CN110174025A - A kind of wind and solar integrated new energy guided missile vertical air flat pad - Google Patents
A kind of wind and solar integrated new energy guided missile vertical air flat pad Download PDFInfo
- Publication number
- CN110174025A CN110174025A CN201810169609.XA CN201810169609A CN110174025A CN 110174025 A CN110174025 A CN 110174025A CN 201810169609 A CN201810169609 A CN 201810169609A CN 110174025 A CN110174025 A CN 110174025A
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- Prior art keywords
- guided missile
- cabin
- solar
- wind
- main nacelle
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- 230000001681 protective effect Effects 0.000 claims abstract description 42
- 230000002093 peripheral effect Effects 0.000 claims abstract description 27
- 238000009434 installation Methods 0.000 claims abstract description 20
- 125000001475 halogen functional group Chemical group 0.000 claims abstract description 10
- 238000010248 power generation Methods 0.000 claims description 8
- 239000007921 spray Substances 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 230000007774 longterm Effects 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 230000005611 electricity Effects 0.000 description 7
- 241000209094 Oryza Species 0.000 description 4
- 235000007164 Oryza sativa Nutrition 0.000 description 4
- 235000009566 rice Nutrition 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
Abstract
A kind of wind and solar integrated new energy guided missile vertical air flat pad, it is by main nacelle, guided missile Vertical Launch well and its peripheral protective protect structure, MISSILE LAUNCHING controls cabin, wind and solar integrated generator, solar energy power generating umbrella, which forms, on peripheral protective protective cradle and its top surface in platform main nacelle suspends barrel shape body in midair under a photovoltaic umbrella, around barrel shape body up and down, layered distribution type installation pressure solar or lunar halo, air expands injector, solar energy power generating flying wing, manufacturing into one kind can be with vertical rise and fall, the aerial long-term wind and solar integrated new energy guided missile vertical air flat pad to hover or fly, it can be used for the transmitting of guided missile vertical air, air transport, the dual-use product of rescue and relief work multiple use.Market prospects are bright.
Description
Technical field
The invention patent relates to aircraft industry more particularly to a kind of wind and solar integrated new energy guided missile vertical air transmitting are flat
Platform.
Background technique
A kind of the applicant's utility model patent being authorized on May 6th, 2015: wind and solar integrated generator.The patent No.:
ZL201520051312.5.A kind of wind and solar integrated power generation solution is disclosed, wind and solar integrated power generating industry development side is proposed
To being integrally formed generator for wind-power electricity generation, solar energy power generating and started a new route.The applicant in order to as early as possible will
Patented technology achievements conversion is engineering project, patent application that the present invention is specifically proposed.
Summary of the invention
The technical problem to be solved is that group is built up based on wind and solar integrated generator weeks quiet honourable one for the invention patent
Body generation of electricity by new energy station provides never exhausted electric power for guided missile vertical air flat pad.Make guided missile vertical air flat pad
It does not need using traditional fuel, by based on wind-power electricity generation, supplemented by solar energy power generating, realizing its VTOL, aerial long
Phase is outstanding stay or fly guided missile vertical air flat pad weapon is driven by pure electric power.
The technical solution to solve the above problems that the invention patent proposes is: a kind of wind and solar integrated new energy guided missile hangs down in the air
Straight flat pad, it is characterised in that: on the center of platform main nacelle 1, in the upper cabin of platform main nacelle 1, open peace
Dress through platform main nacelle 1 guided missile Vertical Launch well 2 and its peripheral protective protection structure 3 round mouth, in lower cabin, open with
MISSILE LAUNCHING controls the consistent round mouth of opening of the upper-deck cabin dignity of cabin 14, and the two is open and welds integral, MISSILE LAUNCHING
Control cabin 14 be under 1 bottom surface of platform main nacelle, for guided missile Vertical Launch well 2 and peripheral protective protection structure 3 installation and
The cabin of launch control equipment installation；On the upper-deck cabin top surface of platform main nacelle 1, around the peripheral protective of guided missile Vertical Launch well 2
Structure 3 is protected, wind and solar integrated generator 4 is installed；On the upper-deck cabin top surface of platform main nacelle 1, outside wind and solar integrated generator 4
Peripheral protective protective cradle 5 is installed in side；On the top end face of peripheral protective protective cradle 5, solar energy power generating umbrella 6 is installed, too
On the center of positive energy photovoltaic power generation umbrella 6, guided missile Vertical Launch well head 7 and hole cover 8 are set；In peripheral protective protective cradle 5
On lateral surface, the distributed pressure solar or lunar halo 9 of layering installation and air expand injector 10；On the outer side elevation of platform main nacelle 1, peace
Door 11 and window 12 are filled, above and below the door 11 of platform main nacelle 1 and the interval position of window 12, distribution installation solar energy power generating
Flying wing 13；On the bottom surface of MISSILE LAUNCHING control cabin 14, setting MISSILE LAUNCHING wake flame sprays drain port 15 and wake flame sprays drain port
Lid 16；Under the bottom on-deck of platform main nacelle 1, cabin 14, distributed installation platform VTOL are controlled around MISSILE LAUNCHING
Land play landing-gear 17 and the water surface and play landing-gear 18, the wind and solar integrated new energy guided missile for forming a barrel shape is aerial
Vertical Launch platform.
Guided missile Vertical Launch well 2 and its peripheral protective protect structure 3, it is necessary to assure vertical under any environmental condition in the sky
State.In addition to the requirement of guided missile Vertical Launch well to be met, and to guarantee on guided missile vertical air flat pad all sets
Standby and personnel safety are important to guarantee the wind and solar integrated generator that the peripheral protective protection structure 3 around Vertical Launch well 2 is installed
4 safety.
Platform main nacelle 1 and its wind and solar integrated generator 4 and peripheral protective protective cradle 5 determine that guided missile vertical air is sent out
Penetrate the diameter and the scale of construction of the barrel shape of platform.It is simultaneously to be at tumbler state, guarantees that guided missile Vertical Launch well is in office
It can be in plumbness under what environmental weather conditions, make to stand vertically the guided missile , Longitude in silo and be often in arm-to-arm,
It can emit immediately after being connected to order.
Dashed line view indicates guided missile Vertical Launch well 2 and its peripheral protective protection structure 3, platform main nacelle 1 and its outer in Fig. 1
Go along with sb. to guard him the guided missile vertical air flat pad true form of image height neck vase in the protection big module of structure 5 two composition drum.Simultaneously
Indicate that two big modules belong to user oneself and configure interior range.High neck vase shape is more convenient to realize tumbler target.In platform
All devices, instrument, power grid and control room are installed in main nacelle 1.
Wind and solar integrated generator 4 be guarantee wind-power electricity generation based on, supplemented by solar energy power generating, to guided missile vertical air send out
It penetrates platform and sufficient, never exhaustion power equipment is provided.
Since the guided missile vertical air flat pad scale of construction is very big, general load is all at hundred tons or more.It hangs down to meet it
It directly rises and falls, aerial long-term hang is stayed or fly, it is necessary to assure sufficient electric power.This is that a typhoon light integrated generator can not meet
, it is necessary to be install load quantity wind and solar integrated generator guarantee electricity supply jointly.Thus composition week quiet honourable one
Body generation of electricity by new energy station.
The wind and solar integrated generator 4 for the load quantity installed on guided missile vertical air flat pad, each wind and solar integrated
Generator be all it is independently operated, will not adversely affect from each other, be conducive to regulation and administration and maintenance.Nominal number
Measuring wind and solar integrated generator 4 is determined by the electricity needs total amount of drum guided missile vertical air flat pad.Its mounting means root
According to the power grid composed structure mode of guided missile vertical air flat pad, wind and solar integrated generator 4 is installed using distribution.
Electronic pressure solar or lunar halo 9 is that guided missile vertical air flat pad realizes that landing of taking off vertically, aerial long-term hang are stayed or fly
Power-equipment.Above and below 5 lateral surface of peripheral protective protective cradle of 1 cabin top surface of platform main nacelle, it is uniform, equidistant, symmetrical
The electronic pressure solar or lunar halo 9 of installation is a kind of interior electronic extrusion wind power installation for installing motor, propeller blade composition of shield solar or lunar halo.It
It is the mounting structure that air-out direction can be pressed with rotation transformation, when it presses down air, guided missile vertical air flat pad is risen
It ascends to heaven sky, when it extrudes air upwards, platform quickly lands, and when it extrudes air to any horizontal direction, platform is to going out
The flight of gas opposite direction.
Each electronic pressure solar or lunar halo 9 is all to have specified lifting force value, the 9 general increase power number of electronic pressure solar or lunar halo of load quantity
Value is to be determined by the guided missile vertical air flat pad own wt of barrel shape with the overall load numerical value for appraising and deciding load weight
Fixed, and there are security value (s)s.
It is to provide the electrical equipment of propulsion power for guided missile vertical air flat pad that air, which expands injector 10,.By high pressure
Air compressor and air expander and connecting conduit composition.High-Pressure Compressor is mounted in platform main nacelle 1, and air expands
Big device is mounted on 5 lateral surface of peripheral protective protective cradle.
Air expands injector 10 and pressure solar or lunar halo 9 is all to separate into a group distribution to be mounted on 5 outside of peripheral protective protective cradle
On face, the dynamical system for cooperating and being uniformly controlled is formed, provides vertical rise and fall for guided missile vertical air flat pad, it is aerial long
The power-equipment of phase hovering or flight.
Solar energy power generating flying wing 13 is a kind of flexible, can change nyctitropic flying wing, it is aerial to guided missile
Vertical Launch platform provides a kind of solar energy power generating flying wing of intermittent, complementary power supply, is for guided missile vertical air
Flat pad provides balanced in plane a kind of stable flying wing, is that heading guide is provided for guided missile vertical air flat pad
A kind of flying wing.
Solar energy power generating flying wing 13 by flight wing support and solar photovoltaic electrification component form it is shrinkable, can
It stretches, a kind of equipment of direction-changeable.It is mounted on the lateral surface of platform main nacelle 1, it is faced using the left and right sides
Claim installation control structure, every four flying wings are one cross group.According to the flying wing group of load quantity, platform main nacelle is surrounded
1 lateral surface is equidistant, upper and lower that is balanced, being symmetrically mounted on its interval part of door 11 on side and window 12 out of my cabin.It is each
A symmetrical group is all to have respective control system, and thus a kind of equipment of power generation, balance, airbound target guide can be achieved in composition.
Solar energy power generating umbrella 6 is mounted in one kind on the top of the peripheral protective protective cradle 5 in platform main nacelle 1
Flat parachute is provided with a guided missile Vertical Launch mouth 7 above guided missile Vertical Launch well head, installs on emission port in umbrella central point
Be movable Sunny energy photovoltaic power generation canopy 8 to be opened/closed.
Solar energy power generating umbrella 6 is the fixed sun of the fixed bracket in 5 top surface of peripheral protective protective cradle in platform main nacelle 1
It can photovoltaic power generation umbrella 6.Solar energy power generating umbrella 6 is by fixed umbrella and recoverable extensible active sun energy photovoltaic power generation umbrella
6 two parts composition.When the solar energy power generating umbrella 6 entirely to trail is outstanding stays in aerial, the barrel shape that is suspended in midair under umbrella
Guided missile vertical air flat pad can be enhanced it and keep suspending power and equilibrium state, be provided simultaneously with photovoltaic power generation function.
It is to connect integral cabin in 1 bottom opening of platform main nacelle that MISSILE LAUNCHING, which controls cabin 14, is hung down around guided missile
The bottom end part setting of straight silo 2 and peripheral protective protection structure 3, the dedicated bay for guided missile installation launch control equipment.
The bottom surface setting MISSILE LAUNCHING wake flame that MISSILE LAUNCHING controls cabin 14 sprays drain port 15 and wake flame sprays drain port lid 16.
It is that cabin 14, distribution are controlled around MISSILE LAUNCHING that landing-gear 17 is played on the land of guided missile vertical air flat pad
Formula is mounted on the bilge face of platform main nacelle 1, is made of floor stand and two component of floor wheel, load quantity is aerial by guided missile
The overall weight and floor space requirement of Vertical Launch platform determine.
It is that distribution is mounted on land landing-gear 17 that the water surface of guided missile vertical air flat pad, which plays landing-gear 18,
Between, it is a kind of aircushion vehicle.
A kind of vertical rise and fall of wind and solar integrated new energy guided missile vertical air flat pad aerial long-term is hovered or flight
Technical characteristic, become it is a kind of can be used for the transmitting of guided missile vertical air, air transport, a variety of the army and the people's purposes of rescue and relief work reality
With product, market prospects light.
Detailed description of the invention
Fig. 1: wind and solar integrated new energy guided missile vertical air flat pad diagrammatic cross-section；
Specific embodiment
Embodiment is described in detail according to Figure of description as follows:
A kind of wind and solar integrated new energy guided missile vertical air flat pad of embodiment: take off vertically weight: 200 tons, drum
The diameter of shape guided missile Vertical Launch platform: 70 meters, height: 38 meters.The diameter of guided missile Vertical Launch well 2 determining first: 5 meters,
Highly: 25 meters；Further according to 2 specification of guided missile Vertical Launch well, the peripheral protective for making guided missile Vertical Launch well protects structure 3,
It is 15 meters of diameter, 35 meters of height, and the cylinder of the two open ends for the profile production that 3 meters of thickness protects structure 3, is inside led
Play the installation site of Vertical Launch well 2 and related accessories；Then the barrel shape main nacelle 1 of platform for making main nacelle 1, drum master
70 meters of the diameter of cabin 1,12 meters of height.The diameter center point in the overhead bin face of drum main nacelle 1 opens the circle of 15 rice diameters
Opening, the peripheral protective for being inserted in silo protect structure 3；Diameter 30 according to on-deck opening in MISSILE LAUNCHING control cabin 14
Rice opens 30 meters of circular opens at the center in 1 bilge face of platform main nacelle, and is open and welds with the top surface of MISSILE LAUNCHING control cabin 14
It is connected into whole cabin；Then on the cabin top surface of platform main nacelle 1, peripheral protective is installed along the excircle of platform main nacelle 1
Protective cradle 5；Peripheral protective protective cradle 5 is 70 meters of diameter, 21 meters of height, the hollow branch for the profile production that 5 meters of thickness
Frame is used for fixed solar photovoltaic power generating umbrella 6, circumference with sunlight irradiation, the cylinder stent structure of top opening for divulging information
On outside, expand injector 10 for layered distribution type installation pressure solar or lunar halo 9 and air；The diameter 30 of MISSILE LAUNCHING control cabin 14
Rice, 3 meters of height, cabin is suitable for reading consistent with 1 under shed size of platform main nacelle and welds integral cabin, in MISSILE LAUNCHING control cabinet
14 bottom surface midpoint of body opens up 5 rice diameter wake flames spray drain port 15 and wake flame spray drain port lid 16.Then by two cylinder stent structure sets
Together, between two cylinder stents, distribution installs wind and solar integrated generator 4；Under the hold face of platform main nacelle 1,
Cabin 14, distribution installation land take-off and landing device 17 and water surface take-off and landing device 18, land take-off and landing device are controlled around MISSILE LAUNCHING
17 are made of bracket and two parts of wheel, and water surface take-off and landing device 18 is a kind of aircushion vehicle, is distributed between land take-off and landing device 17.
Claims (1)
1. a kind of wind and solar integrated new energy guided missile vertical air flat pad, it is characterised in that: at the center of platform main nacelle (1)
On position, in the upper cabin of platform main nacelle (1), open installation through platform main nacelle (1) guided missile Vertical Launch well (2) and
Its peripheral protective protects the round mouth of structure (3), in lower cabin, opens the opening with the upper-deck cabin dignity of MISSILE LAUNCHING control cabin (14)
Consistent round mouth, and the two opening is welded into integral cabin, it is in platform main nacelle (1) that MISSILE LAUNCHING, which controls cabin (14),
Under bottom surface, cabin is installed in installation and launch control equipment for guided missile Vertical Launch well (2) and peripheral protective protection structure (3)；
On the upper-deck cabin top surface of platform main nacelle (1), the peripheral protective around guided missile Vertical Launch well (2) protects structure (3), installation scene
Integrated generator (4)；On the upper-deck cabin top surface of platform main nacelle (1), on the outside of wind and solar integrated generator (4), installation periphery
It protects protective cradle (5)；On the top end face of peripheral protective protective cradle (5), install solar energy power generating umbrella (6), in solar energy
On the center of photovoltaic power generation umbrella (6), guided missile Vertical Launch well head (7) and hole cover (8) are set；In peripheral protective protective cradle
(5) on lateral surface, distributed pressure solar or lunar halo (9) of layering installation and air expand injector (10)；In the outside of platform main nacelle (1)
On facade, installation door (11) and window (12), above and below the door (11) of platform main nacelle (1) and the interval position of window (12), distribution
Formula installs solar energy power generating flying wing (13)；On the bottom surface of MISSILE LAUNCHING control cabin (14), MISSILE LAUNCHING is set
Wake flame sprays drain port (15) and wake flame spray drain port lid (16)；Under the bottom on-deck of platform main nacelle (1), controlled around MISSILE LAUNCHING
Cabin (14), landing-gear (17) are played on the land of distributed installation platform VTOL and the water surface plays landing-gear (18), composition
The wind and solar integrated new energy guided missile vertical air flat pad of one barrel shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810169609.XA CN110174025A (en) | 2018-02-20 | 2018-02-20 | A kind of wind and solar integrated new energy guided missile vertical air flat pad |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810169609.XA CN110174025A (en) | 2018-02-20 | 2018-02-20 | A kind of wind and solar integrated new energy guided missile vertical air flat pad |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110174025A true CN110174025A (en) | 2019-08-27 |
Family
ID=67688918
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810169609.XA Pending CN110174025A (en) | 2018-02-20 | 2018-02-20 | A kind of wind and solar integrated new energy guided missile vertical air flat pad |
Country Status (1)
| Country | Link |
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| CN (1) | CN110174025A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113525696A (en) * | 2021-06-02 | 2021-10-22 | 南昌市周静新能源有限公司 | Integrative new forms of energy unmanned aerial vehicle of scene |
| SE545295C2 (en) * | 2022-07-20 | 2023-06-20 | Elevated Launch AB | A wind power plant nacelle configured to enabling a missile launch platform to be mounted to said wind power plant nacelle, and a method for mounting a missile launch platform to a wind power plant nacelle |
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| CN201382739Y (en) * | 2009-03-10 | 2010-01-13 | 张辉 | Rocket launcher |
| US7861973B1 (en) * | 2008-04-01 | 2011-01-04 | Gaylord Olson | Wind responsive power generation system |
| CN105173106A (en) * | 2015-09-18 | 2015-12-23 | 上海长语信息科技有限公司 | External power source electric aircraft aerial platform launching method and device |
| CN204988031U (en) * | 2015-09-18 | 2016-01-20 | 邱玉燕 | Platform is launched in air to electronic aircraft of external power source |
| US20170146317A1 (en) * | 2014-06-19 | 2017-05-25 | Lockheed Martin Corporation | Launching aerial devices |
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2018
- 2018-02-20 CN CN201810169609.XA patent/CN110174025A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7861973B1 (en) * | 2008-04-01 | 2011-01-04 | Gaylord Olson | Wind responsive power generation system |
| CN201382739Y (en) * | 2009-03-10 | 2010-01-13 | 张辉 | Rocket launcher |
| US20170146317A1 (en) * | 2014-06-19 | 2017-05-25 | Lockheed Martin Corporation | Launching aerial devices |
| CN105173106A (en) * | 2015-09-18 | 2015-12-23 | 上海长语信息科技有限公司 | External power source electric aircraft aerial platform launching method and device |
| CN204988031U (en) * | 2015-09-18 | 2016-01-20 | 邱玉燕 | Platform is launched in air to electronic aircraft of external power source |
Non-Patent Citations (1)
| Title |
|---|
| 杨华保等: "空中发射及其关键技术", 《火力与指挥控制》 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113525696A (en) * | 2021-06-02 | 2021-10-22 | 南昌市周静新能源有限公司 | Integrative new forms of energy unmanned aerial vehicle of scene |
| SE545295C2 (en) * | 2022-07-20 | 2023-06-20 | Elevated Launch AB | A wind power plant nacelle configured to enabling a missile launch platform to be mounted to said wind power plant nacelle, and a method for mounting a missile launch platform to a wind power plant nacelle |
| SE2230244A1 (en) * | 2022-07-20 | 2023-06-20 | Elevated Launch AB | A wind power plant nacelle configured to enabling a missile launch platform to be mounted to said wind power plant nacelle, and a method for mounting a missile launch platform to a wind power plant nacelle |
| WO2024019645A1 (en) * | 2022-07-20 | 2024-01-25 | Elevated Launch AB | A wind power plant nacelle configured to enabling a missile launch platform to be mounted to said wind power plant nacelle, and a method for mounting a missile launch platform to a wind power plant nacelle |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190827 |
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| WD01 | Invention patent application deemed withdrawn after publication |