CN211167368U - Transportation airship convenient to descend in complex environment - Google Patents

Transportation airship convenient to descend in complex environment Download PDF

Info

Publication number
CN211167368U
CN211167368U CN201920900015.1U CN201920900015U CN211167368U CN 211167368 U CN211167368 U CN 211167368U CN 201920900015 U CN201920900015 U CN 201920900015U CN 211167368 U CN211167368 U CN 211167368U
Authority
CN
China
Prior art keywords
gripper
airship
fixedly connected
transportation
complex environment
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201920900015.1U
Other languages
Chinese (zh)
Inventor
不公告发明人
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Meng Guanghong
Original Assignee
Meng Guanghong
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Meng Guanghong filed Critical Meng Guanghong
Priority to CN201920900015.1U priority Critical patent/CN211167368U/en
Application granted granted Critical
Publication of CN211167368U publication Critical patent/CN211167368U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Buffer Packaging (AREA)

Abstract

The utility model discloses a transportation airship convenient to land under complex environment, which comprises an airship main body, a balance empennage, an engine nacelle, an air cabin and a control nacelle, wherein the airship is suspended firstly when the transportation airship flies under severe environment and needs to convey goods at a specified position by the matching operation mode of a first grab, a second grab, a third grab, a fourth grab and an air cylinder, the rotating shaft is driven by a rotating motor to rotate anticlockwise so as to put down a contraction rope and a protective shell together, the surrounding environment is observed by an infrared camera on the outer surface of the protective shell, a container is conveniently found by a fixing device, the air cylinder is opened by a controller, the first grab, the second grab, the third grab and the fourth grab are opened, fixed clamping grooves around the outer surface of the container are grasped, and an electromagnetic lock is used for adsorbing an iron plate at the top of the container, the cargo can be quickly loaded and transported, the conveying efficiency of the flying body is effectively improved, and the method is suitable for wide popularization.

Description

Transportation airship convenient to descend in complex environment
Technical Field
The utility model belongs to the technical field of the transportation dirigible, specifically be a transportation dirigible convenient to descend under the complex environment.
Background
An airship is a lighter-than-air craft that differs from a hot-air balloon in having means to propel and control the flight conditions. The airship consists of a huge streamline hull, a nacelle positioned below the hull, a tail surface with a stabilizing control function and a propelling device, wherein buoyancy gas with density smaller than that of air is filled in an air bag of the hull to generate buoyancy force to lift the airship. The gondola is used for passengers to take and load cargo. The tail surface is used for controlling and maintaining the stability of course and pitching. The large civil airship can also be used for transportation, entertainment, disaster relief, film and television shooting, scientific experiments and the like. For example, when a natural disaster occurs, a communication interruption can quickly launch an aerostat, and the mobile communication recovery of the whole disaster area can be completed in a very short time by carrying a communication transponder through a floating balloon.
However, the existing airship has disadvantages, for example, the existing airship has disadvantages of light weight and large volume, and when a geological disaster occurs, the existing airship encounters severe weather in the transportation process, so that the airship is inconvenient to land to rapidly transport goods or ship goods, and thus disaster relief materials are difficult to transport to corresponding positions.
Disclosure of Invention
The utility model aims to provide a: in order to solve the problems, the transportation airship convenient to descend in a complex environment is provided.
The utility model adopts the technical scheme as follows:
a transportation airship convenient to land under a complex environment comprises an airship main body, a balance empennage, an engine nacelle, an air cabin and a control nacelle, wherein the balance empennage is fixedly connected to the tail of the airship main body, a mooring cone is fixedly connected to the head of the airship main body, the control nacelle is fixedly connected to the bottom of the head of the airship main body, the engine nacelle is fixedly connected to the bottom of the tail of the airship main body, the air cabin is arranged inside the middle end of the airship main body, a rotating motor is fixedly connected to both ends inside the airship main body, a transmission shaft is fixedly connected to the end of the rotating motor, a contraction rope is fixedly wound on the outer surface of the transmission shaft, one end of the contraction rope is fixedly connected with a protective shell, the protective shell comprises a protective flap and a fixed plate, the protective flap is arranged around the bottom of the protective shell, and a connector is fixedly connected to the middle end, the bottom fixedly connected with fixing device of fixed plate, fixing device includes connecting plate, controller, first tongs, cylinder, second tongs, third tongs, fourth tongs and electromagnetic lock, first tongs, second tongs, third tongs and fourth tongs pass through connecting plate and fixed plate fixed connection, be provided with the controller between the top of first tongs, second tongs, third tongs and fourth tongs, the equal fixedly connected with cylinder in top of first tongs, second tongs, third tongs and fourth tongs, the bottom fixedly connected with electromagnetic lock of connecting plate, the bottom of electromagnetic lock is provided with the packing box.
The protective petals are petal-shaped structures, the number of the protective petals is four, the end portions of the four protective petals are closed to form a conical structure, and the wide head ends of the protective petals are hinged to the bottom edge of the protective shell through spring hinges.
The top of the fixed plate is fixedly connected with the contraction rope through a connector, the fixed plate is of a square hollow bottom opening structure, and the fixed plate is made of polyethylene.
The wire arranging grooves are formed in two sides of the interior of the contraction rope, a transmission line is arranged on one side of the wire arranging groove in the interior of the contraction rope, and a tension line is arranged on the other side of the wire arranging groove in the interior of the contraction rope.
Wherein, a gasket is filled between the tension line and the transmission line and between the transmission line and the flat cable groove, and the gasket is made of a soft steel wire mesh.
The first gripper and the third gripper are distributed relatively, the second gripper and the fourth gripper are distributed relatively, and the first gripper, the second gripper, the third gripper and the fourth gripper are distributed in a petal type structure.
The outer surface of the protective flap is provided with an infrared camera, and the model of the infrared camera is EH 414C-120.
The output end of the controller is electrically connected with the input end of the air cylinder, and the input end of the controller is electrically connected with the output end of the infrared camera.
The top of the container is fixedly connected with an iron plate, and the periphery of the outer surface of the container is provided with fixing clamping grooves.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
1. in the utility model, through the matching operation mode of the first gripper, the second gripper, the third gripper, the fourth gripper and the cylinder, when the transport airship flies in a severe environment and needs to convey goods at a specified position, the airship is firstly suspended, then the rotating motor is quickly opened, the rotating shaft is driven by the rotating motor to rotate anticlockwise, so that the contraction rope and the protective shell are put down together, the surrounding environment is observed through the infrared camera on the outer surface of the protective shell, a fixing device is convenient to find a fixed position, at the moment, the cylinder is opened through the controller, the first gripper, the second gripper, the third gripper and the fourth gripper are opened, fixed clamping grooves around the outer surface of the container are grasped, the iron plate at the top of the container is adsorbed through the electromagnetic lock, goods can be quickly shipped, when goods on the airship need to be put down, only need to prop open first tongs, the second tongs, third tongs and fourth tongs, grab packing box surface fixed slot all around, rethread electromagnetic lock adsorbs the iron plate at packing box top, open the rotating electrical machines again, drive the axis of rotation through the rotating electrical machines and carry out anticlockwise rotation, thereby put down shrink rope and protective housing together, can put down the goods from the airship, this method can avoid under the complex environment that the airship can't descend and carry the goods, the efficiency of carrying the goods has effectively been improved.
2. The utility model discloses in, through being provided with the protective housing to under the cooperation of shrink rope, when the transportation dirigible takes off, at first controller control cylinder is flexible, retrieves first tongs, second tongs, third tongs and fourth tongs, opens the rotating electrical machines again, with shrink rope upwards shrink, in retracting the protective housing with fixing device, on scraping the fixture when preventing to take off, improve the dirigible security of taking off.
Drawings
FIG. 1 is a schematic view of the overall external structure of the present invention;
fig. 2 is a schematic view of the protective shell of the present invention showing a top-down unfolded structure;
FIG. 3 is an enlarged schematic view of the fixing device of the present invention;
FIG. 4 is a schematic view of the internal cross-sectional structure of the retractable rope of the present invention;
FIG. 5 is a schematic view of the retractable transmission structure of the retractable rope of the present invention;
fig. 6 is a schematic view of the overall structure of the cargo box of the present invention.
The labels in the figure are: 1. an airship body; 2. balancing the tail wing; 3. an engine nacelle; 4. a gas cabin; 5. a protective shell; 6. retracting the cord; 7. maneuvering the pod; 8. a mooring cone; 9. a connector; 10. an infrared camera; 11. a fixing device; 12. a protective flap; 13. a fixing plate; 14. a connecting plate; 15. a controller; 16. a first gripper; 17. a cylinder; 18. a second gripper; 19. a third gripper; 20. a fourth gripper; 21. a gasket; 22. a wire arrangement groove; 23. a transmission line; 24. a tension line; 25. a rotating electric machine; 26. a rotating shaft; 27. an electromagnetic lock; 28. a cargo box; 29. an iron plate; 30. and fixing the clamping groove.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance; furthermore, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, as they may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Example 1
Referring to fig. 1-6, a transportation airship convenient for landing in a complex environment comprises an airship body 1, a balance empennage 2, an engine nacelle 3, an air cabin 4 and a control nacelle 7, wherein the tail of the airship body 1 is fixedly connected with the balance empennage 2, the head of the airship body 1 is fixedly connected with a mooring cone 8, the bottom end of the head of the airship body 1 is fixedly connected with the control nacelle 7, the bottom end of the tail of the airship body 1 is fixedly connected with the engine nacelle 3, the air cabin 4 is arranged in the middle end of the airship body 1, two ends in the airship body 1 are both fixedly connected with a rotating motor 25, the end of the rotating motor 25 is fixedly connected with a transmission shaft 26, a contraction rope 6 is fixedly wound on the outer surface of the transmission shaft 26, one end of the contraction rope 6 is fixedly connected with a protective shell 5, the protective shell 5 comprises a protective flap 12 and a fixed plate 13, the protective flap 12 is arranged around the bottom of the bottom protective shell 5, the middle end of the top of the fixed plate 13 is fixedly connected with a connector 9, the bottom of the fixed plate 13 is fixedly connected with a fixing device 11, the fixing device 11 comprises a connecting plate 14, a controller 15, a first gripper 16, an air cylinder 17, a second gripper 18, a third gripper 19, a fourth gripper 20 and an electromagnetic lock 27, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are fixedly connected with the fixed plate 13 through the connecting plate 14, the controller 15 is arranged between the tops of the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20, the air cylinder 17 is fixedly connected with the tops of the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20, the electromagnetic lock 27 is fixedly connected with the bottom of the connecting plate 14, a container 28 is arranged at the bottom of the electromagnetic lock 27, protection lamella 12 is petal shape structure, protection lamella 12 is provided with four, and the tip of four protection lamellas 12 is closed and is the toper structure, protection lamella 12's wide head end passes through spring hinge with the base of protective housing 5 and articulates, connector 9 and shrink rope 6 fixed connection are passed through at the top of fixed plate 13, fixed plate 13 is square hollow bottom opening structure, fixed plate 13's material is polyethylene, and through fixed plate 13 and protection lamella 12's cooperation mode, can effectively protect fixing device 11, prevents that fixing device from taking place to damage to can prevent that fixing device 11 from taking place to scrape when the diret takes off, cause the influence to the diret.
Example 2
Referring to fig. 1-6, a transportation airship convenient for landing in a complex environment comprises an airship body 1, a balance empennage 2, an engine nacelle 3, an air cabin 4 and a control nacelle 7, wherein the tail of the airship body 1 is fixedly connected with the balance empennage 2, the head of the airship body 1 is fixedly connected with a mooring cone 8, the bottom end of the head of the airship body 1 is fixedly connected with the control nacelle 7, the bottom end of the tail of the airship body 1 is fixedly connected with the engine nacelle 3, the air cabin 4 is arranged in the middle end of the airship body 1, two ends in the airship body 1 are both fixedly connected with a rotating motor 25, the end of the rotating motor 25 is fixedly connected with a transmission shaft 26, a contraction rope 6 is fixedly wound on the outer surface of the transmission shaft 26, one end of the contraction rope 6 is fixedly connected with a protective shell 5, the protective shell 5 comprises a protective flap 12 and a fixed plate 13, the protective flap 12 is arranged around the bottom of the bottom protective shell 5, the middle end of the top of the fixed plate 13 is fixedly connected with a connector 9, the bottom of the fixed plate 13 is fixedly connected with a fixing device 11, the fixing device 11 comprises a connecting plate 14, a controller 15, a first gripper 16, an air cylinder 17, a second gripper 18, a third gripper 19, a fourth gripper 20 and an electromagnetic lock 27, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are fixedly connected with the fixed plate 13 through the connecting plate 14, the controller 15 is arranged between the tops of the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20, the air cylinder 17 is fixedly connected with the tops of the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20, the electromagnetic lock 27 is fixedly connected with the bottom of the connecting plate 14, a container 28 is arranged at the bottom of the electromagnetic lock 27, open the inside both sides of shrink rope 6 has winding displacement groove 22, inside one side winding displacement groove 22 of shrink rope 6 is provided with transmission line 23, the inside opposite side winding displacement groove 22 of shrink rope 6 is provided with the pulling force line 24, it has gasket 21 to fill between pulling force line 24 and transmission line 23 and the winding displacement groove 22, the material of gasket 21 is soft wire net, can conveniently fix a position transmission line 23 and pulling force line 24 through the inside winding displacement groove 22 of shrink rope 6, prevents to take place the winding, and through soft wire net seat cushion, first can consolidate transmission line 23 and pulling force line 24, prevents to rock, and the second can improve transmission line 23 and pulling force line 24's life, prevents that shrink rope 6 from causing the damage transmission line 23 and pulling force line 24 when twining, conveniently provides electric power for electromagnetic lock 27 through transmission line 23, realizes opening and shutting of electromagnetic lock 27.
Example 3
Referring to fig. 1-6, a transportation airship convenient for landing in a complex environment comprises an airship body 1, a balance empennage 2, an engine nacelle 3, an air cabin 4 and a control nacelle 7, wherein the tail of the airship body 1 is fixedly connected with the balance empennage 2, the head of the airship body 1 is fixedly connected with a mooring cone 8, the bottom end of the head of the airship body 1 is fixedly connected with the control nacelle 7, the bottom end of the tail of the airship body 1 is fixedly connected with the engine nacelle 3, the air cabin 4 is arranged in the middle end of the airship body 1, two ends in the airship body 1 are both fixedly connected with a rotating motor 25, the end of the rotating motor 25 is fixedly connected with a transmission shaft 26, a contraction rope 6 is fixedly wound on the outer surface of the transmission shaft 26, one end of the contraction rope 6 is fixedly connected with a protective shell 5, the protective shell 5 comprises a protective flap 12 and a fixed plate 13, the protective flap 12 is arranged around the bottom of the bottom protective shell 5, the middle end of the top of the fixed plate 13 is fixedly connected with a connector 9, the bottom of the fixed plate 13 is fixedly connected with a fixing device 11, the fixing device 11 comprises a connecting plate 14, a controller 15, a first gripper 16, an air cylinder 17, a second gripper 18, a third gripper 19, a fourth gripper 20 and an electromagnetic lock 27, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are fixedly connected with the fixed plate 13 through the connecting plate 14, the controller 15 is arranged between the tops of the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20, the air cylinder 17 is fixedly connected with the tops of the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20, the electromagnetic lock 27 is fixedly connected with the bottom of the connecting plate 14, a container 28 is arranged at the bottom of the electromagnetic lock 27, the first gripper 16 and the third gripper 19 are distributed oppositely, the second gripper 18 and the fourth gripper 20 are distributed oppositely, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are distributed in a petal type structure, the infrared camera 10 is arranged on the outer surface of the protection petal 12, the model of the infrared camera 10 is EH414C-120, the output end of the controller 15 is electrically connected with the input end of the air cylinder 17, the input end of the controller 15 is electrically connected with the output end of the infrared camera 10, the iron plate 29 is fixedly connected to the top of the cargo box 28, the fixed clamping grooves 30 are formed around the outer surface of the cargo box 28, fixable position information is transmitted to the controller 15 through the infrared camera 10, the airship adjusts the position through manipulating the pod 7, the rotating shaft 26 is driven by the rotating motor 25 to rotate anticlockwise, so that the contraction rope 6 and the protection shell 5 are put down together, the surrounding environment is observed through the infrared camera 10 on the outer surface of the protective shell 5, the fixing device can conveniently find the position of the container 28, at the moment, the air cylinder 17 is opened through the controller 15, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are opened to grip the fixed clamping groove 30 on the periphery of the outer surface of the container 28, the iron plate 29 on the top of the container 28 is adsorbed through the electromagnetic lock 27, finally, the rotating shaft 26 is driven by the rotating motor 25 to rotate clockwise, the container 28 is pulled into the airship, the cargo can be quickly shipped, when the cargo on the airship needs to be put down, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are only required to be opened to grip the fixed clamping groove 30 on the periphery of the outer surface of the container 28, the iron plate 29 on the top of the container 28 is adsorbed through the electromagnetic lock 27, and then the rotating motor 25 is opened, the rotating shaft 26 is driven to rotate anticlockwise through the rotating motor 25, so that the contraction rope 6 and the protective shell 5 are put down together, and the electromagnetic lock 27 is powered off, so that goods can be put down from the airship.
The working principle is as follows: when the device is used, when the transport airship flies in a severe environment and goods need to be transported at a designated position, the transport airship is firstly suspended, then the rotating motor 25 is quickly turned on, the rotating shaft 26 is driven by the rotating motor 25 to rotate anticlockwise, so that the contraction rope 6 and the protective shell 5 are put down together, the surrounding environment is observed through the infrared camera 10 on the outer surface of the protective shell 5, the position of the container 28 is conveniently found by the fixing device 11, at the moment, the cylinder 17 is opened through the controller 15, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are opened, the fixing clamping grooves 30 on the periphery of the outer surface of the container 28 are gripped, the electromagnetic lock 27 is used for absorbing the iron plate 29 on the top of the container 28, finally the rotating shaft 26 is driven by the rotating motor 25 to rotate clockwise, the container 28 is pulled into the airship, and the goods can be rapidly shipped, when the goods on the airship need to be put down, the first gripper 16, the second gripper 18, the third gripper 19 and the fourth gripper 20 are only required to be opened, the fixing clamping groove 30 on the periphery of the outer surface of the container 28 is gripped, the iron plate 29 at the top of the container 28 is adsorbed through the electromagnetic lock 27, the rotating motor 25 is opened again, the rotating shaft 26 is driven to rotate anticlockwise through the rotating motor 25, the contraction rope 6 and the protective shell 5 are put down together, the electromagnetic lock 27 is powered off at the moment, and the goods can be put down from the airship.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims (9)

1. The utility model provides a transportation dirigible convenient to descend under complex environment, includes dirigible main part (1), balanced fin (2), engine nacelle (3), air chamber (4) and manipulation nacelle (7), its characterized in that: the airship is characterized in that a balance tail wing (2) is fixedly connected to the tail of the airship main body (1), a mooring cone (8) is fixedly connected to the head of the airship main body (1), an operation pod (7) is fixedly connected to the bottom end of the head of the airship main body (1), an engine pod (3) is fixedly connected to the bottom end of the tail of the airship main body (1), an air cabin (4) is arranged inside the middle end of the airship main body (1), rotating motors (25) are fixedly connected to both ends inside the airship main body (1), transmission shafts (26) are fixedly connected to the ends of the rotating motors (25), contraction ropes (6) are fixedly wound on the outer surfaces of the transmission shafts (26), a protective shell (5) is fixedly connected to one end of each contraction rope (6), each protective shell (5) comprises a protective flap (12) and a fixed plate (13), the protective flaps (12) are arranged around the bottom of the bottom (5), the middle end of the top of the fixing plate (13) is fixedly connected with a connector (9), the bottom of the fixing plate (13) is fixedly connected with a fixing device (11), the fixing device (11) comprises a connecting plate (14), a controller (15), a first gripper (16), an air cylinder (17), a second gripper (18), a third gripper (19), a fourth gripper (20) and an electromagnetic lock (27), the first gripper (16), the second gripper (18), the third gripper (19) and the fourth gripper (20) are fixedly connected with the fixing plate (13) through the connecting plate (14), the controller (15) is arranged between the tops of the first gripper (16), the second gripper (18), the third gripper (19) and the fourth gripper (20), the tops of the first gripper (16), the second gripper (18), the third gripper (19) and the fourth gripper (20) are fixedly connected with the air cylinder (17), an electromagnetic lock (27) is fixedly connected to the bottom of the connecting plate (14), and a container (28) is arranged at the bottom of the electromagnetic lock (27).
2. A transportation airship for facilitating descent in a complex environment according to claim 1, wherein: the protective petals (12) are petal-shaped structures, the protective petals (12) are four, the end portions of the four protective petals (12) are closed to form a conical structure, and the wide ends of the protective petals (12) are hinged to the bottom edge of the protective shell (5) through spring hinges.
3. A transportation airship for facilitating descent in a complex environment according to claim 1, wherein: the top of fixed plate (13) passes through connector (9) and shrink rope (6) fixed connection, fixed plate (13) are square hollow bottom open structure, the material of fixed plate (13) is polyethylene.
4. A transportation airship for facilitating descent in a complex environment according to claim 1, wherein: the wire arranging groove (22) is opened to the inside both sides of shrink rope (6), wire arranging groove (22) are provided with transmission line (23) on one side of the inside of shrink rope (6), inside opposite side wire arranging groove (22) of shrink rope (6) are provided with pull line (24), electromagnetic lock (27) and transmission line (23) electric connection.
5. A transportation airship for facilitating descent in a complex environment according to claim 4, wherein: and gaskets (21) are filled between the tension lines (24), the transmission lines (23) and the wiring grooves (22), and the gaskets (21) are made of soft steel wire meshes.
6. A transportation airship for facilitating descent in a complex environment according to claim 1, wherein: the first gripper (16) and the third gripper (19) are distributed relatively, the second gripper (18) and the fourth gripper (20) are distributed relatively, and the first gripper (16), the second gripper (18), the third gripper (19) and the fourth gripper (20) are distributed in a petal type structure.
7. A transportation airship for facilitating descent in a complex environment according to claim 1, wherein: an infrared camera (10) is arranged on the outer surface of the protective flap (12), and the model of the infrared camera (10) is EH 414C-120.
8. A transportation airship for facilitating descent in a complex environment according to claim 1, wherein: the output end of the controller (15) is electrically connected with the input end of the air cylinder (17), and the input end of the controller (15) is electrically connected with the output end of the infrared camera (10).
9. A transportation airship for facilitating descent in a complex environment according to claim 1, wherein: an iron plate (29) is fixedly connected to the top of the container (28), and fixing clamping grooves (30) are formed in the periphery of the outer surface of the container (28).
CN201920900015.1U 2019-06-16 2019-06-16 Transportation airship convenient to descend in complex environment Expired - Fee Related CN211167368U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920900015.1U CN211167368U (en) 2019-06-16 2019-06-16 Transportation airship convenient to descend in complex environment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920900015.1U CN211167368U (en) 2019-06-16 2019-06-16 Transportation airship convenient to descend in complex environment

Publications (1)

Publication Number Publication Date
CN211167368U true CN211167368U (en) 2020-08-04

Family

ID=71819645

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920900015.1U Expired - Fee Related CN211167368U (en) 2019-06-16 2019-06-16 Transportation airship convenient to descend in complex environment

Country Status (1)

Country Link
CN (1) CN211167368U (en)

Similar Documents

Publication Publication Date Title
US7887011B1 (en) Apparatus and methods for carrying airborne cargo
US10836509B2 (en) Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods
US11203430B2 (en) Airship launch from a cargo airship with a payload return vehicle
CA2829782C (en) Airborne platform
US8061647B1 (en) High altitude two balloon airship
US10457394B2 (en) Airship launch from a cargo airship
AU2014377667A1 (en) Cargo airship
US9522733B2 (en) Airship launch from a cargo airship
ITMI20091340A1 (en) PERFORMED AUTOSTABLE BALLOON AND RELATIVE INVOLVATION AND RECOVERY SYSTEM
WO2015000088A1 (en) Inflatable structural support for propulsion and control systems of uavs (unmanned aerial vehicle)
US4238095A (en) Method of and apparatus for anchoring airships and propulsion means for airships
CN108408019A (en) Variant stratospheric airship
CN104276281A (en) One-man flight vehicle
CN109760816A (en) A kind of mixed layout dirigible of bandwidth paddle power and vector power device
WO2011042316A1 (en) "momoheli ii" lifting module and vehicles
CN211167368U (en) Transportation airship convenient to descend in complex environment
CN109050866B (en) Airship
CN218055631U (en) Hang fixed wing aircraft of cabin folding and unfolding stability of goods that hangs in improvement
CN109250064A (en) Novel bionic aircraft structure with integrated buoyancy and lift high lift-drag ratio
CN115303433A (en) Carrier-borne inflation recovery platform of fixed-wing unmanned aerial vehicle, unfolding and recovery method
CN112537433A (en) Top open-close type offshore aerostat flying platform
CN211442720U (en) Multi-airbag hybrid airship
EP0088460B1 (en) Aircraft having buoyant gas balloon
CN112776975A (en) Multi-airbag hybrid airship
CN213292685U (en) Airship safety device

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20200804

Termination date: 20210616

CF01 Termination of patent right due to non-payment of annual fee