CN104742673A - Amphibious air and space helicopter - Google Patents
Amphibious air and space helicopter Download PDFInfo
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- CN104742673A CN104742673A CN201510099214.3A CN201510099214A CN104742673A CN 104742673 A CN104742673 A CN 104742673A CN 201510099214 A CN201510099214 A CN 201510099214A CN 104742673 A CN104742673 A CN 104742673A
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Abstract
The invention discloses an amphibious air and space helicopter. The amphibious air and space helicopter comprises a rhombic helicopter body, a hexagonal-column-shaped cabin is arranged in the middle of the helicopter body, wheel-shaped electromagnetic driving propeller units are arranged in triangular main wing planar limiting air and space circles on the two sides of the cabin and rotationally installed on a left point and a right point, the bottom of the cabin is in the shape of a flat boat, a vertical reinforcing and stabilizing wing is longitudinally arranged in the middle of each triangular main wing limiting air and space circle in an up-and-down mode, an air round type wheel-shaped electromagnetic driving propeller unit front and back adjusting rail is arranged in the planar center of each vertical reinforcing and stabilizing wing, a front helicopter head and a rear helicopter head are provided with butt joint type cabin doors, the inner walls of annular hollow columns of the wheel-shaped electromagnetic driving propeller units are provided with two sets of annular electromagnetic driving systems which horizontally correspond to an upper propeller wing electromagnet winding and a lower propeller wing electromagnet winding of the wheel-shaped electromagnetic driving propeller units, propellers are installed in the center of an upper fixing frame and in the center of a lower fixing frame through middle shafts, the upper fixing frame is provided with an auxiliary driving reinforcing ring, a counter-rotation deceleration type power generator is arranged on the butt joint of the middle shafts, a rocket jet engine opening is formed in the back of each wing of the lower propellers, and the engine openings horizontally correspond to the bottom faces of the rear wings and resistance increasing lift force pieces.
Description
Technical field:
The present invention relates to a kind of dual-use amphibious empty sky helicopter.
Background technology:
Slow, the manned few power consumption of existing helicopter speed is large, flying height low wing requirement of strength high frangibility, and adaptive capacity scope is little, dangerous instability.
Summary of the invention:
A kind of structure is the invention provides simple in order to solve the problem, design ingenious maneuverability, safety and comfort energy-conserving and environment-protective, and can in surface navigation and stop, more can roam with limitless ultraspeed space-ward, and the butt joint type cabin door multi rack docking of head is connected before and after utilizing, as train, utilizes wherein a frame or multi rack to start reach the fly able object of joint, utilize the angular adjustment of colyliform Electromagnetic Drive screw propeller unit in spacing sky circle to realize flexible direction controlling.
The present invention is realized by technical scheme below:
The present invention amphibious empty sky helicopter comprises: rhombus body, centre is cabin body, cabin is as hexagonal column, level triangle host wing is respectively had in the middle of body both sides, cabin, elevating plane is slided at triangle host wing rear portion, both sides level triangle host wing planar central is spacing sky circle, colyliform Electromagnetic Drive screw propeller unit is had in spacing sky circle, about colyliform Electromagnetic Drive screw propeller unit, 2 can be rotated installation in front and back, triangle host wing spacing Kong Yuan center, both sides is longitudinally vertically interleaving up and down strengthening vertical stabilizer, strengthening vertical stabilizer and level triangle dominant shape wing spacing Kong Yuan intersection rotate before and after empty round type colyliform Electromagnetic Drive screw propeller unit to adjust track, there is line of travel control flaps at strengthening vertical stabilizer rear portion, both sides, water surface stabilizing float is arranged at strengthening vertical stabilizer bottom, there is horizontal auxiliary wing on strengthening vertical stabilizer top is connected with body, cabin, before and after the body of hexagonal column cabin, head respectively has butt joint type cabin door.
Colyliform Electromagnetic Drive screw propeller unit by inside annular post jamb and its upper and lower two groups by magnet (adjacent heteropole) one by one or electromagnet winding with below it or upper and lower two be attached thereto two groups of annular electromagnetic driving systems that touch article or powered touch article form and isometric the two poles of the earth power, with two groups of annular electro Magnetic driving system levels to there being two groups of helicopter screw propellers, windmill wings sheet is fan-shaped, every sheet wing top taper by one group of magnet or electromagnet winding with its below or different four power supply contacts of its upper and lower two arrays of electrodes or two to touch by electric contact and annular electro Magnetic driving system level and jointly form main drive system, there is increasing resistance lift sheet every sheet wing bottom, every sheet wing back of the body upper level of the one group of helicopter screw propeller in bottom is equipped with one or several rocket jet driving engine mouths (or other kinetic energy surge mouth), the horizontal saliva of driving engine mouth is flat corresponding after it bottom one group of wing and increase resistance lift sheet, two groups of helicopter screw propellers respectively utilize axis and its upper and lower two groups of fixed mount centres to rotate and install, fixed mount is fixedly connected with annular post jamb, often organize pars infrasegmentalis in the fixed mount above helicopter screw propeller and have that annular is auxiliary drives ring stiffener, the top, every sheet windmill wings stage casing that ring stiffener is corresponding have one group of electromagnet winding from or different four power supply contacts of upper and lower two arrays of electrodes or two by electric contact, ring stiffener by magnet (adjacent heteropole) one by one or electromagnet winding with its above or upper and lower to be connected and the annular that forms of isometric two power supply touch articles or powered touch article is auxiliary drives ring stiffener drive system at the two poles of the earth with it, two groups of screw propeller axis joints have brake deceleration function to turning slowdown type electrical generator, screw propeller axis lower end, top is equipped with stator positive dirction and is rotated, there is rotor lower part helical oar axis upper end, rotor reverses in the stator, utilize when amphibious empty sky helicopter slows down or land turning the generating of slowdown type generator operation for battery charge is to reach the effect of energy-saving power generation.
The present invention amphibious empty sky helicopter has following technological merit: colyliform Electromagnetic Drive screw propeller unit utilize two groups of magnet (adjacent heteropole) in the annular electromagnetic driving system inside annular post jamb or electromagnet winding with below it the mobile pole-changing formula electromagnet winding of the isometric with it and powered touch article be connected of upper and lower two or disjunct power supply touch article and corresponding windmill wings top taper or immobilize formula electromagnet winding and below it or upper and lower two of being attached thereto by electric contact or different four power supply contacts of disjunct two arrays of electrodes are corresponding touches energising, these two groups of electromagnet windings are made to produce two kinds of electromagnet windings with wing top tip electromagnet winding magnetic pole same pole propelling thrust phase heteropole motive force, the magnetic pole of the electromagnet winding of annular electromagnetic driving system changes with the mobile change of wing (or annular drive system is the alnico magnets of adjacent not homopolarity, often organize below alnico magnets or upper and lower two power supply touch article with below the taper electromagnet winding of corresponding wing top or upper and lower two to be energized by electric contact and to make top taper electromagnet winding produce one group of permanent magnetic magnetic pole iron identical generation propelling thrust in the annular drive system of magnetic pole and corresponding angle and inhale power with different generation of the permanent magnetic magnetic pole iron in front, wing top taper electromagnet winding magnetic pole with the mobile change of wing change and identical with the permanent magnetic magnetic pole iron in the annular drive system of corresponding angle) lower part helical oar driving principle is identical with top screw propeller type of drive, just electrode direction is different, wing top taper electromagnet is different from the electromagnet corresponding angle of annular drive system, and make lower part helical oar rotation direction contrary with propeller rotational direction, top, often organize screw propeller top fixed mount has and auxiliaryly drive ring stiffener, auxiliaryly drive ring stiffener and there is electromagnet winding in corresponding windmill wings stage casing, auxiliary ring stiffener type of drive of driving is identical with principle and annular main drive systems mode and identical with corresponding propeller rotational direction, the most innovative is that lower part helical oar every sheet wing back portion is equiped with several rocket jet driving engine mouths (or other energy substance injection orifice), the horizontal saliva of driving engine mouth is put down after correspondence and is produced superpower promotion rotational force and certainly push to lift resistance bottom one group of wing with on the increasing resistance lift sheet of bottom.
Helicopter cabin, amphibious empty sky body is designed to hexagonal column, make to be flat boat bottom helicopter cabin, amphibious empty sky, drop in water surface and navigation can be conducive to, water surface stabilizing float is respectively equipped with in the strengthening vertical stabilizer bottom of both sides, cabin, floating drum is conducive to body and keeps balance at the water surface and stablize, before and after amphibious empty sky helicopter, head respectively has butt joint type cabin door mutually to dock the function in energy-conservation flight and turnover cabin before and after multi rack aircraft, both sides annular electro magnetic driving helical oar unit is utilized in triangle host wing spacing sky circle, before and after the empty round type unit of strengthening vertical stabilizer, to adjust track simultaneously or do separately the front and back rotation of front and back 360 deg angle, aircraft is made to reach the flexible function of advancing and rising and retreating and turn
Respectively there is one group of level triangle host wing helicopter fuselage both sides, amphibious empty sky, colyliform Electromagnetic Drive screw propeller unit 2, left and right in level triangle host wing realizing middle limiting sky circle can be installed in front and back rotation, the while that colyliform Electromagnetic Drive screw propeller unit adjusting in track in level triangle host wing realizing middle limiting sky circle before and after the empty round type unit of perpendicular up and down with it strengthening vertical stabilizer plane or do separately before and after 360 deg and rotate, to move forward and backward the function of left and right turn and lifting to reach aircraft, level triangle host wing rear portion have manually and automatically combine slide the elevating control wing, the line of travel control flaps that strengthening vertical stabilizer rear portion has manually and automatically combines, the function sliding the elevating control wing and line of travel control flaps is the safety and stability function controlling the horizontal heading of aircraft and height under aircraft stops power driven state, the line of travel control flaps of strengthening vertical stabilizer also can control the direction controlling of aircraft water face navigation, oval shape surface buoy is respectively had below the strengthening vertical stabilizer of both sides, be beneficial to the stability of aircraft surface navigation, two groups of horizontal auxiliary wings are arranged at strengthening vertical stabilizer top, both sides, horizontal auxiliary wing is connected with body, cabin, the raising force effect of amphibious empty sky helicopter is jointly increased with the intensity and triangle horizontal wings of reinforcing strengthening vertical stabilizer, the present invention has substance and progressive for prior art, the present invention specifically utilizes the best mode of several prior art after brand-new combination, aircraft is made to be more conducive to manual control, recycling economize energy, make it have maneuverability, safety and comfort, the advantage of wide adaptability, break the limitation of traditional single flying method.
Accompanying drawing illustrates:
Below in conjunction with the drawings and specific embodiments, the present invention is further illustrated.
Fig. 1 is the upper and lower birds-eye view of amphibious empty sky helicopter (the horizontal slave wing omits).
Fig. 2 is amphibious empty sky helicopter lateral plan.
Fig. 3 is head front view before and after amphibious empty sky helicopter.
Fig. 4 is the side annular drive magnetic winding of the technology of the present invention and the hollow pillar wall circular electromagnetic driving system schematic diagram of power supply or powered touch article composition.
Fig. 5 is colyliform Electromagnetic Drive screw propeller unit sectional side view of the present invention
Fig. 6 is the upper and lower fixed mount of the technology of the present invention annular electro magnetic driving helical oar unit internal propeller and auxiliaryly drives ring stiffener schematic diagram.
Fig. 7 is that top of the present invention rotates forward the auxiliary increasing resistance lift sheet schematic diagram driving electromagnet winding and four power or be subject to electric contact and wing behind portion's rocket jet driving engine mouth and bottoms of windmill wings and bottom contrary turning propeller wing drive magnetic winding and wing stage casing.
Fig. 8 is ring stiffener electromagnetic driving system of the present invention and electromagnet winding and powered touch article schematic diagram.
Fig. 9 is the positive rotating propeller birds-eye view in top of the present invention.
Figure 10 bottom of the present invention contrary turning propeller birds-eye view.
Detailed description of the invention:
A kind of amphibious empty sky helicopter comprises as shown in the figure, rhombus body 1, cabin body 2 is hexagonal column, respectively there is level triangle host wing 3 cabin body 2 both sides, the elevating control wing 4 is slided at level triangle host wing 3 rear portion, level triangle host wing planar central is spacing sky circle 5, in spacing sky circle 5,2, left and right is rotatablely equipped with colyliform Electromagnetic Drive screw propeller unit 6, colyliform Electromagnetic Drive screw propeller unit 6 does individually or simultaneously before and after 360 deg and rotates in the spacing sky circle 5 of level triangle host wing plane, in order to gesture stability during adjustment flight, both sides level triangle host wing 3 plane spacing sky circle 5 centers are parallel with before and after cabin body 2 and have strengthening vertical stabilizer 7 perpendicular to host wing 3 up and down, there is line of travel control flaps 8 at strengthening vertical stabilizer 7 rear portion, strengthening vertical stabilizer 7 vertical plane surface center is regulate dragging track 25 before and after empty round type colyliform Electromagnetic Drive screw propeller unit 6, strengthening vertical stabilizer 7 plane sky circle dragging track 25 is vertically intersected on level triangle host wing and the spacing sky circle of plane 5 upper and lowers, stability during in order to reinforce the intensity of triangle host wing 3 and to control colyliform Electromagnetic Drive screw propeller unit 6 adjustment direction and upper and lower 2 reinforcement effects, horizontal auxiliary wing 9 is arranged at strengthening vertical stabilizer 7 top, horizontal auxiliary wing 9 is connected with cabin body 2, in order to increase the intensity of strengthening vertical stabilizer 7, oval shape water surface stabilizing float 10 is arranged at strengthening vertical stabilizer 7 bottom, water surface stabilizing float 10 is utilized to make amphibious empty sky helicopter be increased in the left and right stability of the water surface when drop in water surface stops or navigate by water, front and back head has butt joint type cabin door 26 for the front and back of multi rack amphibious empty sky helicopter mutually to connection function.
Colyliform Electromagnetic Drive screw propeller unit 6 is by two groups of annular electromagnetic driving systems upper and lower in the annular post jamb of scheme 1 22, the positive rotating propeller 11 in the top corresponding with this system level and bottom contrary turning propeller 12, upper and lower screw propeller utilizes fixing rotation the in fixed mount 24 center of axis 19 and the fixed mount 23 above it and below to install, in the fixed mount 23 of top, pars infrasegmentalis has and auxiliaryly drives ring stiffener 15, every sheet wing 17 of screw propeller pushes up the electromagnet winding 13 of taper and two groups of electromagnet windings 14 in the annular electromagnetic driving system on corresponding hollow post jamb 22, by below wing top tip electromagnet winding 13 or four power supply contact AB of upper and lower, below the electromagnet winding 14 that BA is corresponding with the annular electromagnetic driving system of hollow post jamb 22 or the powered touch article XY of upper and lower two, after in electromagnetic driving system, two groups of electromagnet windings 14 are energized, produce the poles repel thrust identical with wing top taper electromagnet winding 13, and become the circulation driving principle of heteropole magnet phase suction with anterior one group of electromagnet winding 14, electromagnet winding 14 in annular electromagnetic driving system changes with the mobile change of corresponding wing 17, several are had to increase resistance lift sheet 18 bottom every sheet wing 17.Scheme 2 annular drive system be the magnet 14 of adjacent heteropole and its below or upper and lower two power supply touch article XY, below adjacent magnets 14 or upper and lower be YX two groups power touch article composition annular magnetic drive system, they are separately below magnet 14 or below two power supply touch article XY of upper and lower and wing top taper electromagnet windings 13 or after upper and lower two powered contact A B are energized, produce and corresponding annular electro Magnetic driving system magnet 14 homopolar-repulsion power, and be subject to the suction of adjacent heteropole magnet 14 simultaneously, wing top tip electromagnet winding 13 is changing into mobile change with opposed magnet 14 as homopolarity and circulating drives, several are had to increase resistance lift sheet 18 bottom every sheet wing 17, upper and lower screw propeller utilizes axis and above it, fixed mount 24 central rotation of fixed mount 23 and below is installed, in the fixed mount 23 of top, pars infrasegmentalis has and auxiliaryly drives ring stiffener 15, assistive drive ring stiffener 15, electromagnet winding 13 and four power supply contact AB are arranged at corresponding top, windmill wings stage casing, BA or two powered contact A B, assistive drive ring stiffener 15 type of drive is identical with annular electromagnetic driving system with principle, and it is identical with corresponding propeller rotational direction.
The high-altitude power of the present invention amphibious empty sky helicopter is that in colyliform hollow pillar 22, rocket jet driving engine mouth 16 is equipped with in the every sheet wing 17 behind portion of bottom contrary turning propeller 12, the airflow of rocket jet driving engine mouth 16 ejection makes lower part helical oar 12 hyper-speed rotate, the airflow horizontal-jet that sprays of rocket jet driving engine mouth 16 to the bottom surface of one group of wing 17 below and the increasing resistance lift sheet 18 of wing 17 bottom surface produces superpower rotational force and blowing raising force simultaneously and makes amphibious empty sky helicopter utilize blowing raising force infinitely to accelerate to fly and do not fly by the constant promotion of restriction of flying speed in the environment of high-altitude or space rarefaction of air or vacuum.
The present invention amphibious empty sky upper and lower screw propeller joint of helicopter has deceleration counter rotating type power generator, axis 19 lower end of the positive rotating propeller 11 of colyliform hollow pillar 22 internal upper part has generator unit stator 20 to rotate forward together with top screw propeller 11, rotor 21 is contained in the opposite spin in stator 20 of bottom contrary turning propeller 12 axis 19 upper end, utilizes slowdown type to forwarding electric power generation for battery charge is to reach the object of fall-retarding and energy-saving power generation when amphibious empty sky helicopter slows down or land.
Finally should be noted that above embodiment is only not intended to limit with reference to detailed description of the present invention for illustration of technical scheme of the present invention; still can modify to the specific embodiment of the present invention or replace on an equal basis portion of techniques feature and do not depart from the spirit of the present invention program, it all should be encompassed within the technical scheme scope of Patent request of the present invention protection.
Claims (4)
1. an amphibious empty sky helicopter comprises: rhombus body, be hexagonal column cabin in the middle of rhombus body, level triangle host wing is respectively had in the middle of both sides, cabin, elevating plane is slided at triangle host wing rear portion, level triangle wingpiston centered finite position, both sides sky circle, colyliform Electromagnetic Drive screw propeller unit 2, left and right in spacing sky circle can be installed in front and back rotation, strengthening vertical stabilizer is had with level triangle host wing top-bottom cross is perpendicular with level triangle host wing spacing Kong Yuan center, strengthening vertical stabilizer is parallel with before and after cabin, strengthening vertical stabilizer plane and the spacing Kong Yuan intersection of level triangle host wing have before and after the empty round type of colyliform Electromagnetic Drive screw propeller unit and regulate dragging track, there is line of travel control flaps at strengthening vertical stabilizer rear portion, there is horizontal auxiliary wing on strengthening vertical stabilizer top is connected with body top, cabin, water surface stabilizing float is arranged at strengthening vertical stabilizer bottom, cabin head is respectively had before and after the body of hexagonal column cabin, cabin, front and back head respectively has butt joint type cabin door.
2. according to claim 1: have colyliform Electromagnetic Drive screw propeller unit in the spacing sky circle of body both sides, helicopter cabin, amphibious empty sky level triangle host wing, colyliform Electromagnetic Drive screw propeller is characterized in that its profile is colyliform open column shape.
Scheme 1: in hollow post jamb up and down by two by one by one independently electromagnet winding with its below or upper and lower two be connected and the annular electromagnetic driving system that forms of the powered touch article that electromagnet winding body is isometric with it at the two poles of the earth with it, in hollow pillar, there is positive rotating propeller top, contrary turning propeller is arranged at bottom, two groups of screw propeller every sheet wing top tapers have one group of invariant electromagnet winding, invariant electromagnet winding is corresponding with two groups of electromagnet winding levels in the annular drive system in corresponding hollow post jamb, below the taper electromagnet winding of wing top or upper and lower four power supply contacts having two arrays of electrodes contrary, power supply contact respectively with below two groups of electromagnet windings in corresponding hollow pillar wall circular electromagnetic driving system or two positive and negative powered touch articles of upper and lower touch mutually, wing top taper electromagnet winding magnetic pole is constant, in corresponding annular electromagnetic driving system, two groups of electromagnet winding magnetic poles move change with wing and change circulation driving, two groups of screw propellers are had in hollow pillar, windmill wings is fan-shaped, several are had to increase resistance lift sheet bottom wing, the rocket jet driving engine mouth that lower part helical oar every sheet wing back side has several levels to install, the horizontal saliva of rocket jet driving engine mouth is put down on the bottom surface of the one group of wing in corresponding rear portion and the increasing resistance lift sheet of wing bottom surface, two groups of fixed mount centres that upper and lower two groups of screw propellers utilize axis to be arranged on respective screw propeller upper and lower rotate installs, fixed mount and hollow post jamb are fixedly connected, upper and lower screw propeller axis joint has slowdown type to forwarding motor, often assistive drive ring stiffener is arranged at the fixed mount bottom organized above screw propeller, one group of electromagnet winding and power supply contact are respectively arranged at the wing stage casing top corresponding with fixed mount ring stiffener, the driving principle of ring stiffener is identical with screw propeller driving principle and identical with corresponding screw propeller driving direction.
Scheme 2 respectively has one in hollow post jamb up and down by the magnet of independent adjacent heteropole one by one, with below magnet or the annular magnetic drive system of the positive and negative power supply touch article composition of isometric with it two of upper and lower, in hollow pillar, top is positive rotating propeller, bottom is contrary turning propeller, screw propeller every sheet wing top taper has one group of pole-changing formula electromagnet winding, pole-changing formula electromagnet winding is corresponding with one group of magnet level in the annular magnetic drive system on corresponding hollow post jamb, below the taper electromagnet winding of wing top or upper and lower two be with it connected two, the two poles of the earth by electric contact, by below the magnet in electric contact and respective annular Magnetic driving system or two touch articles of powering of upper and lower touch powered, the invariant magnet of the adjacent heteropole of annular magnetic drive system magnet, the magnetic pole of the pole-changing formula electromagnet winding of wing top taper moves change with wing and is changing into the magnetic pole electromagnet identical with the magnetic pole of the magnet in the annular magnetic drive system of respective angles, two groups of screw propellers are had in hollow pillar, wing is fan-shaped, several are had to increase resistance lift sheet bottom wing, the rocket jet driving engine mouth that lower part helical oar every sheet wing back side has several levels to install, the horizontal saliva of rocket jet driving engine mouth puts down the bottom surface of the one group of wing in corresponding rear portion and the increasing resistance lift sheet of wing bottom surface, two groups of screw propellers utilize axis to be arranged on respective upper and lower two groups of fixed mount centres, upper and lower screw propeller axis joint has slowdown type to forwarding motor, fixed mount and hollow post jamb are fixedly connected, often organize below the fixed mount above screw propeller and have assistive drive ring stiffener, there are one group of electromagnet winding and two in the wing stage casing corresponding with fixed mount ring stiffener by electric contact, the driving principle of ring stiffener is identical with the driving principle of screw propeller and identical with corresponding screw propeller driving direction.
3. according to claim 2: there are several rocket jet driving engine mouths at every sheet wing back of lower part helical oar, the horizontal saliva of rocket jet driving engine mouth puts down the bottom surface of one group of wing after correspondence and the increasing resistance lift sheet of wing bottom surface, and common composition high-altitude or space are from pushing away drive system.
4. according to claim, amphibious empty sky helicopter is characterized in that, in colyliform hollow pillar, upper and lower two groups of screw propeller axis joints have slowdown type to forwarding motor, stator is arranged on positive rotating propeller axis lower end, top, rotor is arranged on contrary turning propeller axis upper end, bottom and opposite spin in the stator, utilizes it to play the function of slowing-down brake and generating when amphibious empty sky helicopter slows down or land.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510099214.3A CN104742673A (en) | 2015-03-09 | 2015-03-09 | Amphibious air and space helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510099214.3A CN104742673A (en) | 2015-03-09 | 2015-03-09 | Amphibious air and space helicopter |
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| Publication Number | Publication Date |
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| CN104742673A true CN104742673A (en) | 2015-07-01 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510099214.3A Pending CN104742673A (en) | 2015-03-09 | 2015-03-09 | Amphibious air and space helicopter |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201646288U (en) * | 2010-05-24 | 2010-11-24 | 付帮勤 | Combined multifunctional rescue boat |
| CN102897315A (en) * | 2011-07-29 | 2013-01-30 | 奥格斯塔韦斯兰股份公司 | Convertiplane |
| CN103158880A (en) * | 2013-03-04 | 2013-06-19 | 陆建收 | Aerospace motor-driven helicopter |
| CN103640445A (en) * | 2013-12-18 | 2014-03-19 | 江苏科技大学 | Amphibious unmanned vehicle with front-mounted double bodies on inclined sides and three bodies on water surface |
| CN103640444A (en) * | 2013-12-18 | 2014-03-19 | 江苏科技大学 | Amphibious unmanned surface boat provided with double bodies on inclined sides |
-
2015
- 2015-03-09 CN CN201510099214.3A patent/CN104742673A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201646288U (en) * | 2010-05-24 | 2010-11-24 | 付帮勤 | Combined multifunctional rescue boat |
| CN102897315A (en) * | 2011-07-29 | 2013-01-30 | 奥格斯塔韦斯兰股份公司 | Convertiplane |
| CN103158880A (en) * | 2013-03-04 | 2013-06-19 | 陆建收 | Aerospace motor-driven helicopter |
| CN103640445A (en) * | 2013-12-18 | 2014-03-19 | 江苏科技大学 | Amphibious unmanned vehicle with front-mounted double bodies on inclined sides and three bodies on water surface |
| CN103640444A (en) * | 2013-12-18 | 2014-03-19 | 江苏科技大学 | Amphibious unmanned surface boat provided with double bodies on inclined sides |
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