CN106240785A - The method of the stratospheric airship stable state lifting of auxiliary liter of balloon belt expanded letter adjustable wing - Google Patents
The method of the stratospheric airship stable state lifting of auxiliary liter of balloon belt expanded letter adjustable wing Download PDFInfo
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- CN106240785A CN106240785A CN201610713068.3A CN201610713068A CN106240785A CN 106240785 A CN106240785 A CN 106240785A CN 201610713068 A CN201610713068 A CN 201610713068A CN 106240785 A CN106240785 A CN 106240785A
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- dirigible
- balloonet
- wing
- balloon
- folding boat
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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
- B64B1/20—Rigid airships; Semi-rigid airships provided with wings or stabilising surfaces
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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
- B64B1/24—Arrangement of propulsion plant
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
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- Aviation & Aerospace Engineering (AREA)
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Abstract
nullThe method of the stratospheric airship stable state lifting of auxiliary liter of balloon belt expanded letter adjustable wing，Dirigible width hull top is equipped with device of solar generating，The folding boat wing is arranged on the both sides of wide hull，The folding boat wing is framing structure，And top is installed with the solaode of device of solar generating，Folding boat wing energy folding shrinking or tiling launch，Vector propeller is symmetrically installed on both sides and the rear portion of wide hull of wide hull，Pressure system completes inflation or the deflation operations of wide hull，Device of solar generating is vector propeller、Pressure system、The folding boat wing and flight control system are powered，Flight control system respectively with device of solar generating、Vector propeller、The folding boat wing and pressure system electrical connection，Solaode is laid on the ship wing，Increase and lay area，Luminous energy is changed into enough electrical energy drive vector propellers，Make dirigible power pure，The pitch angle of dirigible can be controlled simultaneously，Ensure that dirigible maintains certain altitude cruise，Controllability and power all significantly improve.
Description
Technical field
The present invention relates to dirigible field, particularly relate to stratospheric airship field.
Background technology
At the beginning of 21 century, stratospheric airship enjoys the concern of each big country, it was predicted that application spreads all over army civilian, police, quasi-
With, military etc.；At present, stratospheric airship is applied to the civil areas such as ocean research, rescue and relief work, urban traffic control more.
Stratospheric airship is a kind of aerostatics being lighter than air, relies on aerostatic buoyancy to stay sky, can be with long-term suspension in advection
Floor height is empty, solar energy provide energy source and power for it, and with propulsion system, has and is independent of airport or runway can realize vertically
Landing, can hover in overhead, arbitrary geographic position, run height beyond blank pipe scope, not by troposphere adverse weather conditions, can
All-weather round-the-clock works continuously, and except needs ground control and data accept treatment facility, with little need for other ground
Face infrastructure is supported, various aspects have impayable advantage.
But current stratospheric airship technology is not the most the most ripe, and mostly blimp shape is drop-shaped list kayak body, causes too
Sun can lay limited area by TRT, adds that luminous energy transfer power is limited, thus limits the power of dirigible, and dirigible power is not
In the case of foot, dirigible wind loading rating is the most weak, and the most controlled ability of whole dirigible or bearing capacity are the most extremely limited, but
If the simple upper surface area only considering to increase dirigible, the resistance that excessive dirigible is subject to is the biggest, and maneuverability reduces, and controls
Get up inconvenience, be not the most practical.
On the other hand, existing stratospheric airship regulation altitude capability is limited, and usually then waft during helium temperature difference height between daytime liter
To about 30000 meters, then it is down to 18000 meters ~ 20000 meters when night, the helium temperature difference was low, even drops to troposphere, run into high wind
Being blown off, dirigible is had no idea to control flight attitude and is also had no idea to control cruising altitude, and controllability is the poorest, easily causes fatal
Damage.
The takeoff method also having current stratospheric airship uses unstable state elevating method, when taking off, does not inflate
Dirigible is moving upward to stratosphere just expansion molding, and the drawback of this method is a lot, is on the one hand raised to stratosphere and just launches
Dirigible can not well ensure that solaode, in the smooth laying in dirigible back, is on the other hand that this takeoff method makes dirigible
Through tropospheric time, if the most all can not safety arrive flat through troposphere when of running into high wind band or strong wind
Fluid layer.Many employings type self-destroyed method the fallen during landing of current stratospheric airship, it is simply that air bag priming system is burst by dirigible,
Type self-destroyed whereabouts, is on the one hand that pick-up point scope is big especially, and completely random, greatly reduces dirigible recovery utilization rate, separately
On the one hand being this dropping method well damage for instrument and equipment, cost is the highest.
Summary of the invention
For the deficiencies in the prior art, the technical problem to be solved is to provide the advection of a kind of expanded letter adjustable wing
Layer dirigible, dirigible, with the berthon boat wing, the ship wing is laid solaode, is considerably increased the laying of device of solar generating
Area, changes into enough electrical energy drive vector propellers so that dirigible power is pure by luminous energy, and flight is got up controllability and holds
Loading capability is obviously improved.
The technical solution adopted for the present invention to solve the technical problems is:
The stratospheric airship of expanded letter adjustable wing, including wide hull, device of solar generating, vector propeller, the folding boat wing, pressure
System and flight control system；Wide hull top is laid and is provided with device of solar generating, and the folding boat wing is arranged on the both sides of wide hull,
The folding boat wing is framing structure, and top is installed with the solaode of device of solar generating, and the folding boat wing can fold
Shrinking or tiling launches, vector propeller is symmetrically installed on both sides and the rear portion of wide hull of wide hull, and pressure system is complete
Becoming inflation or the deflation operations of wide hull, device of solar generating is vector propeller, pressure system, the folding boat wing and flies control
System power supply, flight control system electrically connects with device of solar generating, vector propeller, the folding boat wing and pressure system respectively, and
Control device of solar generating, vector propeller, the folding boat wing and pressure system work respectively.
Optimum, this dirigible also includes aileron, empennage, rudder face and auxiliary liter of balloon apparatus, after aileron is arranged at the folding boat wing
Portion, and aileron can be relative to folding boat wing regulation angle, empennage includes the double tailplanes being arranged at dirigible two sides of tail and sets
Being placed in double vertical tails on the top of dirigible afterbody, rudder face is arranged at empennage rear portion, and rudder face can regulate angle relative to empennage；
Auxiliary liter of balloon apparatus includes auxiliary liter of balloon, pull rope and snap close, and described snap close is fixedly mounted on dirigible top, and snap close with fly control
System electrically connects, i.e. snap close is controlled locking by flight control system or opens, and auxiliary liter of balloon is fixed on snap close by pull rope, lock
Padlock auxiliary liter of balloon of timing links together with dirigible, and when snap close is opened, auxiliary liter of balloon separates with dirigible.
Optimum, described wide hull is to be formed by three single utricule connected combinations, the length of wide hull and the ratio of width
It is 2.1～2.5:1；One single utricule is positioned at centre, and two single utricules are positioned at both sides, and the head of single utricule of centre protrudes from
The head of single utricule of both sides；Middle single utricule horizontal level is higher than single utricule of both sides, and i.e. three single utricules are in centre
Single utricule bottom surrounds a gondola space；Described pressure system includes aerator and venting valve, aerator and venting valve
Being installed on single utricule, aerator is for inflating in single utricule, and venting valve is for the venting of single utricule；Described single utricule
Including main gasbag and be arranged on the balloonet within main gasbag, described balloonet is divided into front balloonet and rear balloonet, main gasbag,
Front balloonet and rear balloonet have pressure system to complete inflation or deflation operations respectively, fill helium, in balloonet in main gasbag
Filling air, the total measurement (volume) of balloonet accounts for the 93% of whole wide hull volume, and the total measurement (volume) of main gasbag accounts for whole wide hull volume
7%。
Optimum, this dirigible also includes that Landing Buffer device and ship carry equipment protecting equipment, under two single utricules of both sides
Portion is respectively provided with and is provided with Landing Buffer device, and described Landing Buffer device just activates to open when dirigible lands；Ship carries equipment
Protection device dirigible is overweight be difficult to normal flight time, ship is carried equipment and launches away, and open and be fixed on ship load equipment
Parachute, protection ship carries equipment safe landing；The both sides of described dirigible are installed with three vector propellers, and dirigible respectively
Rear portion be installed with two vector propellers, vector propeller uses carbon fiber skeletal support, and inside suspension screen hangs load
It is arranged on dirigible；Described device of solar generating uses thin film or non-crystal silicon solar cell, on the downside of solaode edge
The installation settings folding boat wing at two meters；The framing structure of the described folding boat wing is by carbon fiber, titanium-aluminium alloy or Nitinol material
Material is made, and during ground, uphill process, decline or the when of not having a sun, the folding boat wing is all in folding shrinking shape
State, when being in stratosphere the tiling of the folding boat wing launch, and the expansion of also tiling of the solaode on its top start working.
For the deficiencies in the prior art, the present invention also provides for the stratospheric airship of above-mentioned expanded letter adjustable wing and keeps cruising altitude
Method, dirigible can from main modulation pitch attitude, simultaneously can Autonomous Control height, meet various flight requirement so that dirigible is pacified
The most controlled.
When above-mentioned dirigible is less than cruising altitude, at least one mode in following three kinds of modes is selected to make dirigible return to patrol
Flying height degree:
The first rising manner: the aileron controlling dirigible is adjusted up angle relative to the ship wing, increases the elevation angle of aileron, controls dirigible
Rudder face be adjusted up angle relative to tailplane, increase the elevation angle of rudder face, the vector propeller controlling dirigible provides power,
Dirigible is made to return to cruising altitude；
The second rising manner: control rear balloonet and/or the pressure system of front balloonet of dirigible, makes dirigible keep the elevation angle,
The vector propeller controlling dirigible provides power, makes dirigible return to cruising altitude；
The third rising manner: control the vector propeller of dirigible, make dirigible return to cruising altitude.
Optimum, the concrete grammar making the dirigible holding elevation angle in described the second rising manner is following at least one:
Control the rear balloonet inflation of dirigible and control front balloonet venting simultaneously, making dirigible keep the elevation angle；
Control the air capacity in the rear balloonet of dirigible more than the air capacity in front balloonet, the air quality in i.e. rear balloonet
More than the air quality in front balloonet, dirigible is made to keep the elevation angle；
The concrete grammar of the third rising manner described is following at least one:
The vector propeller controlling dirigible both sides is opened and upwards 30 ~ 90 degree, provides pulling force upwards for dirigible, makes dirigible return to
Cruising altitude；
The vector propeller controlling dirigible rear portion is opened and downward 30 ~ 90 degree, provides thrust upwards for dirigible, makes dirigible return to
Cruising altitude.
When above-mentioned dirigible is higher than cruising altitude, at least one mode in following three kinds of modes is selected to make dirigible return to patrol
Flying height degree:
The first declines mode: control the aileron of dirigible relative to regulation angle under ship flapwise, the angle of depression of increase aileron, control dirigible
Rudder face regulate downwards angle relative to tailplane, increase the angle of depression of rudder face, the vector propeller controlling dirigible provides power,
Dirigible is made to return to cruising altitude；
The second declines mode: control rear balloonet and/or the pressure system of front balloonet of dirigible, makes dirigible keep the angle of depression,
The vector propeller controlling dirigible provides power, makes dirigible return to cruising altitude；
The third declines mode: controls the vector propeller of dirigible, makes dirigible return to cruising altitude.
Optimum, the concrete grammar making the dirigible holding angle of depression in described the second decline mode is following at least one:
Control the rear balloonet venting of dirigible and control front balloonet inflation simultaneously, making dirigible keep the angle of depression；
Control the air capacity in the rear balloonet of dirigible less than the air capacity in front balloonet, the air quality in i.e. rear balloonet
Less than the air quality in front balloonet, dirigible is made to keep the angle of depression；
The third concrete grammar declining mode described is following at least one:
The vector propeller controlling dirigible both sides is opened and downward 30 ~ 90 degree, provides downward pulling force for dirigible, makes dirigible return to
Cruising altitude；
The vector propeller controlling dirigible rear portion is opened and upwards 30 ~ 90 degree, provides downward thrust for dirigible, makes dirigible return to
Cruising altitude.
For the deficiencies in the prior art, the technical problem to be solved is to provide the advection of a kind of expanded letter adjustable wing
The stable state elevating method of layer dirigible, dirigible is just to take off after molding, and deadweight and vector propeller that dirigible is heavier make dirigible steady
State rises, and steadily arrives stratosphere through troposphere, on the other hand falls also without after venting emptying when of dirigible landing,
But vector propeller controls speed while declining by deadweight, land in predetermined smaller range, whole lifting process
The most controlled.
Above-mentioned dirigible climb procedure comprises the following steps:
Dirigible molding: by the hull gassy of dirigible, then installs device of solar generating, vector propeller and flies control system
System, i.e. dirigible molding；
Letting dirigible fly away: let fly away by the dirigible of molding, dirigible rises to stratosphere by natural buoyancy；The folding boat span is opened: arrive
Stratosphere and after having had sunlight, the tiling of the folding boat wing launches, and the expansion of also tiling of the solaode on its top is started working.
Optimum, the dirigible of letting fly away in this dirigible climb procedure specifically includes following steps:
Fixing auxiliary liter of balloon: snap close is fixed on the dirigible top of molding, and snap close locks the pull rope being fixed with auxiliary liter of balloon, auxiliary
Being flushed with hydrogen gas or helium in rising balloon, let fly away by the dirigible being hung with auxiliary liter of balloon, dirigible is by self and the buoyancy of auxiliary liter of balloon
Rise to stratosphere；
Discharging auxiliary liter of balloon: after dirigible arrives at stratosphere, flight control system controls snap close and opens, and is separated with dirigible by auxiliary liter of balloon.
Optimum, described dirigible climbing is 5～7 meter per seconds；The air bag of described dirigible is divided into main gasbag and balloonet, its
Fill in middle main gasbag is helium, and fill in balloonet is air, and helium accounts for the 7% of total aeration quantity, and air accounts for total aeration quantity
93%；In described dirigible forming process, after balloonet is full of air, balloonet pressure is 200～400 handkerchiefs, and main gasbag is full of helium
Rear main gasbag pressure is normally 300～400 handkerchiefs, maximum less than 600 handkerchiefs.
Above-mentioned dirigible descending method comprises the following steps:
The folding boat wing is packed up: flight control system controls folding boat wingfold and shrinks；
Dirigible keeps shape: dirigible helium in external world's extraction air fills dirigible shrinks the space produced, and keeps blimp shape
When rising with dirigible consistent；
Dirigible declines: dirigible declines by gravity；
Dirigible lands: when dirigible drops to more than 1200 meters of ground of distance, start the motor of dirigible, control dirigible angle and under
Fall rate, controls dirigible and lands.
Optimum, described dirigible rate of descent is less than or equal to 5 meter per seconds；What described dirigible landed comprises the concrete steps that, described
When dirigible drops to distance ground more than 1200 rice, start the motor of dirigible, control dirigible and keep-2～0 degree of angles of depression, and
The rate of descent of dirigible is adjusted to 3 meter per seconds；When described dirigible drops to 300 meters of ground of distance, control dirigible and keep 0～+2 degree
The elevation angle, uses the motor of dirigible, adjusts the rate of descent of dirigible to 1 meter per second；When dirigible drops to 50 meters of ground of distance, put
Lower mooring cable；Described dirigible drop to distance 10 meters of ground time, use dirigible motor, the rate of descent of dirigible is adjusted to
0.5 meter per second, motor vector controlled and rudder face are handled dirigible and are landed windward with the holding of 3 ~ 5 degree of the elevation angle；When described dirigible declines,
If overweight state, when dirigible drops to 3000 meters of ground of distance, flight control system controls ship and carries equipment protecting equipment by ship
Load equipment launches away, and opens the parachute being fixed on ship load equipment, and protection ship carries equipment safe landing；In dirigible distance
During about 50 meters of ground, Landing Buffer device starts automatically.
As shown from the above technical solution, the stratospheric airship of the expanded letter adjustable wing that the present invention provides, with the folding boat wing, fly
Ship rise to the stratosphere sun out time the folding boat wing open, the ship wing is equipped with solar panels, considerably increases solar electrical energy generation
The laying area of device, changes into enough electrical energy drive vector propellers so that dirigible power is pure, utilizes simultaneously by luminous energy
The inflation of tail structure, balloonet or the structure such as venting and vector propeller can ensure that and can keep certain angle of pitch at dirigible
Flight, thus keeps a certain predetermined altitude cruise, and safely controllable property is greatly promoted, fly controllability and bearing capacity notable
Promote.
Accompanying drawing explanation
Accompanying drawing 1 is the structural representation of the stratospheric airship of expanded letter adjustable wing.
Accompanying drawing 2 is the top view of the stratospheric airship of expanded letter adjustable wing.
Accompanying drawing 3 is the right view of the stratospheric airship of expanded letter adjustable wing.
Accompanying drawing 4 is the front view of the stratospheric airship of expanded letter adjustable wing.
Accompanying drawing 5 is the stratospheric airship of auxiliary liter of balloon belt expanded letter adjustable wing structural representation when letting fly away.
Accompanying drawing 6 is the structural representation in the stratospheric airship uphill process of auxiliary liter of balloon belt expanded letter adjustable wing.
Accompanying drawing 7 is the structural representation after the stratospheric airship of auxiliary liter of balloon belt expanded letter adjustable wing arrives at stratosphere.
In figure: single utricule 1, main gasbag 2, front balloonet 3, rear balloonet 4, the folding boat wing 5, aileron 6, empennage 7, rudder face 8,
Vector propeller 9, device of solar generating 10, Landing Buffer device 11, auxiliary liter of balloon 12, pull rope 13, snap close 14.
Specific implementation method
In conjunction with the accompanying drawing of the present invention, the technical scheme of inventive embodiments is further elaborated.
Referring to the drawings shown in 1, the stratospheric airship of expanded letter adjustable wing includes wide hull, device of solar generating 10, vector
Propeller 9, pressure system, flight control system, the folding boat wing 5, aileron 6, empennage 7, rudder face 8, Landing Buffer device 11, ship carry equipment
Protection device and auxiliary liter of balloon apparatus.
The folding boat wing 5 is arranged on the both sides of wide hull, and the folding boat wing 5 is framing structure, and top is installed with the sun
The solaode of energy TRT (10), the folding boat wing 5 energy folding shrinking or tiling expansion, the skeleton knot of the folding boat wing 5
Structure is made up of carbon fiber, titanium-aluminium alloy or nickel-titanium alloy material, during ground, uphill process, decline or less than the most too
The when of sun, the folding boat wing 5 is all in folding shrinking state, and when being in stratosphere, the folding boat wing 5 tiling launches, and its top
Solaode expansion of also tiling start working.The folding boat wing 5 considerably increases the area of the solaode of dirigible, the most just
It is the increase in the power of vector propeller 9, increases the controllability of dirigible.
Dirigible also includes the folding boat wing 5, aileron 6, empennage 7 and rudder face 8, and on the downside of solaode edge, at two meters, installation sets
Putting the folding boat wing 5, two folding boat wings 5 are respectively arranged at the both sides in the middle part of dirigible, and aileron 6 is arranged at the folding boat wing 5 rear portion, and
Aileron 6 can regulate angle relative to the folding boat wing 5, and empennage 7 includes double tailplanes and the setting being arranged at dirigible two sides of tail
In double vertical tails on the top of dirigible afterbody, rudder face 8 is arranged at empennage 7 rear portion, and rudder face 8 can regulate angle relative to empennage 7
Degree.
Referring to the drawings shown in 5, auxiliary liter of balloon apparatus includes auxiliary liter of balloon 12, pull rope 13 and snap close 14, described snap close 14
Be fixedly mounted on dirigible top, and snap close 14 electrically connects with flight control system, i.e. snap close 14 is controlled locking by flight control system or opens
Opening, auxiliary liter of balloon 12 is fixed on snap close 14 by pull rope 13, snap close 14 when locking auxiliary liter of balloon 12 be connected to one with dirigible
Rise, snap close 14 when opening auxiliary liter of balloon 12 separate with dirigible.
Referring to the drawings shown in 4, wide hull is to be formed by three the same single utricule 1 connected combinations, wide hull length 186 meters,
Wide 86 meters, high 52 meters, the length of wide hull and the ratio of width are 2.1～2.5:1, single utricule 1 long 168 meters, maximum gauge 42
Rice；One single utricule 1 is positioned at centre, and two single utricules 1 are positioned at both sides, and the head of single utricule 1 of centre protrudes from both sides
The head of single utricule 1；Middle single utricule 1 horizontal level is higher than single utricule 1 of both sides, and i.e. three single utricules 1 are at middle list
Utricule 1 bottom surrounds a gondola space, and this gondola space can be placed ship and be carried equipment, ship load equipment.
Referring to the drawings shown in 2, pressure system includes that aerator and venting valve, aerator and venting valve are installed in list
On utricule, aerator is for inflating in single utricule, and venting valve is for the venting of single utricule；Single utricule 1 includes main gasbag 2 He
Being arranged on the balloonet within main gasbag 2, described balloonet is divided into front balloonet 3 and rear balloonet 4, main gasbag 2, front balloonet
3 and rear balloonet 4 respectively by pressure system complete inflation or deflation operations, aerator and venting valve paired be arranged on master
On air bag 2, front balloonet 3 and rear balloonet 4, aerator is used for inflating, and venting valve is used for exitting, and fills helium in main gasbag 2,
Filling air, main gasbag 2 cumulative volume 309,960 cubic metres in balloonet, balloonet total measurement (volume) is 21,697 cubic metres, main gasbag 2
Surface area 29,358 square metres, balloonet surface area 27,000 square metre, sea level net lift 22,023 kilogram, balloonet total
Volume accounts for the 93% of whole wide hull volume, and the total measurement (volume) of main gasbag 2 accounts for the 7% of whole wide hull volume.
The device of solar generating 10 installing at least 5,600 square metres can be laid in wide hull top, can on the folding boat wing 5
To lay the device of solar generating 10 installing at least 1,000 square metre, device of solar generating 10 uses thin film or non-crystalline silicon
Solaode, the area coverage of solaode is about 2-3 times of water-drop-shaped list ship capsule.
Referring to the drawings shown in 3, vector propeller 9 is symmetrically installed on both sides and the rear portion of wide hull, the dirigible of wide hull
Both sides be installed with three vector propellers 9 respectively, and the rear portion of dirigible is installed with two vector propellers 9, one
Eight vector propellers 9 installed altogether can provide 1, and the power of 020KW, vector propeller 9 uses carbon fiber skeletal support, interior
Portion's suspension screen hangs load and is arranged on dirigible；Pressure system completes inflation or the deflation operations of wide hull, and solar electrical energy generation fills
To put 10 be vector propeller 9, pressure system and flight control system are powered, flight control system respectively with device of solar generating 10, vector
Propeller 9, the folding boat wing 5 and pressure system electrical connection, and control device of solar generating 10, vector propeller 9 respectively, fold
The ship wing 5 and pressure system work.
Two single utricule 1 bottoms of both sides are respectively provided with and are provided with Landing Buffer device 11, and described buffer unit is at dirigible
Just activate to open during landing；Ship carry equipment protecting equipment dirigible is overweight be difficult to normal flight time, ship is carried equipment and launches away,
And open the parachute being fixed on ship load equipment, protection ship carries equipment safe landing.
The stable state climb procedure of the stratospheric airship that the present invention also provides for a kind of auxiliary liter of balloon belt expanded letter adjustable wing include with
Lower step:
Dirigible molding: by the hull gassy of dirigible, the air bag of dirigible is divided into main gasbag 2 and balloonet, wherein in main gasbag 2
Fill is helium, and fill in balloonet is air, and helium accounts for the 7% of total aeration quantity, and air accounts for the 93% of total aeration quantity；Described dirigible
In forming process, after balloonet is full of air, balloonet pressure is 200～400 handkerchiefs, and after main gasbag 2 is full of helium, main gasbag 2 is pressed
Power is less than 600 handkerchiefs, then installs device of solar generating 10, vector propeller 9 and flight control system, i.e. dirigible molding.
Referring to the drawings shown in 5, fixing balloon: snap close 14 is fixed on the dirigible top of molding, and snap close 14 locking is fixed with
The pull rope 13 of auxiliary liter of balloon 12, is flushed with hydrogen gas or helium in auxiliary liter of balloon 12, is let fly away by the dirigible being fixed with auxiliary liter of balloon 12, ginseng
According to shown in accompanying drawing 6, dirigible rises to stratosphere by the buoyancy of self and auxiliary liter of balloon 12, and climbing controls at 5～7 meter per seconds,
After arrival stratosphere has had the sun, the folding boat wing (5) tiling launches, and the solaode on its top also tiles and launches to start work
Make.
Referring to the drawings shown in 7, discharging auxiliary liter of balloon 12: after dirigible arrives at stratosphere, flight control system controls snap close 14 and opens,
Auxiliary liter of balloon 12 is separated with dirigible.
The folding boat span is opened: after arriving stratosphere and having had sunlight, and flight control system controls the folding boat wing 5 tiling and launches, and
The expansion of tiling the most therewith of the solaode on its top is started working.
The stable state descending method of the stratospheric airship that the present invention also provides for a kind of auxiliary liter of balloon belt expanded letter adjustable wing include with
Lower step:
The folding boat wing is packed up: flight control system controls the folding boat wing 5 folding shrinking；
Dirigible keeps shape: dirigible is filled dirigible endogenous cause of ill helium from external world's extraction air and shunk the space produced, and keeps dirigible shape
Shape is consistent when rising with dirigible；
Dirigible declines: be typically selected in dusk and night, and dirigible declines by gravity；Rate of descent control less than or equal to 5 meters/
Second；If decrease speed is too fast until overweight state, when dirigible drops to 3000 meters of ground of distance, flight control system controls ship and carries
Ship is carried equipment and launches away by equipment protecting equipment, and opens the parachute being fixed on ship load equipment, and protection ship carries equipment peace
Full landing；
Dirigible lands: when dirigible drops to more than 1200 meters of ground of distance, start the motor of dirigible, control dirigible keep-2～
0 degree of angle of depression, and the rate of descent of dirigible is adjusted to 3 meter per seconds；When described dirigible drops to 300 meters of ground of distance, control dirigible
Keep 0～+2 degree elevations angle, use the motor of dirigible, the rate of descent of dirigible is adjusted to 1 meter per second；Dirigible drops to distance ground
During 50 meters of face, put down mooring cable；When described dirigible drops to 10 meters of ground of distance, use the motor of dirigible, by under dirigible
Fall rate adjusts to 0.5 meter per second, and motor vector controlled and rudder face are handled dirigible and landed windward, at dirigible with the holding of 3 ~ 5 degree of the elevation angle
During about 50 meters of ground of distance, Landing Buffer device 11 starts automatically.
The present invention also provide for a kind of expanded letter adjustable wing stratospheric airship keep cruising altitude method:
When the stratospheric airship of above-mentioned expanded letter adjustable wing is less than cruising altitude, select at least one side in following three kinds of modes
Formula makes dirigible return to cruising altitude:
The first rising manner: the aileron 6 ship folded against wing 5 controlling dirigible is adjusted up angle, increases the elevation angle of aileron 6,
The rudder face 8 controlling dirigible is adjusted up angle relative to tailplane 7, increases the elevation angle of rudder face 8, and the vector controlling dirigible advances
Device 9 provides power, makes dirigible return to cruising altitude；
The second rising manner: control rear balloonet 4 and/or the pressure system of front balloonet 3 of dirigible, makes dirigible keep facing upward
Angle, the vector propeller 9 controlling dirigible provides power, makes dirigible return to cruising altitude；It can be specifically the rear pair controlling dirigible
Before air bag 4 inflation simultaneously control, balloonet 3 is exitted, and makes dirigible keep the elevation angle；Or control the sky in the rear balloonet 4 of dirigible
Tolerance is more than the air quality in front balloonet 3 more than the air capacity in front balloonet 3, the air quality in i.e. rear balloonet 4,
Dirigible is made to keep the elevation angle.
The third rising manner: control the vector propeller 9 of dirigible, make dirigible return to cruising altitude；Specifically control to fly
The vector propeller 9 of ship both sides is opened and upwards 30 ~ 90 degree, provides pulling force upwards for dirigible, makes dirigible return to cruising altitude；
Or the vector propeller 9 controlling dirigible rear portion is opened and downward 30 ~ 90 degree, provide thrust upwards for dirigible, make dirigible return
To cruising altitude.
When the stratospheric airship of above-mentioned expanded letter adjustable wing is higher than cruising altitude, select at least in following three kinds of modes
Kind of mode makes dirigible return to cruising altitude:
The first declines mode: the aileron 6 ship folded against wing 5 controlling dirigible regulates downwards angle, increases the angle of depression of aileron 6,
The rudder face 8 controlling dirigible regulates downwards angle relative to tailplane 7, increases the angle of depression of rudder face 8, and the vector controlling dirigible advances
Device 9 provides power, makes dirigible return to cruising altitude；
The second declines mode: control rear balloonet 4 and/or the pressure system of front balloonet 3 of dirigible, makes dirigible keep bowing
Angle, the vector propeller 9 controlling dirigible provides power, makes dirigible return to cruising altitude；Specifically control the rear balloonet 4 of dirigible
Before venting simultaneously control, balloonet 3 is inflated, and makes dirigible keep the angle of depression；Or control the air capacity in the rear balloonet 4 of dirigible
Less than the air capacity in front balloonet 3, the air quality in i.e. rear balloonet 4, less than the air quality in front balloonet 3, makes to fly
Ship keeps the angle of depression；
The third declines mode: controls the vector propeller 9 of dirigible, makes dirigible return to cruising altitude；Specifically control dirigible two
The vector propeller 9 of side is opened and downward 30 ~ 90 degree, provides downward pulling force for dirigible, makes dirigible return to cruising altitude；Or
The vector propeller 9 controlling dirigible rear portion is opened and upwards 30 ~ 90 degree, provides downward thrust for dirigible, makes dirigible return to patrol
Flying height degree.
Claims (10)
1. the stratospheric airship of expanded letter adjustable wing, it is characterised in that: this dirigible include wide hull, device of solar generating (10),
Vector propeller (9), the folding boat wing (5), pressure system and flight control system；Wide hull top is laid and is provided with solar electrical energy generation dress
Putting (10), the folding boat wing (5) is arranged on the both sides of wide hull, and the folding boat wing (5) is framing structure, and top is installed with too
The solaode of sun energy TRT (10), the folding boat wing (5) can folding shrinking or tiling expansion, vector propeller (9)
Being symmetrically installed on both sides and the rear portion of wide hull of wide hull, pressure system completes inflation or the deflation operations of wide hull,
Device of solar generating (10) is that vector propeller (9), pressure system, the folding boat wing (5) and flight control system are powered, flight control system
Electrically connect with device of solar generating (10), vector propeller (9), the folding boat wing (5) and pressure system respectively, and control respectively
Device of solar generating (10), vector propeller (9), the folding boat wing (5) and pressure system work.
The stratospheric airship of expanded letter adjustable wing the most according to claim 1, it is characterised in that: this dirigible also includes aileron
(6), empennage (7), rudder face (8) and auxiliary liter of balloon apparatus, aileron (6) is arranged at the folding boat wing (5) rear portion, and aileron (6) can phase
Regulating angle for the folding boat wing (5), empennage (7) includes the double tailplanes being arranged at dirigible two sides of tail and is arranged at dirigible
Double vertical tails on the top of afterbody, rudder face (8) is arranged at empennage (7) rear portion, and rudder face (8) can regulate relative to empennage (7)
Angle；Auxiliary liter of balloon apparatus includes auxiliary liter of balloon (12), pull rope (13) and snap close (14), and described snap close (14) is fixedly mounted on
Dirigible top, and snap close (14) electrically connects with flight control system, i.e. snap close (14) is controlled locking by flight control system or opens, auxiliary liter
Balloon (12) is fixed on snap close (14) by pull rope (13), and during snap close (14) locking, auxiliary liter of balloon (12) is connected to dirigible
Together, when snap close (14) is opened, auxiliary liter of balloon (12) separates with dirigible.
The stratospheric airship of expanded letter adjustable wing the most according to claim 2, it is characterised in that: described wide hull is by three
Single utricule (1) connected combination forms, and the length of wide hull and the ratio of width are 2.1～2.5:1；One single utricule (1) is positioned at
Centre, two single utricules (1) are positioned at both sides, and the head of single utricule (1) of centre protrudes from the head of single utricule (1) of both sides
Portion；Middle single utricule (1) horizontal level is higher than single utricule (1) of both sides, and i.e. three single utricules (1) are at middle single utricule
(1) bottom surrounds a gondola space；Described pressure system includes that aerator and venting valve, aerator and venting valve are all pacified
Being contained on single utricule, aerator is for inflating in single utricule, and venting valve is for the venting of single utricule；Described single utricule (1)
Including main gasbag (2) be arranged on the balloonet that main gasbag (2) is internal, described balloonet is divided into front balloonet (3) and rear pair gas
Capsule (4), main gasbag (2), front balloonet (3) and rear balloonet (4) have pressure system to complete inflation or deflation operations respectively, main
Air bag fills helium in (2), fills air in balloonet, and the total measurement (volume) of balloonet accounts for the 93% of whole wide hull volume, main gasbag (2)
Total measurement (volume) account for the 7% of whole wide hull volume.
The stratospheric airship of expanded letter adjustable wing the most according to claim 3, it is characterised in that: this dirigible also includes landing delaying
Flushing device (11) and ship carry equipment protecting equipment, and two single utricule (1) bottoms of both sides are respectively provided with and are provided with Landing Buffer dress
Putting (11), described Landing Buffer device just activates to open when dirigible lands；Ship carries equipment protecting equipment to be difficult to dirigible is overweight
During normal flight, ship being carried equipment and launches away, and open the parachute being fixed on ship load equipment, protection ship carries equipment safety
Land；The both sides of described dirigible are installed with three vector propellers (9) respectively, and the rear portion of dirigible is installed with two
Vector propeller (9), vector propeller (9) uses carbon fiber skeletal support, and inside suspension screen hangs load and is arranged on dirigible；Institute
Stating device of solar generating (10) and use thin film or non-crystal silicon solar cell, on the downside of solaode edge, at two meters, installation sets
Put the folding boat wing (5)；The framing structure of the described folding boat wing (5) is made up of carbon fiber, titanium-aluminium alloy or nickel-titanium alloy material,
During ground, uphill process, decline or the when of not having a sun, the folding boat wing (5) is all in folding shrinking state,
When being in stratosphere, the folding boat wing (5) tiling launches, and the expansion of also tiling of the solaode on its top is started working.
The stable state climb procedure of the stratospheric airship of the most auxiliary liter of balloon belt expanded letter adjustable wing, it is characterised in that: described dirigible is power
Profit requires the stratospheric airship of the expanded letter adjustable wing in 1～4 described in any one, and this dirigible climb procedure comprises the following steps:
Dirigible molding: by the hull gassy of dirigible, then install device of solar generating (10), vector propeller (9) and
Flight control system, i.e. dirigible molding；
Letting dirigible fly away: let fly away by the dirigible of molding, dirigible rises to stratosphere by natural buoyancy；
The folding boat span is opened: after arriving stratosphere, and flight control system controls the folding boat wing (5) tiling and launches, and the sun on its top
Can battery expansion of also tiling start working.
The stable state climb procedure of the stratospheric airship of auxiliary liter of balloon belt expanded letter adjustable wing the most according to claim 5, it is special
Levy and be:
Dirigible of letting fly away in this dirigible climb procedure specifically includes following steps:
Fixing auxiliary liter of balloon (12): snap close (14) is fixed on the dirigible top of molding, and snap close (14) locking is fixed with auxiliary liter of gas
The pull rope (13) of ball (12), is flushed with hydrogen gas or helium in auxiliary liter of balloon (12), is put by the dirigible being fixed with auxiliary liter of balloon (12)
Flying, dirigible rises to stratosphere by the buoyancy of self and auxiliary liter of balloon (12)；
Discharging auxiliary liter of balloon (12): after dirigible arrives at stratosphere, flight control system controls snap close (14) and opens, by auxiliary liter of balloon (12)
Separate with dirigible.
The stable state climb procedure of the stratospheric airship of auxiliary liter of balloon belt expanded letter adjustable wing the most according to claim 6, it is special
Levy and be: described dirigible climbing is 5～7 meter per seconds；The air bag of described dirigible is divided into main gasbag (2) and balloonet, the most main gas
Fill in capsule (2) is helium, and fill in balloonet is air, and helium accounts for the 7% of total aeration quantity, and air accounts for the 93% of total aeration quantity；
In described dirigible forming process, after balloonet is full of air, balloonet pressure is 200～400 handkerchiefs, after main gasbag (2) is full of helium
Main gasbag (2) pressure is normally 300～400 handkerchiefs, maximum less than 600 handkerchiefs.
8. the stable state descending method of the stratospheric airship of expanded letter adjustable wing, it is characterised in that: described dirigible is Claims 1 to 4
The stratospheric airship of the expanded letter adjustable wing described in middle any one, this dirigible descending method comprises the following steps:
The folding boat wing is packed up: flight control system controls the folding boat wing (5) folding shrinking；
Dirigible keeps shape: dirigible helium in external world's extraction air fills dirigible shrinks the space produced, and keeps blimp shape
When rising with dirigible consistent；
Dirigible declines: dirigible declines by gravity；
Dirigible lands: when dirigible drops to more than 1200 meters of ground of distance, starts the motor of dirigible, controls dirigible luffing angle
And rate of descent, control dirigible and land.
The stable state descending method of the stratospheric airship of expanded letter adjustable wing the most according to claim 8, it is characterised in that: described
Dirigible rate of descent is less than or equal to 5 meter per seconds；What described dirigible landed comprises the concrete steps that, described dirigible drops to distance ground
When more than 1200 meters, start the motor of dirigible, control dirigible and keep-2～0 degree of angles of depression, and the rate of descent of dirigible is adjusted
To 3 meter per seconds；When described dirigible drops to 300 meters of ground of distance, control dirigible and keep 0～+2 degree elevations angle, use the electronic of dirigible
Machine, adjusts the rate of descent of dirigible to 1 meter per second；When dirigible drops to 50 meters of ground of distance, put down mooring cable；Under described dirigible
When being down to 10 meters of ground of distance, the motor of dirigible is used to be adjusted by the rate of descent of dirigible to 0.5 meter per second, motor vector control
System and rudder face are handled dirigible and are landed windward with the holding of 3 ~ 5 degree of the elevation angle；When described dirigible declines, if overweight state, at dirigible
When dropping to 3000 meters of ground of distance, ship is carried equipment and launches away by flight control system control ship load equipment protecting equipment, and opens
Being fixed on the parachute on ship load equipment, protection ship carries equipment safe landing；When dirigible about 50 meters of ground of distance, land slow
Flushing device (11) starts automatically.
10. the method that the stratospheric airship of an expanded letter adjustable wing keeps cruising altitude, it is characterised in that: when claim 1～4
When dirigible described in middle any one is less than cruising altitude, at least one mode in following three kinds of modes is selected to make dirigible return to
Cruising altitude:
The first rising manner: aileron (6) the ship folded against wing (5) controlling dirigible is adjusted up angle, increases aileron (6)
The elevation angle, the rudder face (8) controlling dirigible is adjusted up angle relative to tailplane (7), increases the elevation angle of rudder face (8), control to fly
The vector propeller (9) of ship provides power, makes dirigible return to cruising altitude；
The second rising manner: control rear balloonet (4) and/or the pressure system of front balloonet (3) of dirigible, make dirigible keep
The elevation angle, the vector propeller (9) controlling dirigible provides power, makes dirigible return to cruising altitude；
The third rising manner: control the vector propeller (9) of dirigible, make dirigible return to cruising altitude；Described the second rises
The concrete grammar making the dirigible holding elevation angle in mode is following at least one:
Control rear balloonet (4) inflation of dirigible and control front balloonet (3) venting simultaneously, making dirigible keep the elevation angle；
Control the air capacity that the air capacity in the rear balloonet (4) of dirigible is more than in front balloonet (3), in i.e. rear balloonet (4)
Air quality more than the air quality in front balloonet (3), make dirigible keep the elevation angle；
The concrete grammar of the third rising manner described is following at least one:
The vector propeller (9) controlling dirigible both sides is opened and upwards 30 ~ 90 degree, provides pulling force upwards for dirigible, makes dirigible
Return to cruising altitude；
The vector propeller (9) controlling dirigible rear portion is opened and downward 30 ~ 90 degree, provides thrust upwards for dirigible, makes dirigible
Return to cruising altitude；
When the dirigible described in any one in claim 1～4 is higher than cruising altitude, in the following three kinds of modes of selection at least
A kind of mode makes dirigible return to cruising altitude:
The first declines mode: aileron (6) the ship folded against wing (5) controlling dirigible regulates downwards angle, increases aileron (6)
The angle of depression, the rudder face (8) controlling dirigible regulates downwards angle relative to tailplane (7), increases the angle of depression of rudder face (8), control to fly
The vector propeller (9) of ship provides power, makes dirigible return to cruising altitude；
The second declines mode: controls rear balloonet (4) and/or the pressure system of front balloonet (3) of dirigible, makes dirigible keep
The angle of depression, the vector propeller (9) controlling dirigible provides power, makes dirigible return to cruising altitude；
The third declines mode: controls the vector propeller (9) of dirigible, makes dirigible return to cruising altitude；Described the second declines
The concrete grammar making the dirigible holding angle of depression in mode is following at least one:
Control rear balloonet (4) venting of dirigible and control front balloonet (3) inflation simultaneously, making dirigible keep the angle of depression；
Control the air capacity that the air capacity in the rear balloonet (4) of dirigible is less than in front balloonet (3), in i.e. rear balloonet (4)
Air quality less than the air quality in front balloonet (3), make dirigible keep the angle of depression；
The third concrete grammar declining mode described is following at least one:
The vector propeller (9) controlling dirigible both sides is opened and downward 30 ~ 90 degree, provides downward pulling force for dirigible, makes dirigible
Return to cruising altitude；
The vector propeller (9) controlling dirigible rear portion is opened and upwards 30 ~ 90 degree, provides downward thrust for dirigible, makes dirigible
Return to cruising altitude.
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4995572A (en) * | 1989-06-05 | 1991-02-26 | Piasecki Aircraft Corporation | High altitude multi-stage data acquisition system and method of launching stratospheric altitude air-buoyant vehicles |
| US20060261213A1 (en) * | 2005-05-17 | 2006-11-23 | Lavan Charles K | Inflatable endurance unmanned aerial vehicle |
| CN101913424A (en) * | 2010-06-24 | 2010-12-15 | 哈尔滨工业大学 | Airship with inflating skeleton expanding in air |
| US20120043416A1 (en) * | 2008-07-07 | 2012-02-23 | Lockheed Martin Corporation | Retracting air cushioned landing system for air vehicles |
| CN103786863A (en) * | 2014-02-17 | 2014-05-14 | 李彦征 | Jet-propelled vertical-lift air bag aircraft |
-
2016
- 2016-08-24 CN CN201610713068.3A patent/CN106240785B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4995572A (en) * | 1989-06-05 | 1991-02-26 | Piasecki Aircraft Corporation | High altitude multi-stage data acquisition system and method of launching stratospheric altitude air-buoyant vehicles |
| US20060261213A1 (en) * | 2005-05-17 | 2006-11-23 | Lavan Charles K | Inflatable endurance unmanned aerial vehicle |
| US20120043416A1 (en) * | 2008-07-07 | 2012-02-23 | Lockheed Martin Corporation | Retracting air cushioned landing system for air vehicles |
| CN101913424A (en) * | 2010-06-24 | 2010-12-15 | 哈尔滨工业大学 | Airship with inflating skeleton expanding in air |
| CN103786863A (en) * | 2014-02-17 | 2014-05-14 | 李彦征 | Jet-propelled vertical-lift air bag aircraft |
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