and bone
On frame.
Further, the connecting rod and the connected mode of center-pole are chain connection or bolt connection.
Further, the rear screw shaft device includes driver, and the driver connects propeller, the driver
Installing rack is provided with mutually perpendicular horizontal stand and vertical support frame, and the horizontal rudder face of connection is rotated on the horizontal stand, described
Horizontal stand is provided with the horizontal rudder face rotation of the first Motor drive, and the vertical rudder face of connection is rotated on the vertical support frame, described vertical
Support is provided with the vertical rudder face rotation of the second Motor drive.The driver is electromotor or motor.
Or, the rear screw shaft device includes base, first support, second support, propeller and driver, described the
One support is connected with base rotation, and the base is provided with the rotation of the 3rd Motor drive first support, the second support and first
Holder pivots connect, and the first support is provided with the rotation of the 4th Motor drive second support, and the second support is provided with driver
And propeller, the driver drives propeller rotation.The driver is electromotor or motor.
Or, the rear screw shaft device includes base and actuator base, and described actuator base one end is provided with driving
Device and propeller, the driver drives propeller rotation, the other end is with base by mutually perpendicular first rotating shaft and second
Axis of rotation connects, and the base and actuator base side are connected by universal joint and flexible servomechanism, the base with fly
Ship is fixedly connected, and the actuator base can realize the steering of dirigible around first rotating shaft left-right rotation, and the actuator base can
The luffing angle for changing dirigible is rotated upwardly and downwardly around the second rotating shaft.The driver is electromotor or motor.
Further, the skeleton includes two parallel center-poles, and connecting rod is respectively equipped with front and back between the center-pole
Connection, anterior connecting rod both sides are provided with side propeller set.The structure of side propeller set is aforementioned three kinds of rear screw shafts dress
One kind in putting.
Further, the skeleton includes three center-poles, and three center-poles are distinguished in front and back between same plane, center-pole
Connecting rod connection is provided with, anterior connecting rod both sides are provided with side propeller set.The structure of side propeller set is aforementioned three kinds
One kind in rear screw shaft device.
Further, the skeleton includes three center-poles, and the first center-pole is parallel to the second center-pole and the 3rd center
The plane that bar is located, the projection of the plane that the first center-pole is located in the second center-pole and the 3rd center-pole is located at the second center-pole
And the 3rd between center-pole, connecting rod group is respectively equipped with before and after the first center-pole and the second center-pole and the 3rd center-pole, is connected
Bar group to be referred to and connect two connecting rods of the second center-pole and the 3rd center-pole, anterior connecting rod respectively in head rod somewhere
Group both sides are provided with side propeller set.The structure of side propeller set is the one kind in aforementioned three kinds of rear screw shaft devices.
Further, the skeleton includes three center-poles, and three center-poles are anterior in sustained height, and rear portion is different high
Degree, front portion is provided with connecting rod between the center-pole, and rear portion is provided with connecting rod group, and anterior connecting rod both sides are provided with side propeller dress
Put.The structure of side propeller set is the one kind in aforementioned three kinds of rear screw shaft devices.
Further, the skeleton also includes bracing piece, and the bracing piece is vertically arranged.The design of bracing piece can enter one
The structure of step web frame, so as to strengthen the intensity of dirigible, and for the length for increasing dirigible also functions to positive role.
Further, dirigible also includes gondola, and the gondola is located at dirigible bottom.
The principle of the present invention：The present invention strengthens the structure of ship capsule by way of arranging skeleton in the intracapsular portion of ship, rigidity
Good, intensity is big, makes that dirigible size is unrestricted, solves the short technical problem of the low intensity of traditional blimp, hull, and
And simple structure, gently, what skeleton was primarily served is the effect for supporting whole ship capsule to structure, does not limit it and specifically includes center
The quantity of bar, connecting rod and bracing piece, the quantity of center-pole is related to the intensity of the width of dirigible and design requirement, connecting rod
Quantity it is related to the intensity of the length of dirigible and design requirement, the quantity of bracing piece and the size of dirigible and design requirement
Intensity it is related.
Beneficial effects of the present invention：After using such structure, efficiently solve that traditional blimp intensity is relatively low, size
Limited, air pressure maintains the technical problem that big, ship capsule affiliated facility affects ship capsule intensity to cause ship capsule to deform, have simple structure,
The good, intensity of rigidity is big, not by the advantage that dirigible size is limited and structure is light.
Description of the drawings
The specific embodiment of the present invention is further elucidated below in conjunction with the accompanying drawings.
Fig. 1 is that the intracapsular portion of dirigible ship of the present invention pulls structural representation；
Fig. 2 is the structural representation of the dirigible in embodiment 1；
Fig. 3 is the framing structure schematic diagram of the dirigible in embodiment 1；
Fig. 4 is a kind of propeller set structural representation of dirigible of the present invention；
Fig. 5 is another kind of propeller set structural representation of dirigible of the present invention；
Fig. 6 is another kind of propeller set structural representation of dirigible of the present invention；
Fig. 7 is the structural representation of the dirigible in embodiment 2；
Fig. 8 is the framing structure schematic diagram of the dirigible in embodiment 2；
Fig. 9 is the structural representation of the dirigible in embodiment 3；
The framing structure schematic diagram of the dirigible in Figure 10 embodiments 3；
The structural representation of the dirigible in Figure 11 embodiments 4；
The framing structure schematic diagram of the dirigible in Figure 12 embodiments 4；
Figure 13 is the dirigible schematic diagram of four body ship capsule structures.
Specific embodiment
Embodiment 1
With reference to Fig. 1, Fig. 2 and Fig. 3, the dirigible of the present invention includes skeleton and ship capsule 1, and the skeleton is placed in the inner support ship capsule of ship capsule 1
1, the both sides of ship capsule 1 are provided with tailplane 101, and tailplane 101 is arranged on the sidepiece rear of ship capsule 1, and the top of the ship capsule 1 sets
There is vertical tail 102, vertical tail 102 is arranged on the top rear of ship capsule 1, and the tailplane 101 and vertical tail 102 are all provided with
There is rudder face 5, the rudder face 5 is rotated with tailplane 101 and is connected, and the rudder face 5 is rotated with vertical tail 102 and is connected；Vertical end
The number of the wing 102 is suitably adjusted according to the width of ship capsule 1；The skeleton includes many center-poles, and the center-pole is along dirigible kayak body
Direction is arranged, and is connected by connecting rod 22 between the center-pole, and the center-pole afterbody is provided with rear screw shaft device 3, described
Rear screw shaft device 3 is provided with driving means.In the present embodiment, the top rear of ship capsule 1 is provided with 2 vertical tails 102.
Further, the rotational angle of the rudder face 5 is -90 °～90 °, i.e., around tailplane 101 or vertical tail
102 angular ranges for turning clockwise are 0～90 °, and the angular range of rotate counterclockwise is 0～90 °, provides what is turned to dirigible
Power.
Further, the length of the connecting rod 22 is more than the Breadth Maximum between center-pole.
Further, the ship capsule 1 is provided with hollow cavity, and the center-pole and connecting rod 22 are placed in the hollow cavity
Interior, the center-pole and ship capsule inner wall are connected by pulling rope 7 and drawing cloth 6, and the one end of the pulling rope 7 is connected with center-pole,
The other end is connected with drawing cloth 6, and described drawing one end of cloth 6 is connected with pulling rope 7, and the other end is connected with ship capsule inner wall.In hollow
The design in chamber can just accommodate the center-pole or connecting rod 22 of skeleton, can be airtight so that it goes without doing while structural strength is ensured
Property process.Certainly, the junction of skeleton and ship capsule 1 can also adopt conventional seals structure, set in the junction of skeleton and ship capsule 1
There is sealing structure.Dirigible bottom hung weight（Such as gondola）, the effect for pulling structure is to be distributed to the weight average of weight
On dirigible ship capsule surface and skeleton.
Further, the connecting rod 22 and the connected mode of center-pole are chain connection or bolt connection.
As shown in figure 4, in the present embodiment, the rear screw shaft device 3 includes driver 8, the connection spiral of the driver 8
Oar 9, the installing rack of the driver 8 is provided with mutually perpendicular horizontal stand 810 and vertical support frame 811, the horizontal stand
The horizontal rudder face 812 of connection is rotated on 810, the horizontal stand 810 is provided with the horizontal rudder face 812 of the driving of the first motor 814 and rotates, changes
Become dirigible luffing angle, the vertical rudder face 813 of connection is rotated on the vertical support frame 811, it is electric that the vertical support frame 811 is provided with second
Machine 815 drives vertical rudder face 813 to rotate, and changes dirigible direction of advance.The driver 8 is electromotor or motor.
This enforcement is preferred, and the skeleton includes two parallel center-poles 21, is respectively equipped with front and back between the center-pole
Connecting rod 22 connects, and more than the distance between two center-poles 21, the anterior both sides of connecting rod 22 are provided with the length of connecting rod 22
Side propeller set 4.In the present embodiment, side propeller set is identical with the structure of rear screw shaft device 3 in the present embodiment, such as schemes
Shown in 4.
Further, the skeleton also includes bracing piece 23, and the bracing piece 23 is vertically arranged.In the present embodiment, strengthen
Bar 23 has 2, is arranged on the connecting rod 22 at rear portion and the junction of center-pole 21.The design of bracing piece 23 can further be strengthened
The structure of skeleton, so as to strengthen the intensity of dirigible, and for the length for increasing dirigible also functions to positive role.
Further, dirigible also includes gondola, and the gondola is located at dirigible bottom.
The principle of the present embodiment：By way of skeleton is set inside ship capsule 1, the structure of ship capsule 1 is strengthened, rigidity
Good, intensity is big, makes that dirigible size is unrestricted, solves the short technical problem of the low intensity of traditional blimp, hull, and
And simple structure, gently, what skeleton was primarily served is the effect for supporting whole ship capsule 1 to structure, does not limit it and specifically includes center
The quantity of bar, connecting rod 22 and bracing piece 23, the quantity of center-pole is related to the intensity of the width of dirigible and design requirement, even
The quantity of extension bar 22 is related to the intensity of the length of dirigible and design requirement, the quantity of bracing piece 23 and the size of dirigible and
The intensity of design requirement is related.
The dirigible of the present embodiment efficiently solves relatively low traditional blimp intensity, limited size, air pressure and maintains big, ship capsule
Affiliated facility affects the technical problem that ship capsule intensity causes ship capsule to deform, and has simple structure, rigid good, intensity greatly, to be flown
Ship size is limited and the light advantage of structure.
Embodiment 2
With reference to Fig. 1, Fig. 7 and Fig. 8, the dirigible of the present invention includes skeleton and ship capsule 1, and the skeleton is placed in the inner support ship capsule of ship capsule 1
1, the both sides of ship capsule 1 are provided with tailplane 101, and tailplane 101 is arranged on the sidepiece rear of ship capsule 1, and the top of the ship capsule 1 sets
There is vertical tail 102, vertical tail 102 is arranged on the top rear of ship capsule 1, and the tailplane 101 and vertical tail 102 are all provided with
There is rudder face 5, the rudder face 5 is rotated with tailplane 101 and is connected, and the rudder face 5 is rotated with vertical tail 102 and is connected；Vertical end
The number of the wing 102 is suitably adjusted according to the width of ship capsule 1；The skeleton includes many center-poles, and the center-pole is along dirigible kayak body
Direction is arranged, and is connected by connecting rod 22 between the center-pole, and the center-pole afterbody is provided with rear screw shaft device 3, described
Rear screw shaft device 3 is provided with driving means.In the present embodiment, the top rear of ship capsule 1 is provided with 3 vertical tails 102.
Further, the rotational angle of the rudder face 5 is -90 °～90 °, i.e., around tailplane 101 or vertical tail
102 angular ranges for turning clockwise are 0～90 °, and the angular range of rotate counterclockwise is 0～90 °, provides what is turned to dirigible
Power.
Further, the length of the connecting rod 22 is more than the Breadth Maximum between center-pole.
Further, the ship capsule 1 is provided with hollow cavity, and the center-pole and connecting rod 22 are placed in the hollow cavity
Interior, the center-pole and ship capsule inner wall are connected by pulling rope 7 and drawing cloth 6, and the one end of the pulling rope 7 is connected with center-pole,
The other end is connected with drawing cloth 6, and described drawing one end of cloth 6 is connected with pulling rope 7, and the other end is connected with ship capsule inner wall.In hollow
The design in chamber can just accommodate the center-pole or connecting rod 22 of skeleton, can be airtight so that it goes without doing while structural strength is ensured
Property process.Certainly, the junction of skeleton and ship capsule 1 can also adopt conventional seals structure, set in the junction of skeleton and ship capsule 1
There is sealing structure.Dirigible bottom hung weight（Such as gondola）, the effect for pulling structure is to be distributed to the weight average of weight
On dirigible ship capsule surface and skeleton.
Further, the connecting rod 22 and the connected mode of center-pole are chain connection or bolt connection.
As shown in figure 5, in the present embodiment, rear screw shaft device 3 includes base 820, first support 821, second support
822nd, propeller 9 and driver 8, the first support 821 is rotated with base 820 and is connected, and the base 820 is provided with the 3rd motor
823 driving first supports 821 rotate, and change dirigible luffing angle, and the second support 822 is rotated with first support 821 and is connected,
The first support 821 is provided with the 4th Motor drive second support 822 and rotates, and changes dirigible direction of advance, the second support
822 are provided with driver 8 and propeller 9, and the driver 8 drives propeller 9 to rotate.The driver 8 is electromotor or electronic
Machine.
The present embodiment is preferred, and the skeleton includes three center-poles, before three center-poles are between same plane, center-pole
After be respectively equipped with connecting rod 22 and connect, the length of connecting rod 22 is more than the distance between adjacent two center-poles 21, anterior company
The both sides of extension bar 22 are provided with side propeller set 4.In the present embodiment, side propeller set 4 is filled with the rear screw shaft in the present embodiment
Put 3 structures identical.Preferably, three center-poles are parallel two-by-two.
Further, the skeleton also includes bracing piece 23, and the bracing piece 23 is vertically arranged.In the present embodiment, strengthen
Bar 23 is 3.The design of bracing piece 23 can further web frame structure, so as to strengthen the intensity of dirigible, and for
The length for increasing dirigible also functions to positive role.
Further, dirigible also includes gondola, and the gondola is located at dirigible bottom.
The principle of the present embodiment：By way of skeleton is set inside ship capsule 1, the structure of ship capsule 1 is strengthened, rigidity
Good, intensity is big, makes that dirigible size is unrestricted, solves the short technical problem of the low intensity of traditional blimp, hull, and
And simple structure, gently, what skeleton was primarily served is the effect for supporting whole ship capsule 1 to structure, does not limit it and specifically includes center
The quantity of bar, connecting rod 22 and bracing piece 23, the quantity of center-pole is related to the intensity of the width of dirigible and design requirement, even
The quantity of extension bar 22 is related to the intensity of the length of dirigible and design requirement, the quantity of bracing piece 23 and the size of dirigible and
The intensity of design requirement is related.
The dirigible of the present embodiment efficiently solves relatively low traditional blimp intensity, limited size, air pressure and maintains big, ship capsule
Affiliated facility affects the technical problem that ship capsule intensity causes ship capsule to deform, and has simple structure, rigid good, intensity greatly, to be flown
Ship size is limited and the light advantage of structure.
Embodiment 3
With reference to Fig. 1, Fig. 9 and Figure 10, the dirigible of the present invention includes skeleton and ship capsule 1, and the skeleton is placed in the inner support ship capsule of ship capsule 1
1, the both sides of ship capsule 1 are provided with tailplane 101, and tailplane 101 is arranged on the sidepiece rear of ship capsule 1, and the top of the ship capsule 1 sets
There is vertical tail 102, vertical tail 102 is arranged on the top rear of ship capsule 1, and the tailplane 101 and vertical tail 102 are all provided with
There is rudder face 5, the rudder face 5 is rotated with tailplane 101 and is connected, and the rudder face 5 is rotated with vertical tail 102 and is connected；Vertical end
The number of the wing 102 is suitably adjusted according to the width of ship capsule 1；The skeleton includes many center-poles, and the center-pole is along dirigible kayak body
Direction is arranged, and is connected by connecting rod 22 between the center-pole, and the center-pole afterbody is provided with rear screw shaft device 3, described
Rear screw shaft device 3 is provided with driving means.In the present embodiment, the top rear of ship capsule 1 is provided with 3 vertical tails 102.
Further, the rotational angle of the rudder face 5 is -90 °～90 °, i.e., around tailplane 101 or vertical tail
102 angular ranges for turning clockwise are 0～90 °, and the angular range of rotate counterclockwise is 0～90 °, provides what is turned to dirigible
Power.
Further, the length of the connecting rod 22 is more than the Breadth Maximum between center-pole.
Further, the ship capsule 1 is provided with hollow cavity, and the center-pole and connecting rod 22 are placed in the hollow cavity
Interior, the center-pole and ship capsule inner wall are connected by pulling rope 7 and drawing cloth 6, and the one end of the pulling rope 7 is connected with center-pole,
The other end is connected with drawing cloth 6, and described drawing one end of cloth 6 is connected with pulling rope 7, and the other end is connected with ship capsule inner wall.In hollow
The design in chamber can just accommodate the center-pole or connecting rod 22 of skeleton, can be airtight so that it goes without doing while structural strength is ensured
Property process.Certainly, the junction of skeleton and ship capsule 1 can also adopt conventional seals structure, set in the junction of skeleton and ship capsule 1
There is sealing structure.Dirigible bottom hung weight（Such as gondola）, the effect for pulling structure is to be distributed to the weight average of weight
On dirigible ship capsule surface and skeleton.
Further, the connecting rod 22 and the connected mode of center-pole are chain connection or bolt connection.
As shown in fig. 6, in the present embodiment, rear screw shaft device 3 includes base 830 and actuator base 831, the driving
The one end of device base 831 is provided with driver 8 and propeller 9, and the driver 8 drives propeller 9 to rotate, the other end and base 830
Connection, the base 830 and the side of actuator base 831 are rotated by 832 and second rotating shaft of mutually perpendicular first rotating shaft 833
Connected by universal joint 834 and flexible servomechanism 835, the base 830 is fixedly connected with dirigible, the actuator base 831
The steering of dirigible can be realized around the left-right rotation of first rotating shaft 832, the actuator base 831 can turn around the second rotating shaft about 833
The dynamic luffing angle for changing dirigible.The driver 8 is electromotor or motor.
Further, the base 830 and actuator base 831 connect respectively side by two groups of flexible servomechanisms 835
Universal joint 834.The present embodiment is preferred, and the skeleton includes three center-poles, and three center-poles are anterior in sustained height, after
In differing heights, front portion is provided with connecting rod 22 between the center-pole in portion, and rear portion is provided with connecting rod group, and the both sides of anterior connecting rod 22 set
There is side propeller set 4.In the present embodiment, side propeller set 4 is identical with the structure of rear screw shaft device 3 in the present embodiment.
Further, the skeleton also includes bracing piece 23, and the bracing piece 23 is vertically arranged.In the present embodiment, strengthen
Bar 23 is 3, and bracing piece 23 is arranged at center-pole rear portion, and vertical with center-pole.The design of bracing piece 23 can be further
The structure of web frame, so as to strengthen the intensity of dirigible, and for the length for increasing dirigible also functions to positive role.
Further, dirigible also includes gondola, and the gondola is located at dirigible bottom.
The principle of the present embodiment：By way of skeleton is set inside ship capsule 1, the structure of ship capsule 1 is strengthened, rigidity
Good, intensity is big, makes that dirigible size is unrestricted, solves the short technical problem of the low intensity of traditional blimp, hull, and
And simple structure, gently, what skeleton was primarily served is the effect for supporting whole ship capsule 1 to structure, does not limit it and specifically includes center
The quantity of bar, connecting rod 22 and bracing piece 23, the quantity of center-pole is related to the intensity of the width of dirigible and design requirement, even
The quantity of extension bar 22 is related to the intensity of the length of dirigible and design requirement, the quantity of bracing piece 23 and the size of dirigible and
The intensity of design requirement is related.
The dirigible of the present embodiment efficiently solves relatively low traditional blimp intensity, limited size, air pressure and maintains big, ship capsule
Affiliated facility affects the technical problem that ship capsule intensity causes ship capsule to deform, and has simple structure, rigid good, intensity greatly, to be flown
Ship size is limited and the light advantage of structure.
Embodiment 4
With reference to Fig. 1, Figure 11 and Figure 12, the dirigible of the present invention includes skeleton and ship capsule 1, and the skeleton is placed in the inner support ship of ship capsule 1
Capsule 1, the both sides of ship capsule 1 are provided with tailplane 101, and tailplane 101 is arranged on the sidepiece rear of ship capsule 1, the top of the ship capsule 1
Vertical tail 102 is provided with, vertical tail 102 is arranged on the top rear of ship capsule 1, and the tailplane 101 and vertical tail 102 are equal
Rudder face 5 is provided with, the rudder face 5 is rotated with tailplane 101 and is connected, and the rudder face 5 is rotated with vertical tail 102 and is connected；Vertically
The number of empennage 102 is suitably adjusted according to the width of ship capsule 1；The skeleton includes many center-poles, and the center-pole is along dirigible ship
Body direction is arranged, and is connected by connecting rod 22 between the center-pole, and the center-pole afterbody is provided with rear screw shaft device 3, institute
State rear screw shaft device 3 and be provided with driving means.In the present embodiment, the top rear of ship capsule 1 is provided with 3 vertical tails 102.
Further, the rotational angle of the rudder face 5 is -90 °～90 °, i.e., around tailplane 101 or vertical tail
102 angular ranges for turning clockwise are 0～90 °, and the angular range of rotate counterclockwise is 0～90 °, provides what is turned to dirigible
Power.
Further, the length of the connecting rod 22 is more than the Breadth Maximum between center-pole.
Further, the ship capsule 1 is provided with hollow cavity, and the center-pole and connecting rod 22 are placed in the hollow cavity
Interior, the center-pole and ship capsule inner wall are connected by pulling rope 7 and drawing cloth 6, and the one end of the pulling rope 7 is connected with center-pole,
The other end is connected with drawing cloth 6, and described drawing one end of cloth 6 is connected with pulling rope 7, and the other end is connected with ship capsule inner wall.In hollow
The design in chamber can just accommodate the center-pole or connecting rod 22 of skeleton, can be airtight so that it goes without doing while structural strength is ensured
Property process.Certainly, the junction of skeleton and ship capsule 1 can also adopt conventional seals structure, set in the junction of skeleton and ship capsule 1
There is sealing structure.Dirigible bottom hung weight（Such as gondola）, the effect for pulling structure is to be distributed to the weight average of weight
On dirigible ship capsule surface and skeleton.
Further, the connecting rod 22 and the connected mode of center-pole are chain connection or bolt connection.
As shown in figure 4, in the present embodiment, the rear screw shaft device 3 includes driver 8, the connection spiral of the driver 8
Oar 9, the installing rack of the driver 8 is provided with mutually perpendicular horizontal stand 810 and vertical support frame 811, the horizontal stand
The horizontal rudder face 812 of connection is rotated on 810, the horizontal stand 810 is provided with the horizontal rudder face 812 of the driving of the first motor 814 and rotates, changes
Become dirigible luffing angle, the vertical rudder face 813 of connection is rotated on the vertical support frame 811, it is electric that the vertical support frame 811 is provided with second
Machine 815 drives vertical rudder face 813 to rotate, and changes dirigible direction of advance.The driver 8 is electromotor or motor.This enforcement
Example is preferred, and the skeleton includes three center-poles, and the first center-pole 211 is parallel to the second center-pole 212 and the 3rd center-pole
213 planes being located, the projection of the plane that the first center-pole 211 is located in the second center-pole 212 and the 3rd center-pole 213 is located at
Between second center-pole 212 and the 3rd center-pole 213, the first center-pole 211 and the second center-pole 212 and the 3rd center-pole 213
Connecting rod group is respectively equipped with front and back, and connecting rod group to be referred to and connect the second center-pole 212 and respectively in the somewhere of the first center-pole 211
Two connecting rods of three center-poles 213, in the present embodiment, anterior connecting rod group connects respectively for the front portion of the first center-pole 211
Two center-poles 212 and the connecting rod 222 of head rod 221 and second of the front portion of the 3rd center-pole 213, rear portion connecting rod group is the
The rear portion of one center-pole 211 connects respectively the 3rd connecting rod 223 and the 4th at the second center-pole 212 and the rear portion of the 3rd center-pole 213
Connecting rod 224, the connecting rod outside of anterior connecting rod group is provided with side propeller set 4.In the present embodiment, side propeller set 4
It is identical with the structure of rear screw shaft device 3 in the present embodiment.
Further, the skeleton also includes bracing piece 23, and the bracing piece 23 is vertically arranged.In the present embodiment, strengthen
Bar 23 has 3.The design of bracing piece 23 can further web frame structure, so as to strengthen the intensity of dirigible, and for
The length for increasing dirigible also functions to positive role.
Further, dirigible also includes gondola, and the gondola is located at dirigible bottom.
The principle of the present embodiment：By way of skeleton is set inside ship capsule 1, the structure of ship capsule 1 is strengthened, rigidity
Good, intensity is big, makes that dirigible size is unrestricted, solves the short technical problem of the low intensity of traditional blimp, hull, and
And simple structure, gently, what skeleton was primarily served is the effect for supporting whole ship capsule 1 to structure, does not limit it and specifically includes center
The quantity of bar, connecting rod 22 and bracing piece 23, the quantity of center-pole is related to the intensity of the width of dirigible and design requirement, even
The quantity of extension bar 22 is related to the intensity of the length of dirigible and design requirement, the quantity of bracing piece 23 and the size of dirigible and
The intensity of design requirement is related.
The dirigible of the present embodiment efficiently solves relatively low traditional blimp intensity, limited size, air pressure and maintains big, ship capsule
Affiliated facility affects the technical problem that ship capsule intensity causes ship capsule to deform, and has simple structure, rigid good, intensity greatly, to be flown
Ship size is limited and the light advantage of structure.
Above example is used only for explanation of the invention, and the present invention is not embodied as limiting by above-mentioned, every employing
The present invention the intracapsular mode that skeleton Os Draconis are set of ship design, such as dirigible of four body ship capsule structures as shown in fig. 13 that, no
By the rear screw shaft device or side propeller set that are equipped with which kind of structure, no matter it changes center-pole, connecting rod and bracing piece
Radical and position, all fall within the range of technical solution of the present invention protection.
Elaborate many details in order to fully understand the present invention in the above description.But above description is only
Presently preferred embodiments of the present invention, the present invention can be implemented with being much different from alternate manner described here, therefore this
Invention is not embodied as being limited by disclosed above.Simultaneously any those skilled in the art are without departing from the technology of the present invention
In the case of aspects, all make many possible to technical solution of the present invention using the methods and techniques content of the disclosure above
Change and modify, or the Equivalent embodiments for being revised as equivalent variations.Every content without departing from technical solution of the present invention, according to this
The technical spirit of invention still falls within skill of the present invention to any simple modification made for any of the above embodiments, equivalent variations and modification
In the range of the protection of art scheme.
Claims (10)
1. a kind of dirigible, it is characterised in that：Including skeleton and ship capsule, the skeleton is placed in the intracapsular support ship capsule of ship, the ship capsule
Both sides are provided with tailplane, and the ship capsule top is provided with vertical tail, and the tailplane and vertical tail are equipped with rudder face, institute
State rudder face and rotate with tailplane and be connected, the rudder face is rotated with vertical tail and is connected；The skeleton includes many center-poles, institute
State center-pole to arrange along dirigible kayak body direction, connected by connecting rod between the center-pole, after the center-pole afterbody is provided with
Propeller set, the rear screw shaft device is provided with driving means.
2. dirigible according to claim 1, it is characterised in that：The ship capsule is provided with hollow cavity, the center-pole and company
Extension bar is placed in the hollow cavity, and the center-pole and ship capsule inner wall are by pulling rope and drawing cloth connection, the pulling rope
One end is connected with center-pole, and the other end is connected with drawing cloth, and described drawing cloth one end is connected with pulling rope, and the other end is intracapsular with ship
Wall connects.
3. dirigible according to claim 1, it is characterised in that：The rear screw shaft device includes driver, the driving
Device connects propeller, and the installing rack of the driver is provided with mutually perpendicular horizontal stand and vertical support frame, the level
The horizontal rudder face of connection is rotated on frame, the horizontal stand is provided with the horizontal rudder face rotation of the first Motor drive, on the vertical support frame
The vertical rudder face of connection is rotated, the vertical support frame is provided with the vertical rudder face rotation of the second Motor drive.
4. dirigible according to claim 1, it is characterised in that：The rear screw shaft device include base, first support, the
Two supports, propeller and driver, the first support is connected with base rotation, and the base is provided with the 3rd Motor drive first
Support rotates, and the second support is rotated with first support and is connected, and the first support is provided with the 4th Motor drive second support
Rotation, the second support is provided with driver and propeller, the driver drives propeller rotation.
5. dirigible according to claim 1, it is characterised in that：The rear screw shaft device includes base and driver bottom
Seat, described actuator base one end is provided with driver and propeller, the driver drives propeller rotation, the other end and base
Connected by mutually perpendicular first rotating shaft and the second axis of rotation, the base and actuator base side by universal joint and
Flexible servomechanism connection, the base is fixedly connected with dirigible, and the actuator base can be realized around first rotating shaft left-right rotation
The steering of dirigible, the actuator base can rotate upwardly and downwardly the luffing angle for changing dirigible around the second rotating shaft.
6. dirigible according to claim 1, it is characterised in that：The skeleton include two parallel center-poles, it is described in
Connecting rod connection is respectively equipped with before and after between core bar, anterior connecting rod both sides are provided with side propeller set.
7. dirigible according to claim 1, it is characterised in that：The skeleton includes three center-poles, and three center-poles exist
Same plane, is respectively equipped with front and back connecting rod connection between center-pole, anterior connecting rod both sides are provided with side propeller set.
8. dirigible according to claim 1, it is characterised in that：The skeleton includes three center-poles, and the first center-pole is put down
The plane that row is located in the second center-pole and the 3rd center-pole, divides before and after the first center-pole and the second center-pole and the 3rd center-pole
Connecting rod group is not provided with, anterior connecting rod group both sides are provided with side propeller set.
9. dirigible according to claim 1, it is characterised in that：The skeleton includes three center-poles, before three center-poles
In sustained height, in differing heights, front portion is provided with connecting rod between the center-pole at rear portion, and rear portion is provided with connecting rod group in portion, anterior
Connecting rod both sides are provided with side propeller set.
10. the dirigible according to any one of claim 1-9, it is characterised in that：The skeleton also includes bracing piece, described to add
Strong bar is vertically arranged.
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| CN201610913828.5A CN106564580B (en) | 2016-10-19 | 2016-10-19 | A kind of dirigible |
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| CN201610913828.5A CN106564580B (en) | 2016-10-19 | 2016-10-19 | A kind of dirigible |
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| CN106564580B CN106564580B (en) | 2019-02-19 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110127023A (en) * | 2019-06-16 | 2019-08-16 | 郭屹 | A kind of dirigible with efficient balance |
| CN112046724A (en) * | 2020-09-09 | 2020-12-08 | 重庆交通大学 | Self-rotating rotor type airship |
| CN113086221A (en) * | 2021-04-07 | 2021-07-09 | 台州学院 | Soft unmanned aerial vehicle |
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| US20070267537A1 (en) * | 2006-05-18 | 2007-11-22 | Daniel Nachbar | Internal Support Structure for an Airship |
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| CN105000186A (en) * | 2015-07-09 | 2015-10-28 | 华南农业大学 | Anti-falling and anti-drifting unmanned aerial vehicle |
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| US5285986A (en) * | 1991-04-18 | 1994-02-15 | Luftschiffbau Zeppelin Gmbh | Rigid airship with a carrier frame of ribs and beams enclosed by skin sections forming an envelope |
| US20070267537A1 (en) * | 2006-05-18 | 2007-11-22 | Daniel Nachbar | Internal Support Structure for an Airship |
| EP2143610A2 (en) * | 2008-07-07 | 2010-01-13 | Lockheed Martin Corporation | Retracting Air Cushioned Landing System for Air Vehicles |
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| CN110127023A (en) * | 2019-06-16 | 2019-08-16 | 郭屹 | A kind of dirigible with efficient balance |
| CN112046724A (en) * | 2020-09-09 | 2020-12-08 | 重庆交通大学 | Self-rotating rotor type airship |
| CN113086221A (en) * | 2021-04-07 | 2021-07-09 | 台州学院 | Soft unmanned aerial vehicle |
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| Publication number | Publication date |
|---|---|
| CN106564580B (en) | 2019-02-19 |
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Effective date of registration: 20220104 Address after: 211100 floor 3, building 16, baijiahu science and Technology Industrial Park, No. 2, qingshuiting West Road, moling street, Jiangning District, Nanjing, Jiangsu Province Patentee after: NANJING ZUHANG AVIATION TECHNOLOGY Co.,Ltd. Address before: No. 37 General Avenue, Jiangning Economic and Technological Development Zone, Nanjing City, Jiangsu Province, 210000 Patentee before: NANJING DASSAULT AVIATION TECHNOLOGY Co.,Ltd. |
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Effective date of registration: 20231220 Address after: Room 402, Building 6, No. 137 Jinghuai Street, Moling Street, Jiangning District, Nanjing City, Jiangsu Province, 211100 Patentee after: Yang Siqiang Address before: 211100 floor 3, building 16, baijiahu science and Technology Industrial Park, No. 2, qingshuiting West Road, moling street, Jiangning District, Nanjing, Jiangsu Province Patentee before: NANJING ZUHANG AVIATION TECHNOLOGY Co.,Ltd. |
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