CN109592035A - High speed information platform and its application method can be suspended - Google Patents
High speed information platform and its application method can be suspended Download PDFInfo
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- CN109592035A CN109592035A CN201811471033.9A CN201811471033A CN109592035A CN 109592035 A CN109592035 A CN 109592035A CN 201811471033 A CN201811471033 A CN 201811471033A CN 109592035 A CN109592035 A CN 109592035A
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- speed information
- information platform
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/34—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising inflatable structural components
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/20—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Train Traffic Observation, Control, And Security (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention provides one kind can suspend high speed information platform and its application method, and it includes: booster that this, which can suspend high speed information platform, booster for realizing high speed information platform assisting flight；Platform class, platform class is connect with booster, platform class includes power unit, reversed only winged system, storage inflation system, class airbag apparatus and load system, power unit is for driving high speed information platform to fly to setting position, the reversed system that only flies after power unit stops working for making platform class be decelerated to command speed range, storage inflation system is connect with class airbag apparatus, storage inflation system is used to inflate to class airbag apparatus to realize that high speed information platform stops setting position in the sky, load system for realizing high speed information platform task execution.It applies the technical scheme of the present invention, to solve the technical issues of remote information transmission in the prior art is insufficient and class aerostatics equipment cannot be applied at a distance.
Description
Technical field
The present invention relates to high-speed aircraft technical fields more particularly to one kind can suspend high speed information platform and its user
Method.
Background technique
Face the future war, the disaster relief when defend stars and other information transmission system exist failure and information transmission with information in relay protection
The problems such as hindering scarce capacity it is necessary to have can rapid fire reach designated position and can have the certain of similar aerostatics and leave a blank
The equipment of time is answered for completing functions, this equipment such as the transmission of emergency information, information relaying, signal interference, Target indication
Has intelligent networking synergistic function.Class aerostatics equipment cannot be applied at a distance, and Asia/supersonic aircraft flying speed is slow,
It is difficult to meet urgent need, needs high-speed aircraft, the fixed point that single high-speed aircraft does not have certain time is left a blank function.
Currently, overseas high speed technical field mainly studies strike weapon, it is applied in war, when the disaster relief by high speed technology
Endoatmosphere quick response, emergency networking carry out information relaying, information interference or search for and have the height for pinpointing ability of leaving a blank
Fast aircraft project does not occur also.
Summary of the invention
The present invention provides one kind can suspend high speed information platform and its application method, is able to solve prior art medium-long range
The technical issues of information transmission is insufficient and class aerostatics equipment cannot apply at a distance.
According to an aspect of the present invention, high speed information platform can be suspended by providing one kind, can suspend high speed information platform packet
Include: booster, booster for realizing high speed information platform assisting flight；Platform class, platform class are connect with booster, platform
Grade includes power unit, reversed only winged system, storage inflation system, class airbag apparatus and load system, and power unit is for driving
Dynamic high speed information platform flies to setting position, and the reversed system that only flies after power unit stops working for making platform class slow down
It to command speed range, stores inflation system and is connect with class airbag apparatus, storage inflation system is used to inflate to class airbag apparatus with reality
Existing high speed information platform stops setting position in the sky, load system for realizing high speed information platform task execution.
Further, load system includes that information transmission is searched with relay system equipment, signal interference system equipment or target
Cable system equipment, information transmission are relayed with relay system equipment for realizing the information transmission of high speed information platform and information, letter
Number interference system equipment is for carrying out signal interference, and target acquisition system equipment is for realizing target search.
Further, platform class has the first accommodation chamber and the second accommodation chamber, and the first accommodation chamber is arranged in the second accommodation chamber
Top, stores inflation system and class airbag apparatus is arranged in the first accommodation chamber, reversed only to fly system, load system and power unit
It is arranged in the second accommodation chamber.
Further, platform class further includes slidably hatch door, and slidably hatch door is arranged at the first accommodation chamber, slidably cabin
Door is used to open or closes the first accommodation chamber.
Further, high speed information platform further includes fuel system, and fuel system is arranged in the second accommodation chamber, fuel system
System is connect with power unit.
Further, power unit includes engine.
Further, platform class further includes destruct system, and destruct system is arranged in platform class, and destruct system is in office
The self-destruction of high speed information platform is realized after the completion of business.
Further, can suspend high speed information platform further includes guidance control system, and guidance control system is arranged in platform
Grade in, guidance control system be used for adjust high speed information platform posture and track so that high speed information platform according to desired trajectory
Flight.
Further, can suspend high speed information platform further includes structure and thermal protection system and rudder face, and structure and heat are anti-
Protecting system is used to carry out structural bearing d type to high speed information platform and the tail end of platform class, rudder face is arranged in thermal protection, rudder face
For adjusting the posture of high speed information platform.
According to another aspect of the invention, a kind of application method of high speed information platform is provided, high speed information platform
Application method includes: step 1, and high speed information platform emits according to instruction from platform, and boosting is realized in booster igniting；Step 2,
After high speed information platform reaches burble point, booster is separated with platform class, and platform class is accelerated using power unit to realize high speed
The high-speed flight of information platform；Step 3, when platform class will reach setting position, power unit is closed, reversed only to fly system
Starting is to be decelerated to command speed range for platform class；Step 4, in platform class moderating process, the reversed systems stay that only flies is made
With class airbag apparatus pops up and passes through storage inflation system and is inflated；Step 5, after high speed information platform reaches setting position,
Class airbag apparatus completes inflation, and platform class suspends in the sky, and load system completes inter-related task；Step 6, after the completion of task, from
Ruin system acting to complete the self-destruction of platform class or jettisoning class airbag apparatus, platform class self gravity undershoot to the ground.
It applies the technical scheme of the present invention, high speed information platform can be suspended by providing one kind, which passes through
Class airbag apparatus is set, high-speed aircraft technology is combined with aerostatics technology, can either be flown speed using high-speed aircraft
Fast advantage is spent, while the feature that can leave a blank in conjunction with aerostatics fixed point, aerial setting position can be reached quickly to complete to leave a blank
Intelligent, emergency quick response is realized in operation according to actual needs.Furthermore high speed information platform of the invention passes through load
System can execute task in setting position in the sky, to realize the transmission of emergency information, information relaying, signal interference and target
The functions such as search.In addition, high speed information platform of the invention being capable of different spaces within the scope of ultimate run according to actual needs
Position is quickly layouted, and platform application range is expanded, and improves working platform efficiency.
Detailed description of the invention
Included attached drawing is used to provide to be further understood from the embodiment of the present invention, and which constitute one of specification
Point, for illustrating the embodiment of the present invention, and come together to illustrate the principle of the present invention with verbal description.It should be evident that below
Attached drawing in description is only some embodiments of the present invention, for those of ordinary skill in the art, is not paying creation
Property labour under the premise of, be also possible to obtain other drawings based on these drawings.
Fig. 1 shows the high speed information platform that suspends provided according to a particular embodiment of the invention and leaves a blank in non-fixed point
The structural schematic diagram of state；
Fig. 2 shows the high speed information platforms that suspends provided according to a particular embodiment of the invention to be in fixed point and leave a blank shape
The structural schematic diagram of state.
Wherein, the above drawings include the following reference numerals:
10, booster；20, platform class；20a, the first accommodation chamber；20b, the second accommodation chamber；21, power unit；22, reversed
Only fly system；23, inflation system is store；24, class airbag apparatus；25, load system；26, slidably hatch door；27, fuel system；
28, destruct system；29, rudder face.
Specific embodiment
It should be noted that in the absence of conflict, the features in the embodiments and the embodiments of the present application can phase
Mutually combination.Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Ground description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is right below
The description only actually of at least one exemplary embodiment be it is illustrative, never as to the present invention and its application or use
Any restrictions.Based on the embodiments of the present invention, those of ordinary skill in the art are without creative efforts
Every other embodiment obtained, shall fall within the protection scope of the present invention.
It should be noted that term used herein above is merely to describe specific embodiment, and be not intended to restricted root
According to the illustrative embodiments of the application.As used herein, unless the context clearly indicates otherwise, otherwise singular
Also it is intended to include plural form, additionally, it should be understood that, when in the present specification using term "comprising" and/or " packet
Include " when, indicate existing characteristics, step, operation, device, component and/or their combination.
Unless specifically stated otherwise, positioned opposite, the digital table of the component and step that otherwise illustrate in these embodiments
It is not limited the scope of the invention up to formula and numerical value.Simultaneously, it should be appreciated that for ease of description, each portion shown in attached drawing
The size divided not is to draw according to actual proportionate relationship.For technology, side known to person of ordinary skill in the relevant
Method and equipment may be not discussed in detail, but in the appropriate case, and the technology, method and apparatus should be considered as authorizing explanation
A part of book.In shown here and discussion all examples, any occurrence should be construed as merely illustratively, and
Not by way of limitation.Therefore, the other examples of exemplary embodiment can have different values.It should also be noted that similar label
Similar terms are indicated in following attached drawing with letter, therefore, once it is defined in a certain Xiang Yi attached drawing, then subsequent attached
It does not need that it is further discussed in figure.
As depicted in figs. 1 and 2, high speed information platform can be suspended by providing one kind according to a particular embodiment of the invention, should
It includes booster 10 and platform class 20 that high speed information platform, which can be suspended, and booster 10 flies for realizing the boosting of high speed information platform
Row, platform class 20 connect with booster 10, platform class 20 include power unit 21, reversed only winged system 22, store inflation system 23,
Class airbag apparatus 24 and load system 25, power unit 21 is for driving high speed information platform to fly to setting position, reversely
Only fly system 22 for making platform class 20 be decelerated to command speed range after power unit 21 stops working, stores inflation system 23
It is connect with class airbag apparatus 24, storage inflation system 23 is used to inflate to class airbag apparatus 24 to realize that high speed information platform rests on
Aerial setting position, load system 25 for realizing high speed information platform task execution.
Using such configuration mode, high speed information platform can be suspended by providing one kind, which passes through setting
Class airbag apparatus combines high-speed aircraft technology with aerostatics technology, can either be fast using high-speed aircraft flying speed
The advantages of, it while can leave a blank feature in conjunction with aerostatics fixed point, aerial setting position can be reached quickly to complete operation of leaving a blank,
Intelligent, emergency quick response is realized according to actual needs.Furthermore high speed information platform of the invention passes through load system energy
Enough setting positions in the sky execute task, to realize the transmission of emergency information, information relaying, signal interference and target search etc.
Function.In addition, high speed information platform of the invention can different spatial be fast within the scope of ultimate run according to actual needs
Speed is layouted, and platform application range is expanded, and improves working platform efficiency.
Further, in the present invention, it is transmitted to complete emergency information, information relaying, signal interference, target search
Etc. functions, load system 25 can be configured to include information transmission with relay system equipment, signal interference system equipment or target
Search system equipment, information transmission are relayed with relay system equipment for realizing the information transmission of high speed information platform and information,
Signal interference system equipment is for carrying out signal interference, and target acquisition system equipment is for realizing target search.
Using such configuration mode, after high speed information platform reaches aerial setting position, platform class is filled by class air bag
Set suspension in the sky, load system is started to work at this time, and information transmission carries out in information transmission and information with relay system equipment
After signal interference system equipment carries out signal interference, and target acquisition system carries out target search, is achieved in high speed information platform
Task execution function.
It further, in the present invention, can be by platform class as shown in Figure 1, normal work in order to guarantee class airbag apparatus
20 are configured to have the first accommodation chamber 20a and the second accommodation chamber 20b, the first accommodation chamber 20a setting on the second accommodation chamber 20b
Portion, stores inflation system 23 and class airbag apparatus 24 is arranged in the first accommodation chamber 20a, reversed only to fly system 22, load system 25
It is arranged in the second accommodation chamber 20b with power unit 21.As a specific embodiment of the invention, class airbag apparatus 24 includes
Air bag and other can play the role of the component of air bag.
In addition, in the present invention, platform class 20 further includes that slidably hatch door 26, the slidably setting of hatch door 26 are accommodated first
At the 20a of cabin, slidably hatch door 26 is used to open or closes the first accommodation chamber 20a.It is high as a specific embodiment of the invention
Fast information platform emits after being connected to instruction from the platforms such as vehicle-mounted, airborne, carrier-borne, the igniting boosting of booster 10.Work as high speed information
After platform reaches burble point, booster 10 is separated with 20 phase of platform class at this time, and platform class 20 is speeded up to realize using power unit 21
High-speed flight.When platform class 20 will reach predetermined spatial position, power unit 21 shuts down, it is reversed only fly the starting of system 22 with
Platform class 20 is set to be decelerated to command speed range, during platform class 20 slows down, slidably hatch door 26 is opened, at this time class gas
Bag apparatus 24 pops up and is the inflation of class airbag apparatus by storage inflation system 23.After platform class 20 reaches predetermined spatial position,
The inflation of class airbag apparatus 24 terminates, and platform class 20 suspends in the sky, the loading device start information transmission inside platform class 20, letter
Number interference or search, instruction target, networking communication etc. work.After the completion of task, platform class can carry out self-destruction or rush at ground.
In the present invention, engine can be used as power unit 21.In addition, high speed information platform further includes fuel system
27, fuel system 27 is arranged in the second accommodation chamber 20b, and fuel system 27 is connect with power unit 21.
Further, in the present invention, platform class 20 further includes destruct system 28, and destruct system 28 is arranged in platform class 20
Interior, destruct system 28 after the completion of task for realizing the self-destruction of high speed information platform.
In addition, in the present invention, in order to guarantee the correctness of high speed information platform running track, can suspend high speed and believe
Breath platform configuration is further includes guidance control system, and in platform class 20, guidance control system is used for for guidance control system setting
The posture for adjusting high speed information platform and track are so that high speed information platform flies according to desired trajectory.
Further, in the present invention, in order to guarantee the working performance of high speed information platform, high speed information can be suspended
To further include structure and thermal protection system and rudder face 29, structure and thermal protection system are used for high speed information platform platform configuration
Structural bearing d type and thermal protection are carried out, the tail end of platform class 20 is arranged in rudder face 29, and rudder face 29 is flat for adjusting high speed information
The posture of platform.
According to another aspect of the present invention, a kind of application method of high speed information platform is provided, the high speed information platform
Application method include: step 1, high speed information platform emits according to instruction from platform, and boosting is realized in the igniting of booster 10；Step
Rapid two, after high speed information platform reaches burble point, booster 10 is separated with platform class 20, and platform class 20 is added using power unit 21
Speed is to realize the high-speed flight of platform class 20；Step 3, when platform class 20 will reach setting position, power unit 21 is closed,
It is reversed to fly the starting of system 22 only platform class 20 is decelerated to command speed range；Step 4, in 20 moderating process of platform class, instead
To 22 continuous action of system is only flown, class airbag apparatus 24 is popped up and is inflated by storing inflation system 23；Step 5, platform class
After 20 reach setting position, class airbag apparatus 24 completes inflation, and platform class 20 suspends in the sky, and load system 25 completes related appoint
Business；Step 6, after the completion of task, the movement of destruct system 28 to complete self-destruction or the jettisoning class airbag apparatus 24 of platform class 20,
Platform class 20 self gravity undershoot to the ground.
Using the application method of high speed information platform of the invention, high speed information platform can be realized in ultimate run range
Interior different spatial is quickly layouted, while can realize intelligent, emergency quick response according to actual needs, has information
The multiple functions such as relaying, information transmission, information interference, multiple networkings communication.
Further understand to have to the present invention, the high speed information that suspends of the invention is put down below with reference to Fig. 1 and Fig. 2
Platform and its application method are described in detail.
As depicted in figs. 1 and 2, high speed information platform can be suspended by providing one kind according to a particular embodiment of the invention, should
High speed information platform includes booster 10 and platform class 20, and platform class 20 includes power unit 21, reversed only winged system 22, stores and fill
Gas system 23, class airbag apparatus 24, load system 25, slidably hatch door 26, fuel system 27, destruct system 28, structure and heat
Guard system and rudder face 29, using engine as power unit 21, fuel system 27 is connected with engine, platform class 20
With the first accommodation chamber 20a and the second accommodation chamber 20b, the first accommodation chamber 20a setting in the second top accommodation chamber 20b, storage inflation
System 23 and class airbag apparatus 24 are arranged in the first accommodation chamber 20a, reversed only to fly system 22, load system 25, fuel system
27, destruct system 28, power unit 21 are arranged in the second accommodation chamber 20b, and load system 25 includes information transmission and relaying is
System equipment, signal interference system equipment or target acquisition system equipment, structure and thermal protection system are mainly disposed to high speed information
Between the wall surface and bay section of platform, for realizing the structural bearing d type and thermal protection effect to high speed information platform.
In a specific embodiment of the present invention, can suspend high speed information platform track be divided into acceleration climb section, high speed fly
Row section, active section of leaving a blank etc., after completion task, platform class has self-destruction or rushes at the ability on ground.Specifically, high speed information is flat
The course of work of platform is as follows.
Step 1, high speed information platform upon command, emit, 10 points of booster from the platforms such as vehicle-mounted, airborne, carrier-borne
Fiery boosting is to realize the transmitting of high speed information platform.
Step 2, after high speed information platform reaches burble point, booster 10 is separated with platform class 20, and platform class 20 utilizes hair
Motivation accelerates the high-speed flight to realize platform class 20.
Step 3, when platform class 20 will reach setting position, tail-off is reversed to fly the starting of system 22 only put down
Platform grade 20 is decelerated to command speed range.
Step 4, reversed only to fly 22 continuous action of system in 20 moderating process of platform class, slidably hatch door 26 is opened, storage
Inflation system 23 starts, and class airbag apparatus 24 is popped up and is inflated by storing inflation system 23.
Step 5, after platform class 20 reaches setting position, class airbag apparatus 24 completes inflation, and platform class 20 is suspended in sky
In, the work such as 25 start information transmission of load system, signal interference, target search, networking communication.
Step 6, after the completion of task, the movement of destruct system 28 is to complete self-destruction or the jettisoning class air bag dress of platform class 20
Set 24, platform class 20 self gravity undershoot to the ground.
In conclusion the present invention overcomes existing remote information transmission insufficient and class aerostatics equipment cannot be applied at a distance
The problems such as, provide intelligent Application under a kind of following emergency rating can quickly reach and can to suspend the high speed information that uses flat
Platform and application method.High speed information platform provided by the present invention compared with prior art, has the following advantages that.
First, high speed information platform of the invention is by setting class airbag apparatus, by high-speed aircraft technology and aerostatics
Technology combines, the advantage that high-speed aircraft flying speed can either be utilized fast, while the spy that can leave a blank in conjunction with aerostatics fixed point
Point can reach aerial setting position quickly to complete operation of leaving a blank, and realize that intelligent, emergency is quickly rung according to actual needs
It answers.
Second, high speed information platform of the invention can complete emergency group in setting position in the sky by load system
Net, to realize the functions such as the transmission of emergency information, information relaying, signal interference and Target indication.
Third, high speed information platform of the invention being capable of the different spatials within the scope of ultimate run according to actual needs
It quickly layouts, expands platform application range, improve working platform efficiency.
For ease of description, spatially relative term can be used herein, as " ... on ", " ... top ",
" ... upper surface ", " above " etc., for describing such as a device shown in the figure or feature and other devices or spy
The spatial relation of sign.It should be understood that spatially relative term is intended to comprising the orientation in addition to device described in figure
Except different direction in use or operation.For example, being described as if the device in attached drawing is squeezed " in other devices
It will be positioned as " under other devices or construction after part or construction top " or the device of " on other devices or construction "
Side " or " under other devices or construction ".Thus, exemplary term " ... top " may include " ... top " and
" in ... lower section " two kinds of orientation.The device can also be positioned with other different modes and (is rotated by 90 ° or in other orientation), and
And respective explanations are made to the opposite description in space used herein above.
In addition, it should be noted that, limiting components using the words such as " first ", " second ", it is only for be convenient for
Corresponding components are distinguished, do not have Stated otherwise such as, there is no particular meanings for above-mentioned word, therefore should not be understood as to this
The limitation of invention protection scope.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, for the skill of this field
For art personnel, the invention may be variously modified and varied.All within the spirits and principles of the present invention, made any to repair
Change, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (10)
1. one kind can suspend high speed information platform, which is characterized in that the high speed information platform that suspends includes:
Booster (10), the booster (10) for realizing the high speed information platform assisting flight；
Platform class (20), the platform class (20) connect with the booster (10), and the platform class (20) includes power unit
(21), reversed only to fly system (22), storage inflation system (23), class airbag apparatus (24) and load system (25), the power
For driving the high speed information platform to fly to setting position, described reversed only fly system (22) are used for described unit (21)
Power unit (21) makes the platform class (20) be decelerated to command speed range after stopping working, the storage inflation system (23) with
Class airbag apparatus (24) connection, the storage inflation system (23) are used to inflate to the class airbag apparatus (24) to realize
Stating the stop of high speed information platform, setting position, the load system (25) are held in the sky for realizing the task of high speed information platform
Row.
2. according to claim 1 suspend high speed information platform, which is characterized in that the load system (25) includes letter
Breath transmission and relay system equipment, signal interference system equipment or target acquisition system equipment, the information transmission are with relaying
Unite equipment for realizing the high speed information platform information transmission and information relaying, the signal interference system equipment be used for into
Row signal interference, the target acquisition system equipment is for realizing target search.
3. according to claim 1 suspend high speed information platform, which is characterized in that the platform class (20) has first
Accommodation chamber (20a) and the second accommodation chamber (20b), first accommodation chamber (20a) are arranged on second accommodation chamber (20b)
Portion, the storage inflation system (23) and the class airbag apparatus (24) setting are described reversed in first accommodation chamber (20a)
It is interior in second accommodation chamber (20b) only to fly system (22), the load system (25) and the power unit (21) setting.
4. according to claim 3 suspend high speed information platform, which is characterized in that the platform class (20) further includes can
It slides hatch door (26), the slidably hatch door (26) is arranged at first accommodation chamber (20a), the slidably hatch door (26)
It is used to open or closes first accommodation chamber (20a).
5. according to claim 4 suspend high speed information platform, which is characterized in that the high speed information platform further includes
Fuel system (27), fuel system (27) setting is in second accommodation chamber (20b), the fuel system (27) and institute
State power unit (21) connection.
6. according to claim 5 suspend high speed information platform, which is characterized in that the power unit (21) includes hair
Motivation.
7. according to any one of claim 1 to 6 suspend high speed information platform, which is characterized in that the platform class
It (20) further include destruct system (28), destruct system (28) setting is in the platform class (20), the destruct system
(28) for realizing the self-destruction of the high speed information platform after the completion of task.
8. according to claim 7 suspend high speed information platform, which is characterized in that described to suspend high speed information platform
It further include guidance control system, in the platform class (20), the guidance control system is used for the guidance control system setting
In the posture and track for adjusting the high speed information platform so that the high speed information platform flies according to desired trajectory.
9. according to claim 8 suspend high speed information platform, which is characterized in that described to suspend high speed information platform
It further include structure and thermal protection system and rudder face (29), the structure and thermal protection system are used for the high speed information platform
Carry out structural bearing d type and thermal protection, tail end of rudder face (29) setting in the platform class (20), the rudder face (29)
For adjusting the posture of the high speed information platform.
10. a kind of application method of high speed information platform, which is characterized in that the application method of the high speed information platform includes:
Step 1, high speed information platform emit according to instruction from platform, and boosting is realized in booster (10) igniting；
Step 2, after the high speed information platform reaches burble point, the booster (10) separates with platform class (20), described flat
Platform grade (20) accelerates the high-speed flight to realize the high speed information platform using power unit (21)；
Step 3, when the platform class (20) will reach setting position, the power unit (21) is closed, reversed only to fly system
(22) starting is to be decelerated to command speed range for the platform class (20)；
Step 4, it is described reversed only to fly system (22) continuous action, class airbag apparatus in platform class (20) moderating process
(24) it pops up and is inflated by storing inflation system (23)；
Step 5, after the platform class (20) reaches setting position, the class airbag apparatus (24) completes inflation, the platform class
(20) it suspends in the sky, load system (25) completes inter-related task；
Step 6, after the completion of task, destruct system (28) is acted to complete described in self-destruction or the jettisoning of the platform class (20)
Class airbag apparatus (24), the platform class (20) self gravity undershoot to the ground.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811471033.9A CN109592035A (en) | 2018-12-04 | 2018-12-04 | High speed information platform and its application method can be suspended |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811471033.9A CN109592035A (en) | 2018-12-04 | 2018-12-04 | High speed information platform and its application method can be suspended |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109592035A true CN109592035A (en) | 2019-04-09 |
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ID=65960637
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811471033.9A Pending CN109592035A (en) | 2018-12-04 | 2018-12-04 | High speed information platform and its application method can be suspended |
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Application publication date: 20190409 |