CN103231633A - Turtle-type land-sea-air spacecraft - Google Patents

Turtle-type land-sea-air spacecraft Download PDF

Info

Publication number
CN103231633A
CN103231633A CN2012104723763A CN201210472376A CN103231633A CN 103231633 A CN103231633 A CN 103231633A CN 2012104723763 A CN2012104723763 A CN 2012104723763A CN 201210472376 A CN201210472376 A CN 201210472376A CN 103231633 A CN103231633 A CN 103231633A
Authority
CN
China
Prior art keywords
port
communicated
air
cabin
air compressor
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.)
Pending
Application number
CN2012104723763A
Other languages
Chinese (zh)
Inventor
陈正茂
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN2012104723763A priority Critical patent/CN103231633A/en
Publication of CN103231633A publication Critical patent/CN103231633A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention relates to a turtle-type land-sea-air spacecraft. The turtle-type land-sea-air spacecraft comprises a cabin, wings and power machines, stator-free single screw air compressors, a control console, an air inlet, front exhaust ports, rear exhaust ports, a tail exhaust port and vibration reduction wheels, wherein the air inlet is composed of a plastic hose, is provided with a controller therein, and is connected to the stator-free single screw air compressors by pipelines; the stator-free single screw air compressors are connected to the gasolene power machines or electric motors; the air inlets of the gasoline machines are communicated with the inner chamber of the air inlet; electric motors are communicated with storage batteries; the exhaust ports of the stator-free single screw air compressors are communicated with the front exhaust ports, the rear exhaust ports and the tail exhaust port; and the wings are arranged at the periphery of the cabin; and the control console is arranged in the cabin. According to the invention, all functions of a ship, a submarine, an aircraft, an automobile are integrated to provide a multifunctional spacecraft, which can move fast in underwater, on water surface, on land and in air, and can be widely used in military, transportation, rescue, aerial work and travel.

Description

A kind of soft-shelled turtle formula aeroamphibious airship
Technical field
The present invention relates to a kind of hovercraft, Submarine, a kind of jet airplane, a kind of wheeled free air suspension car relates in particular to a kind of soft-shelled turtle formula aeroamphibious airship.
Background technology
Present steamer, submarine, aircraft, automobile, defective such as exist function singleness, efficiency is lower, and body weight is heavier.
Summary of the invention
It is the soft-shelled turtle formula aeroamphibious airship of one that its purpose of the present invention just is to provide a kind of ship, ship, machine, car function, has that body is light, efficient, the safe characteristics of landing.
The technical scheme that realizes above-mentioned purpose and take, comprise cabin, wing, engine, no stator single-screw air compressor, operator's station, admission port, front-seat gas port, rear exhaust port, the tail exhausr port, the vibration damping wheel is formed, described admission port is to be made of the plasticity flexible pipe, be provided with control device in the admission port, admission port is connected with no stator single-screw air compressor by pipeline, no stator single-screw air compressor is connected with gasoline-engine driven machine or electrical motor, the spark ignition engine admission port is communicated with the admission port inner chamber, electrical motor is communicated with storage battery, the exhausr port of no stator single-screw air compressor is by gas line and front-seat gas port, rear exhaust port, the tail exhausr port is connected, front-seat gas port, rear exhaust port, the tail exhausr port all adopts the ball interface to connect, and controller is housed, controller system is communicated with operator's station, wing is located at the week periphery of cabin, is provided with operator's station in the cabin.
Compared with prior art, the present invention has the following advantages,
1, adopted no stator single-screw air compressor, the design of spark ignition engine or electric motor structure has that body is light, characteristics of high efficiency;
2, exhaust system structure is simple, flexibly easily control, the characteristics that working environment is scalable, thus can be under water, the water surface, aerial, ground, flight and walking;
3, whole ship is taked flat design, to alleviating hull weight and running resistance, has great advantage.
Description of drawings
Fig. 1 is this apparatus structure lateral plan.
Fig. 2 is this apparatus structure scheme drawing.
The specific embodiment
Embodiment, as depicted in figs. 1 and 2, comprise cabin 9, wing 7, engine 6, no stator single-screw air compressor 4, operator's station 3, admission port 1, front-seat gas port 5, rear exhaust port 10, tail exhausr port 13, vibration damping wheel 14, the described admission port 1 of diving bag is the plasticity hose construction, be provided with control device 2 in the admission port 1, admission port is connected with no stator single-screw air compressor 4 by pipeline, no stator single-screw air compressor 4 is connected with spark ignition engine 5 or electrical motor 5, spark ignition engine 5 admission ports are communicated with main air inlet 1 inner chamber, 5 of electrical motors are communicated with storage battery or external power, no stator single-screw air compressor 4 exhausr ports by delivery piping 8 with respectively with front-seat gas port 5, rear exhaust port 10, tail exhausr port 13 is connected, front-seat gas port 5, rear exhaust port 10, tail exhausr port 13 all adopts ball interface 12 to connect, and controller 11 is housed, and controller 11 systems are communicated with operator's station 2, vibration damping wheel 14 is located at respectively on the base plate of front and back, during use, under the effect of engine 6, drive no stator single-screw air compressor 4 rotations and produce high pressure air by each exhausr port ejection, promote each exhausr port of airship and control the motion rising by operator's station by controller, descend or move ahead setback.

Claims (4)

1. soft-shelled turtle formula aeroamphibious airship, it is characterized in that, comprise cabin (9), wing (7), engine (6), no stator single-screw air compressor (4), operator's station (3), admission port (1), front-seat gas port (5), rear exhaust port (10), tail exhausr port (13), vibration damping wheel (14, the diving bag, described admission port (1) is the plasticity hose construction, be provided with control device (2) in the admission port (1), admission port (1) is connected with Air compressor (4) by pipeline, Air compressor (4) is connected with spark ignition engine (5) or electrical motor (5), spark ignition engine (5) admission port is communicated with the inner chamber of primary stage port (1), electrical motor then is communicated with storage battery or external power, Air compressor (4) exhausr port is communicated with gas line (8), and with front-seat gas port (5), rear exhaust port (10), tail exhausr port (13) is connected, front-seat gas port (5), rear exhaust port (10), tail exhausr port (13) all adopts the ball interface to connect, and controller (11) is housed is communicated with operator's station (2).
2. a kind of soft-shelled turtle formula aeroamphibious airship according to claim 1 is characterized in that engine (5) both can adopt spark ignition engine, also can adopt storage battery electrical motor or external power motor.
3. a kind of soft-shelled turtle formula aeroamphibious airship according to claim 1 is characterized in that Air compressor (4) is located at the outer preceding both sides of cabin (9), drives air nozzle and is provided with 5, and be located at the below periphery of wing (7).
4. a kind of soft-shelled turtle formula aeroamphibious airship according to claim 1 is characterized in that, is provided with the special-purpose bag of diving in the cabin (9).
CN2012104723763A 2012-11-21 2012-11-21 Turtle-type land-sea-air spacecraft Pending CN103231633A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012104723763A CN103231633A (en) 2012-11-21 2012-11-21 Turtle-type land-sea-air spacecraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012104723763A CN103231633A (en) 2012-11-21 2012-11-21 Turtle-type land-sea-air spacecraft

Publications (1)

Publication Number Publication Date
CN103231633A true CN103231633A (en) 2013-08-07

Family

ID=48879731

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2012104723763A Pending CN103231633A (en) 2012-11-21 2012-11-21 Turtle-type land-sea-air spacecraft

Country Status (1)

Country Link
CN (1) CN103231633A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105922829A (en) * 2016-06-24 2016-09-07 济南银河路桥试验检测有限公司 Municipal pipeline sonar detection equipment balance traction device
CN106240263A (en) * 2016-08-15 2016-12-21 浙江建设职业技术学院 A kind of ducted fan power vehicle
CN107985580A (en) * 2017-12-14 2018-05-04 西南交通大学 A kind of multi-modal deformable rotor robot
CN110884309A (en) * 2019-12-12 2020-03-17 周丽娟 Safe and reliable's intelligent unmanned aerial vehicle with online power generation function

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1312296A (en) * 1970-05-14 1973-04-04 Akad Wissenschaften Ddr Air land or water craft
CN1245120A (en) * 1999-07-16 2000-02-23 朱明华 Structure, running and operating method for flying dish type of triphibious flying vehicle
DE19840847A1 (en) * 1998-09-07 2000-03-09 Mathias Klug Modular hybrid vehicle for air, land or sea operation has cell module, bearing surface module, water drive mechanism module as well as appropriate units for air, land and water travel
US20050247819A1 (en) * 2004-05-08 2005-11-10 Anthony Caruso Lightweight vehicle operable on land, water and in the air
CN101961974A (en) * 2010-09-15 2011-02-02 北京理工大学 Land, water and air multi-domain engine-driven carriage vehicle
CN201849273U (en) * 2010-11-16 2011-06-01 沈东明 Four-function jet-propelled helicopter-type diving airship

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1312296A (en) * 1970-05-14 1973-04-04 Akad Wissenschaften Ddr Air land or water craft
DE19840847A1 (en) * 1998-09-07 2000-03-09 Mathias Klug Modular hybrid vehicle for air, land or sea operation has cell module, bearing surface module, water drive mechanism module as well as appropriate units for air, land and water travel
CN1245120A (en) * 1999-07-16 2000-02-23 朱明华 Structure, running and operating method for flying dish type of triphibious flying vehicle
US20050247819A1 (en) * 2004-05-08 2005-11-10 Anthony Caruso Lightweight vehicle operable on land, water and in the air
CN101961974A (en) * 2010-09-15 2011-02-02 北京理工大学 Land, water and air multi-domain engine-driven carriage vehicle
CN201849273U (en) * 2010-11-16 2011-06-01 沈东明 Four-function jet-propelled helicopter-type diving airship

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105922829A (en) * 2016-06-24 2016-09-07 济南银河路桥试验检测有限公司 Municipal pipeline sonar detection equipment balance traction device
CN106240263A (en) * 2016-08-15 2016-12-21 浙江建设职业技术学院 A kind of ducted fan power vehicle
CN106240263B (en) * 2016-08-15 2018-12-25 浙江建设职业技术学院 A kind of ducted fan power vehicle
CN107985580A (en) * 2017-12-14 2018-05-04 西南交通大学 A kind of multi-modal deformable rotor robot
CN107985580B (en) * 2017-12-14 2023-12-05 西南交通大学 Multi-mode deformable rotor robot
CN110884309A (en) * 2019-12-12 2020-03-17 周丽娟 Safe and reliable's intelligent unmanned aerial vehicle with online power generation function

Similar Documents

Publication Publication Date Title
US10371066B2 (en) Unmanned aircraft and operation method for the same
US9505282B2 (en) Amphibious flying car
US20180354613A1 (en) Aerial vehicle
CN204915162U (en) Navy, army and air force four -axis binary vehicle
CN103231633A (en) Turtle-type land-sea-air spacecraft
CN205615711U (en) Many rotor unmanned aerial vehicle with all -round ultrasonic sensor
CN102848870A (en) Land airship
CN107554783A (en) A kind of amphibious unmanned plane of VTOL
CN105217033A (en) Amphibious rotor wing unmanned aerial vehicle
EP0601212A4 (en) Multifunctional flying vehicle.
CN112265419A (en) Light high-speed amphibious diving vehicle
CN113306354A (en) Air-water integrated propulsion system of amphibious aircraft
CN105109695A (en) Multifunctional aircraft with hybrid of oil and electricity
CN105329448A (en) Oil-electricity mixed power system of vertical taking-off and landing unmanned aerial vehicle
CN102849209A (en) Composite power simple aircraft
RU2662600C2 (en) Aerocraft (flying car) (embodiments)
CN105035328A (en) Hybrid-power flight vehicle
CN205418106U (en) Duct formula stationary vane oil -electricity hybrid vehicle unmanned aerial vehicle
CN102555710A (en) Multifunctional flying fish used in water, land and sky
CN104369651A (en) Displacement of different power devices, fuel and power sources and traffic tool designed and manufactured through displacement and permutation and combination
CN202529147U (en) Worm disk-shaped aircraft
RU2634609C1 (en) Unmanned aerial vehicle control method and flight control actuating unit for method actualization
CN202669411U (en) Amphibious diving vehicle
RU2719993C1 (en) Multi-mode ground-effect vehicle - airplane
CN202879793U (en) Hybrid power simple aircraft

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20130807