CN109263890A - A kind of rescue flight device - Google Patents
A kind of rescue flight device Download PDFInfo
- Publication number
- CN109263890A CN109263890A CN201811274597.3A CN201811274597A CN109263890A CN 109263890 A CN109263890 A CN 109263890A CN 201811274597 A CN201811274597 A CN 201811274597A CN 109263890 A CN109263890 A CN 109263890A
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- CN
- China
- Prior art keywords
- rescue
- tail
- cabin
- control equipment
- flight device
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/14—Attitude, flight direction, or altitude control by jet reaction the jets being other than main propulsion jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The invention discloses a kind of rescue flight devices, comprising: body, multiple duct lift units, multiple posture jet flow devices, tail push away engine, tailplane, vertical tail, flying control equipment cabin, rescue storage cabin and solar panels；Wherein, multiple duct lift units are built in body course direction two sides；Flying control equipment cabin and rescue storage cabin are disposed in parallel in the middle position of body, and solar panels setting is at the top of flying control equipment cabin and rescue storage cabin；Flying control equipment cabin is provided with lithium battery, super capacitor, control system, and solar panels are connect with lithium battery, and lithium battery is connect with super capacitor, and super capacitor connects control system and duct lift unit.The present invention solves the problems, such as existing helicopter since the longer feature of rotor can not be implemented to rescue in small space, and has reached environmental protection, long-endurance requirement.
Description
Technical field
The present invention relates to airplane design technical field, more particularly to a kind of rescue flight device.
Background technique
Since air rescue has many advantages, such as that fast response time, maneuverability are strong, rescue range is wide, rescue effect is good, because
This plays vital effect during disaster assistance.
The aircraft for being generally used for rescue is mainly helicopter, big and long rotor is external, at all can not it is some it is narrow,
Rescue task is implemented in complicated space, and to reduce kinetic equation loss, reaches long-time cruising ability, aircraft body can only be taken
With a small amount of first aid goods and materials.
Therefore, how to provide one kind can small space carry out rescue and long-endurance aircraft be this field skill
The problem of art personnel's urgent need to resolve.
Summary of the invention
In view of this, solving existing helicopter since rotor is longer the present invention provides a kind of rescue flight device
Feature can not implement the problem of rescuing in small space, and reach long-endurance requirement.
To achieve the goals above, the present invention adopts the following technical scheme:
A kind of rescue flight device, comprising: body, multiple duct lift units, multiple posture jet flow devices, tail push away engine, level
Empennage, vertical tail, flying control equipment cabin, rescue storage cabin and solar panels；
Multiple duct lift units are built in body course direction two sides；
Multiple posture jet flow devices are built in body spanwise direction two sides in pairs；
The body tail end is equipped with the orthogonal tailplane and the vertical tail, wherein the tailplane
It is arranged according to the body spanwise direction, the vertical tail is installed on the tailplane both ends, pacifies on the vertical tail
Engine is pushed away equipped with the tail；
The flying control equipment cabin and rescue storage cabin are disposed in parallel in the middle position of the body, and the solar panels are set
It sets at the top of the flying control equipment cabin and rescue storage cabin；
The flying control equipment cabin is provided with lithium battery, super capacitor and control system, and the solar panels and the lithium battery connect
It connects, the lithium battery is connect with the super capacitor, and the super capacitor connects the control system and duct lift dress
It sets.
Further, the duct lift unit is two, including fan, propeller and duct, the fan and described is pushed away
It arranges, and is arranged in the duct along the vertical direction of the body into device, wherein the propeller is located at the fan
Lower section, the propeller connect with the super capacitor, and the propeller provides power, and the fan is driven to rotate.
It further, further include elevator, the elevator is mounted on the tailplane.
It further, further include rudder, the rudder is mounted on the vertical tail.
Further, the tail pushes away engine and is set as two, is respectively arranged on the vertical tail and is respectively positioned on separate
The side of the tailplane.
It further, further include multiple undercarriages, the undercarriage is arranged in the organism bottom.
Further, the undercarriage is four, is symmetrically arranged on body spanwise direction two sides.
Further, it is provided with hatch door on rescue storage cabin, the hatch door is arranged far from the flying control equipment cabin one
Side.
Further, grid is installed, the grid is located in the posture jet flow device vertical direction, described on the body
Grid is used to be discharged the air-flow that the posture jet flow device generates.
Further, the flying control equipment cabin is additionally provided with receiver and life-detection instrument, the receiver and the life
Survey meter is connect with the control system.
It can be seen via above technical scheme that compared with prior art, the present disclosure provides a kind of rescue flight device,
Not only there is VTOL ability, and for traditional helicopter, duct lift unit is arranged in internal body, does not account for
With engine body exterior space, the volume of aircraft is reduced, small and exquisite fuselage allows it anywhere to execute the task of rescuing,
And lithium battery can not only be charged by external power supply, solar panels can also convert solar energy into electric energy storage in real time
The sufficient energy is provided for duct lift unit in lithium battery, and through super capacitor, solves available engine power not
The disadvantage of foot has reached long continuation of the journey requirement, and the feature of environmental protection is good.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 attached drawing is a kind of main view of rescue flight device provided by the invention；
Fig. 2 attached drawing is a kind of top view of rescue flight device provided by the invention；
Fig. 3 attached drawing is flying control equipment cabin and rescue storage cabin schematic internal view in a kind of rescue flight device provided by the invention.
Wherein, each component indicates:
1, body, 2, duct lift unit, 21, fan, 22, propeller, 23, duct, 3, posture jet flow device, 4, tail pushes away and start
Machine, 5, tailplane, 51, elevator, 6, vertical tail, 61, rudder, 7, flying control equipment cabin, 71, control system, 72, lithium electricity
Pond, 73, super capacitor, 74, receiver, 75, life-detection instrument, 8, rescue storage cabin, 9, solar panels, 10, undercarriage.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
The embodiment of the invention discloses a kind of rescue flight devices, fill with reference to attached drawing 1-3, including body 1, multiple duct lift
Set 2, multiple posture jet flow devices 3, tail pushes away engine 4, tailplane 5, vertical tail 6, flying control equipment cabin 7, rescue storage 8 and of cabin
Solar panels 9；Multiple duct lift units 2 are built in 1 course direction two sides of body；Multiple posture jet flow devices 3 are built in pairs
1 spanwise direction two sides of body；
1 tail end of body is equipped with orthogonal tailplane 5 and vertical tail 6, wherein tailplane 5 is opened up according to machine 1 to side
To arrangement, vertical tail 6 is installed on 5 both ends of tailplane, is equipped with tail on vertical tail 6 and pushes away engine 4；
Flying control equipment cabin 7 and rescue storage cabin 8 are disposed in parallel in the middle position of body 1, and solar panels 9 are arranged in flying control equipment
8 top of cabin 7 and rescue storage cabin；
Flying control equipment cabin 7 is provided with lithium battery 72, super capacitor 73 and control system 71, and solar panels 9 are connect with lithium battery 72,
Lithium battery 72 is connect with super capacitor 73, and super capacitor 73 connects control system 71 and duct lift unit 2.
Duct lift unit 2 is two, including fan 21, propeller 22 and duct 23, and fan 21 and propeller 22 are along machine
The vertical direction of body 1 is arranged, and is arranged in duct 23, and propeller 22 is connect with super capacitor, and propeller 22 provides power,
Fan 21 is driven to rotate.
Energy supply principle of the present invention are as follows: when rescue flight device is awaited orders, external power supply charges to lithium battery 72, the sun
Energy plate 9 converts the solar into electric energy and is stored in lithium battery 72；When rescue flight device works, lithium battery 72 is by the electric energy of storage
Pass to super capacitor 73, super capacitor 73 by electrical energy transportation to power devices such as control system 71 and duct lift units 2, with
Them are supplied to work normally.
The present invention not only has VTOL ability, and for traditional helicopter, small and exquisite fuselage makes it
Almost can anywhere execute the task of rescuing, have rapidly and efficiently, flexible multipurpose, by geographical space limit lack etc. it is excellent
Gesture；Also, after control system receives rescue instruction, control system 71 issues rescue order, and rescue flight device enters work
State, the at this time electric discharge of lithium battery 72 are filled to super capacitor 73,73 continued power of super capacitor to control system 71 and duct lift
Set 2, reached long continuation of the journey requirement, solve gasoline as the lift energy cause pollution environment, be short of power, cruise duration it is shorter
The problem of.
It further include elevator 51 to advanced optimize above-mentioned technical proposal, elevator 51 is mounted on tailplane 5, is used for
Adjust aircraft lifting.
It further include rudder 61 to advanced optimize above-mentioned technical proposal, rudder 61 is mounted on vertical tail 6, is used
It is turned in adjustment aircraft.
To advanced optimize above-mentioned technical proposal, tail pushes away engine 4 and is set as two, is respectively arranged on vertical tail 6
And the side far from tailplane 5.
It further include multiple undercarriages 10 to advanced optimize above-mentioned technical proposal, undercarriage 10 is arranged in 1 bottom of body.
To advanced optimize above-mentioned technical proposal, hatch door is provided on rescue storage cabin 8, hatch door is arranged far to fly to control and set
Standby 7 side of cabin facilitates personnel to pass in and out rescue storage cabin.
To advanced optimize above-mentioned technical proposal, grid is installed, grid is for being discharged the production of posture jet flow device 3 on body 1
Raw air-flow.
To advanced optimize above-mentioned technical proposal, flying control equipment cabin 7 is additionally provided with receiver 74 and life-detection instrument 75, connects
Receipts machine 74 and life-detection instrument 75 are connect with control system 71, wherein life-detection instrument 75 connects for detecting ground life entity
Receipts machine 74 is used to receive the life signal of life entity sending.
Embodiment 1: the rescue flight device of the present embodiment exactly likes sport car, including body 1, duct lift unit 2, appearance
State jet flow device 3, tail push away engine 4, tailplane 5, vertical tail 6, flying control equipment cabin 7, rescue storage cabin 8,9 and of solar panels
Undercarriage 10.
Multiple undercarriages 10 for landing are installed on the vertical direction of body 1, the present embodiment preferably four, are symmetrically installed
In 1 spanwise direction two sides of body, every side installs two, and is all located at the same side in the vertical direction of body 1, as shown in Figure 1.It is existing
The side that regulation body 1 is equipped with undercarriage 10 is the lower direction of body 1, and opposite direction is upper direction.
Multiple duct lift units 2 are built in the two sides in 1 course direction of body, the duct lift unit of the present embodiment respectively
2 include fan 21, propeller 22 and duct 23, and quantity is selected as two, wherein fan 21 is with propeller 22 along the vertical of body 1
Arrangement, fan 21 are located at the top of propeller 22, and propeller 22 provides power, and fan 21 is driven to rotate, and generate lift, Jin Erfei
Row device takes off vertically.
Multiple posture jet flow devices 3 are built in 1 spanwise direction two sides of body in pairs, for adjusting flight attitude, the present embodiment
It is preferred that four, that is, it is able to satisfy flight demand.Grid is also equipped on body 1, the installation site of grid is located at posture jet flow device 3
Vertical direction on, for be discharged posture jet flow device 3 generation air-flow.
1 course direction machine tail end of body is equipped with orthogonal tailplane 5 and vertical tail 6, wherein tailplane
5 selections one arrange, vertical tail 6 selects two according to 1 spanwise direction of body, are installed vertically on 5 both ends of tailplane, water
The horizontal tail wing 5, vertical tail 6 are connected with 1 course machine tail end of body.It is equipped in vertical tail 6 far from 5 side of tailplane
Tail pushes away engine 4, and it is two that tail, which pushes away engine 4, i.e., pushes away engine 4 equipped with a tail on each vertical tail 6, tail pushes away hair
Motivation 4 provides thrust, the high-speed flight for rescue flight device of the invention.
Be also equipped with elevator 51 on tailplane 5, elevator 51 be can pitching siding, and be located at level
On the one hand empennage 5 guarantees that aircraft has pitching stability far from 1 one end of fuselage, be on the other hand used to fly when high-speed flight
The pitch control of device, as shown in Figure 2.Be also equipped with rudder 61 on vertical tail 6, rudder 61 be can course swing wall
Plate, and it is located at vertical tail 6 far from 1 one end of fuselage, on the one hand guarantee that aircraft has shipping-direction stability, is on the other hand used for
The directional control of aircraft when high-speed flight, as shown in Figure 1.
It is also equipped with flying control equipment cabin 7 and rescue storage cabin 8 between two duct lift units 2 in body 1, flies control
Equipment compartment 7 and the rescue storage selection of cabin 8 are arranged side by side along 1 spanwise direction of body.Control system is installed in flying control equipment cabin 7
71, receiver 74, life-detection instrument 75, fuel tank, lithium battery 72 and super capacitor 73, control system 71 is for manipulating rescue flight
Device, the situation detected to state of ground and obtain each component of rescue flight device etc., life-detection instrument 75 is for detecting ground
Life entity, receiver 74 are used to receive the life signal of life entity sending, and fuel tank provides fuel oil, lithium battery 72 for rescue flight device
It can not only be charged by external power supply, solar panels 9 can also convert solar energy into electric energy in real time and be stored in lithium electricity
It in pond 72, and is that propeller 22 provides the sufficient energy by super capacitor 73.Rescue storage cabin 8 in be equipped with seat, chaise longue,
Multifunctional medical equipment, seat and chaise longue are used to place the wounded, and Multifunctional medical equipment is used to carry out emergency aid and treatment to the wounded,
In, for the quick boarding of the wounded, the hatch door in rescue storage cabin 8 is opened in far from 7 side of flying control equipment cabin, facilitates entrance, sees Fig. 3
It is shown.
The hovering of rescue flight device, catenary motion, horizontally rotate, open up to telemechanical, yawing rotation and pitching movement etc. be by
Two duct lift units 2, tail, which push away 4, four posture jet flow devices 3 of engine, tailplane 5 and 6 comprehensively control of vertical tail, to be come
It realizes.
Hovering is one of the most basic state of flight of the aircraft and most basic forms of motion.When two fans 21
Blade in the opposite direction constant velocity rotation when, resultant force and the aircraft gravity of lift mutually balance, and aircraft can be kept at this time
Floating state.Simultaneously in order to increase stability, auxiliary control can also be carried out using four downward jets of posture jet flow device 3.
The catenary motion of the rescue flight device is easier to control.When increasing by 21 blade revolving speed of fan simultaneously, rise at this time
The resultant force of power is greater than aircraft gravity, and aircraft will move upwards.When reducing 21 blade revolving speed of fan simultaneously, lift at this time
Resultant force be less than aircraft gravity, aircraft will move downward.For the purposes of increasing stability, four postures can also be utilized
The downward jet of jet flow device 3 carries out auxiliary control.
The torsion that is generated by means of fan 21 blade is horizontally rotated to realize.In 21 rotation process of fan, due to
The drag effect of air forms torsion.The size of torsion is related with revolving speed, when former and later two 21 revolving speeds of fan are identical but turn to phase
Inverse time, aircraft not can rotate；When increasing 21 revolving speed of fan at aircraft head, the torsion of aircraft rear and front end at this time
It cannot cancel out each other, just generating the torque around body 1 vertical (vertical Z axis) horizontally rotates aircraft.At this time in order to protect
The balance for demonstrate,proving power needs two upward jets of jet flow device at head, generates a downward power and makes aircraft in gravity side
Upward resultant force is zero, offsets aircraft new line or tendency of bowing.Otherwise increase another 21 revolving speed of fan then to turn round about
It is dynamic.
Under floating state, aircraft stress balance.When leaning on two posture 3 downward jets of jet flow device of 1 the same side of body,
Aircraft can generate a upward power, which generates a torque around 1 course direction of body and aircraft body 1 is tilted,
And the component of horizontal direction is generated, it opens up aircraft and is moved to the other side, i.e., far from the side for starting posture jet flow device 3；
When leaning on two posture 3 upward jets of jet flow device of 1 the same side of body, aircraft can generate a downward power, and the power is around machine
1 course direction of body generates a torque and aircraft body 1 is tilted, and generates the component of horizontal direction, make aircraft open up to
It is moved to close to the side for starting posture jet flow device 3.
Yaw control is divided into high speed and two kinds of situations of low speed, since 6 efficiency of vertical tail is lower when low-speed operations, flies at this time
The yaw of row device pushes away the thrust difference of engine 4 mainly by two tails to realize.When increase side tail pushes away 4 thrust of engine, this
When a torque around body 1 vertical (vertical Z axis) is generated at mass center, aircraft is yawed to the other side, i.e., far from starting
Tail pushes away the side of engine 4, and when reducing side tail and pushing away 4 thrust of engine, aircraft is to starting close to starting tail and push away at this time
The side of machine 4；When high-speed flight, 61 efficiency of rudder on vertical tail 6 is higher, to save fuel oil, yaws mainly by deflection
Rudder 61 on vertical tail 6 is realized.Two designs of vertical tail 6 ensure that the aircraft has course-stability simultaneously
Property.
The pitch control of the aircraft is also classified into two kinds of situations of low speed and high speed.Under lower-speed state 5 efficiency of tailplane compared with
Low, pitch control is realized mainly by 3 jet flow of posture jet flow device, similar to control with opening up.When aircraft is in equilibrium state, when
When two posture 3 downward jets of jet flow device at 1 course tail of body, aircraft can generate a upward power, and the power is in machine
At the constitution heart generate one around body 1 open up to torque (opening up to axis Y) makes aircraft bow, and generate horizontal direction point
Power makes aircraft travel forward.Otherwise it then comes back when two posture 3 downward jets of jet flow device at head and moves backward.At a high speed
When flight, to save fuel oil, pitching is realized mainly by the elevator 51 on deflection level empennage 5.The effect of horizontal tail simultaneously is also
It ensure that the aircraft has pitching stability.
Since rescue flight device duct lift unit of the invention is arranged in internal body, it is not take up engine body exterior space,
The volume of aircraft is reduced, and can realize the flight progress such as VTOL, low-latitude flying, it can be achieved that rescuing in small space
Help the tasks such as speedily carry out rescue work.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so being described relatively simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest scope of cause.
Claims (10)
1. a kind of rescue flight device characterized by comprising body (1), multiple duct lift units (2), multiple posture jet flows
Device (3), tail push away engine (4), tailplane (5), vertical tail (6), flying control equipment cabin (7), rescue storage cabin (8) and the sun
It can plate (9)；
Multiple duct lift units (2) are built in the body (1) course direction two sides；
Multiple posture jet flow devices (3) are built in the body (1) spanwise direction two sides in pairs；
Body (1) tail end is equipped with the orthogonal tailplane (5) and the vertical tail (6), wherein described
Tailplane (5) arranges that the vertical tail (6) is installed on the tailplane (5) two according to the body (1) spanwise direction
It holds, the tail is installed on the vertical tail (6) and pushes away engine (4)；
The flying control equipment cabin (7) and rescue storage cabin (8) are disposed in parallel in the middle position of the body (1), described
Solar panels (9) setting is at the top of the flying control equipment cabin (7) and rescue storage cabin (8)；
The flying control equipment cabin (7) is provided with control system (71), lithium battery (72) and super capacitor (73), the solar panels
(9) it is connect with the lithium battery (72), the lithium battery (72) connect with the super capacitor (73), the super capacitor (73)
Connect the control system (71) and the duct lift unit (2).
2. rescue flight device according to claim 1, which is characterized in that the duct lift unit (2) is two, is wrapped
Include fan (21), propeller (22) and duct (23), the fan (21) and the propeller (22) hanging down along the body (1)
It arranges, and is arranged in the duct (23) to direction, wherein the propeller (22) is located at below the fan (21),
The propeller (22) connect with the super capacitor (73), and the propeller (22) provides power, drives the fan (21)
Rotation.
3. rescue flight device according to claim 1, which is characterized in that further include elevator (51), the elevator
(51) tailplane (5) are mounted on.
4. rescue flight device according to claim 1, which is characterized in that further include rudder (61), the rudder
(61) it is mounted on the vertical tail (6).
5. rescue flight device according to claim 1, which is characterized in that the tail pushes away engine (4) and is set as two, point
It is not installed on the vertical tail (6) and is respectively positioned on the side far from the tailplane (5).
6. rescue flight device according to claim 1, which is characterized in that it further include multiple undercarriages (10), it is described to rise and fall
Frame (10) is arranged in the body (1) bottom.
7. rescue flight device according to claim 6, which is characterized in that the undercarriage (10) is four, is symmetrically installed
In the body (1) spanwise direction two sides.
8. rescue flight device according to claim 1, which is characterized in that it is provided with hatch door on rescue storage cabin (8),
The hatch door is arranged far from flying control equipment cabin (7) side.
9. rescue flight device according to claim 1, which is characterized in that be equipped with grid, the lattice on the body (1)
Grid are located in posture jet flow device (3) vertical direction, and the grid is used to be discharged the gas that the posture jet flow device (3) generates
Stream.
10. rescue flight device according to claim 1, which is characterized in that the flying control equipment cabin (7) is additionally provided with reception
Machine (74) and life-detection instrument (75), the receiver (74) and the life-detection instrument (75) with the control system (71)
Connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274597.3A CN109263890A (en) | 2018-10-30 | 2018-10-30 | A kind of rescue flight device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274597.3A CN109263890A (en) | 2018-10-30 | 2018-10-30 | A kind of rescue flight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109263890A true CN109263890A (en) | 2019-01-25 |
Family
ID=65194202
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811274597.3A Withdrawn CN109263890A (en) | 2018-10-30 | 2018-10-30 | A kind of rescue flight device |
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| Country | Link |
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| CN (1) | CN109263890A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111292602A (en) * | 2020-03-23 | 2020-06-16 | 陶桂来 | Model and method for flying or diving the model |
-
2018
- 2018-10-30 CN CN201811274597.3A patent/CN109263890A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111292602A (en) * | 2020-03-23 | 2020-06-16 | 陶桂来 | Model and method for flying or diving the model |
| CN111292602B (en) * | 2020-03-23 | 2022-03-04 | 陶桂来 | Model and method for flying or diving the model |
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Application publication date: 20190125 |