CN108186211A - A kind of tilting rotor flight ambulance - Google Patents
A kind of tilting rotor flight ambulance Download PDFInfo
- Publication number
- CN108186211A CN108186211A CN201810168553.6A CN201810168553A CN108186211A CN 108186211 A CN108186211 A CN 108186211A CN 201810168553 A CN201810168553 A CN 201810168553A CN 108186211 A CN108186211 A CN 108186211A
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- Prior art keywords
- wing
- engine
- vehicle body
- tailplane
- ambulance
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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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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61G—TRANSPORT, PERSONAL CONVEYANCES, OR ACCOMMODATION SPECIALLY ADAPTED FOR PATIENTS OR DISABLED PERSONS; OPERATING TABLES OR CHAIRS; CHAIRS FOR DENTISTRY; FUNERAL DEVICES
- A61G3/00—Ambulance aspects of vehicles; Vehicles with special provisions for transporting patients or disabled persons, or their personal conveyances, e.g. for facilitating access of, or for loading, wheelchairs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
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- Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Veterinary Medicine (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a kind of tilting rotor flight ambulances, including vehicle body, wing and empennage, the wing is installed on the top of the vehicle body, the wing includes wing body, wing engine and rotor, the wing body stage casing is rotatablely connected with the vehicle body, the wing engine is installed on the both ends of the wing body by rotary shaft, and the rotor is installed on the top of the wing engine by rotary shaft, and the empennage is installed on the top of the tail of the body.The present invention has the function of automobile and tilting rotor helicopter, it can be on land and aerial work, it can hedgehopping, can hover rescue work, can be in road traveling, using tilting rotor type wing, VTOL and quick horizontal flight rapid translating can be achieved, wing can carry out rotation pack up, utmostly reduce occupied space, have the characteristics that conveniently, safely, fast, maneuverability.
Description
Technical field
The present invention relates to a kind of vehicles, and in particular to a kind of tilting rotor flight ambulance, technical field include vapour
Vehicle manufactures and aircraft manufacture.
Background technology
Oneself as hospital transports the main means of transport used during the wounded for the world today, dustoff and ambulance, and
Both of which respectively has advantage and disadvantage.The advantages of dustoff, is that speed is fast, and take the air line distance, and spatial dimension is big, is not in
Crowded and traffic jam phenomenon, shortcoming are to need dedicated airport and complicated navigation equipment and expensive, it is difficult to as rescue
Vehicle equally easily travels；The advantages of ambulance is easily to stop, and traveling freely facilitates, and price is relatively cheap, and shortcoming is by road
Road environment influences greatly, and speed is slow；How the vehicles that oneself popularizes by this two morning of dustoff and ambulance combine,
Make it that can not only be travelled as automobile on common road surface, but also can fly as helicopter, be people for a long time
Research direction.
Invention content
In view of this, the present invention provides a kind of tilting rotor flight ambulance,
To achieve these goals, the present invention adopts the following technical scheme that：
A kind of tilting rotor flight ambulance, including vehicle body, wing and empennage；The wing is installed on the top of the vehicle body,
The empennage is installed on the tail portion of the vehicle body；
The vehicle body includes radar module, driver's cabin, enging cabin and rescue cabin, and the enging cabin is located in the vehicle body
Portion, and top is equipped with bearing block；The chassis of the enging cabin is equipped with engine, transmission shaft, controllable coupling, speed changer and machine
Wing axis fixed seat, the both ends of the drive shaft are connect respectively with the engine and the speed changer, and the speed changer is arranged on institute
The lower section of wing axis fixed seat is stated, and is sequentially connected with the wing axis fixed seat by the controllable coupling；
The wing includes wing body, wing engine, rotor and wing axis；The wing axis be arranged in the bearing block respectively with
The wing fixed seat and wing body rotation connection；Tapered teeth is equipped between the wing body both ends and the wing engine to pass
Dynamic device, the taper tooth driving device are orthogonal conical tooth；The wing engine is installed on institute by rotary shaft
The both ends of wing body are stated, the rotor is installed on the top of the wing engine by rotary shaft.
The beneficial effects of the invention are as follows：The present invention has the function of automobile and tilting rotor helicopter, it can be on land
With aerial work, can hedgehopping, can hover rescue work, can in road traveling, using tilting rotor type wing, it can be achieved that
VTOL and the rapid translating of quick horizontal flight control the rotation of wing body by controllable coupling, convenient and efficient；Wing can
It carries out rotation to pack up, utmostly reduces occupied space, wing body both ends rotor wing rotation direction is adjusted by tapered tooth driving device,
Offer is taken off lift and preceding winged flying power, have the characteristics that conveniently, safely, fast, maneuverability.
Further, the bearing block is equipped with the torque control device for adjusting wing body rotation angle.
It is using above-mentioned further advantageous effect：Control the expansion of wing body and folding and unfolding.
Further, the wing body leading edge sweep is 5 °, and the wing body aspect ratio is 3.75, and the wing body contraction coefficient is
1.25。
The empennage includes tailplane and vertical tail, and the tailplane is fixedly connected with the vehicle body, described to hang down
Straight tail is respectively arranged in the both ends of the tailplane, and the tailplane is structure as a whole with the vertical tail.
The tailplane leading edge sweep is 5 °, and the tailplane and elevator aspect ratio is 2.45, the tailplane root tip
Than being 1.25, the vertical tail leading edge sweep is 42 °, and the fin and rudder aspect ratio is 1.4, the vertical end wing root tip
Than being 2.8.
It is using above-mentioned further advantageous effect：Increase tilting rotor flight ambulance in VTOL process and water
The stability of flat flight course.
Further, the vehicle body is structure as a whole, and the driver's cabin and the rescue cabin are equipped with the door passed in and out for personnel.
It is using above-mentioned further advantageous effect：The present invention be respectively provided in driver's cabin relatively independent aircraft and
The control steerable system of automobile, instrument and meter, and there is provided automatically control changeable control loop control with computer manually and fill
It puts, the automatic checkout and diagnosis alarm system of failure, doctor is configured with according to the installing of national first aid ambulance standard in rescue cabin
Treat first-aid apparatus equipment, can quickly reach first aid scene, and timely take the wounded effective treatment, avoid because
Traffic or rescue not in time the reason of caused by give treatment to not in time, utmostly ensure that the efficiency of first aid and surviving for the wounded
Rate.
Description of the drawings
Fig. 1 is tilting rotor of the present invention flight rescue vehicle travelling state schematic diagram；
Fig. 2 is tilting rotor flight ambulance lift mode schematic diagram of the present invention；
Fig. 3 is tilting rotor flight ambulance level flight condition schematic diagram of the present invention.
In attached drawing, parts list represented by the reference numerals are as follows：
1st, vehicle body, 2, wing, 3, empennage, 11, radar module, 12, driver's cabin, 13, enging cabin, 14, rescue cabin, 21, wing body,
22nd, wing engine, 23, rotor, 31, vertical tail, 32, tailplane.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes：
Tilting rotor flight ambulance as shown in Figs. 1-3, including vehicle body 1, wing 2 and empennage 3；
Vehicle body 1 is structure as a whole, and radar module 11, driver's cabin 12, enging cabin 13 and rescue cabin are followed successively by backward by 1 front end of vehicle body
14, driver's cabin 12 and rescue cabin 14 are equipped with the door passed in and out for personnel；
Enging cabin is located at the middle part of vehicle body 1, and top is equipped with bearing block；The chassis of enging cabin 13 is equipped with engine, transmission
Axis, controllable coupling, speed changer and wing axis fixed seat, both ends of the drive shaft are connect respectively with engine and speed changer, speed changer
The lower section of wing axis fixed seat is arranged on, and is sequentially connected with wing axis fixed seat by controllable coupling；
Wing 2 includes wing body 21, wing engine 22 and rotor 23 and wing axis；Wing axis be arranged in bearing block respectively with wing
Fixed seat and wing body 21 are rotatablely connected；Tapered tooth driving device is equipped between 21 both ends of wing body and wing engine, conical tooth passes
Dynamic device is orthogonal conical tooth；Wing engine 22 is installed on the both ends of wing body 21 by rotary shaft, and rotor 23 passes through
Rotary shaft is installed on the top of 2 engine of wing, and 21 leading edge sweep of wing body is 5 °, and 21 aspect ratio of wing body is 3.75, wing body 21
Contraction coefficient is 1.25；
Empennage 3 is installed on the top of 1 tail portion of vehicle body, and including tailplane 32 and vertical tail 31, tailplane 32 is solid with vehicle body 1
Fixed connection, vertical tail 31 are respectively arranged in the both ends of tailplane 32, and tailplane 32 is structure as a whole with vertical tail 31,
32 leading edge sweep of tailplane is 5 °, and 32 aspect ratio of tailplane is 2.45, and 32 contraction coefficient of tailplane is 1.25, vertical end
31 leading edge sweep of the wing is 42 °, and 31 aspect ratio of vertical tail is 1.4, and 31 contraction coefficient of vertical tail is 2.8.
The tilting rotor flight ambulance of present invention wing body 21 in VTOL is unfolded, and rotor 23 is horizontality, is
Tilting rotor flight ambulance provides upward lift, when tilting rotor flight ambulance rises to required height, machine
It is plumbness that wing engine 22 and rotor 23, which are rotated along rotary shaft to rotor 23, realizes horizontal flight；Tilting rotor ambulance
Wing 2 is VTOL state during landing, and wing engine 22 is stopped after ground is drop to, and wing body 21, wing start
Machine 22 and rotor 23 are packed up by rotary shaft, start automobile engine, you can realize road traveling.
Above-described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.Based in the present invention
Embodiment, those of ordinary skill in the art's all other embodiments obtained without making creative work, all
Belong to the scope of protection of the invention.
Claims (6)
1. a kind of tilting rotor flight ambulance, which is characterized in that including vehicle body（1）, wing（2）And empennage（3）；The wing
（2）It is installed on the vehicle body（1）Top, the empennage（3）It is installed on the vehicle body（1）Tail portion；
The vehicle body（1）Including radar module（11）, driver's cabin（12）, enging cabin（13）And rescue cabin（14）；The engine
Cabin（13）Positioned at the vehicle body（1）Middle part, and top be equipped with bearing block；The enging cabin（13）Chassis be equipped with start
Machine, transmission shaft, controllable coupling, speed changer and wing axis fixed seat, the both ends of the drive shaft respectively with the engine and institute
Speed changer connection is stated, the speed changer is arranged on the lower section of the wing axis fixed seat, and passes through with the wing axis fixed seat
The controllable coupling is sequentially connected；
The wing（2）Including wing body（21）, wing engine（22）And rotor（23）And wing axis；The wing axis is arranged in
The bearing block respectively with the wing fixed seat and the wing body（21）Rotation connection；The wing body（21）Both ends and the machine
Wing engine（22）Between be equipped with tapered tooth driving device, the taper tooth driving device be orthogonal conical tooth；It is described
Wing engine（22）The wing body is installed on by rotary shaft（21）Both ends, the rotor（23）It is installed on by rotary shaft
The wing（2）The top of engine.
2. a kind of tilting rotor flight ambulance according to claim 1, which is characterized in that the bearing block is equipped with and is used for
Adjust the torque control device of wing body rotation angle.
A kind of 3. tilting rotor flight ambulance according to claim 1, which is characterized in that the wing body（21）After leading edge
Sweep angle is 5 °, the wing body（21）Aspect ratio is 3.75, the wing body（21）Contraction coefficient is 1.25.
A kind of 4. tilting rotor flight ambulance according to claim 1, which is characterized in that the empennage（3）Including water
The horizontal tail wing（32）And vertical tail（31）, the tailplane（32）With the vehicle body（1）It is fixedly connected, the vertical tail
（31）It is respectively arranged in the tailplane（32）Both ends, the tailplane（32）With the vertical tail（31）It is integrated
Structure.
A kind of 5. tilting rotor flight ambulance according to claim 4, which is characterized in that the tailplane（32）Before
Edge angle of sweep is 5 °, the tailplane（32）Aspect ratio is 2.45, the tailplane（32）Contraction coefficient is 1.25, described to hang down
Straight tail（31）Leading edge sweep is 42 °, the vertical tail（31）Aspect ratio is 1.4, the vertical tail（31）Contraction coefficient
It is 2.8.
6. according to a kind of tilting rotor flight ambulance of claim 1-5 any one of them, which is characterized in that the vehicle body
（1）It is structure as a whole, the driver's cabin（12）With the rescue cabin（14）It is equipped with the door for personnel's disengaging.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810168553.6A CN108186211A (en) | 2018-02-28 | 2018-02-28 | A kind of tilting rotor flight ambulance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810168553.6A CN108186211A (en) | 2018-02-28 | 2018-02-28 | A kind of tilting rotor flight ambulance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108186211A true CN108186211A (en) | 2018-06-22 |
Family
ID=62594594
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810168553.6A Withdrawn CN108186211A (en) | 2018-02-28 | 2018-02-28 | A kind of tilting rotor flight ambulance |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108186211A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112440858A (en) * | 2020-11-30 | 2021-03-05 | 中国人民解放军总医院第三医学中心 | Outdoor carriage expansion adjusting mechanism and using method |
-
2018
- 2018-02-28 CN CN201810168553.6A patent/CN108186211A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112440858A (en) * | 2020-11-30 | 2021-03-05 | 中国人民解放军总医院第三医学中心 | Outdoor carriage expansion adjusting mechanism and using method |
| CN112440858B (en) * | 2020-11-30 | 2022-06-17 | 中国人民解放军总医院第三医学中心 | Outdoor carriage expansion adjusting mechanism and using method |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180622 |