CN2557422Y

CN2557422Y - Aircraft

Info

Publication number: CN2557422Y
Application number: CN 02274143
Authority: CN
Inventors: 薄继杰
Original assignee: Individual
Current assignee: Individual
Priority date: 2002-07-12
Filing date: 2002-07-12
Publication date: 2003-06-25
Anticipated expiration: 2012-07-12

Abstract

The utility model relates to an aircraft which is composed of a cockpit, an undercarriage, a balancing and steering mechanism, a lifting and advancing mechanism, etc., wherein the balancing and steering mechanism forms a dish-shaped rotary body of which the outer ring is a rotary balancer and the inner ring is an inner rotary frame, and a fixing frame is arranged between the rotary balancer and the inner rotary frame. A bearing or a roller group through the fixing frame is respectively connected with the rotary balancer and the inner rotary frame, the rotary balancer is provided with an inner gear ring for driving a gear, the inner rotary frame is provided with an outer gear ring for driving a gear, and the cockpit is fixed on the inner rotary frame. The lifting and advancing mechanism comprises a lifting jetting type engine, a lowering jetting type engine and an advancing jetting type engine, wherein the lifting jetting type engine is arranged at the bottom surface of the inner rotary frame and downwards jets, the lowering jetting type engine is arranged at the top surface of the inner rotary frame and upwards jets, and the advancing jetting type engine is arranged at the bottom or the top part of the inner rotary frame and jets in the horizontal and the same direction mode. The utility model can vertically take off and land without airscrews, does not need to use air buoyancy, and has the advantages of good balance performance, safety and reliability.

Description

Aircraft

Technical field

The utility model relates to the Aeronautics and Astronautics field, is specially a kind of aircraft.

Background technology

Present outer space vehicle has spacecraft, space shuttle and aerospace plane etc., and spacecraft relies on rocket to send the Heaven fully, and cost is very high, limited by feedway; Space flight has multiple with aircraft, though as aerospace plane without rocket launching, cost is low, but it can not vertical takeoff and landing, limited by runway, realizes lifting and turning by air lift force, its turn radius has several kms, be subjected to weather influence bigger, balance is relatively poor, makes troubles for operation and safety; Autogyro adopts propeller in its top, needs by the air lift force vertical lift.

Chinese patent (application number: 98112980.3, publication number: 1224681) disclose a kind of flying disc with rotary hull, at the dish body by interior storehouse, the shell double-decker is formed, with aviation nuclear electric power generation, the superconduction generating, super-conductive magnetic suspension, the ionized air, the multiplication of voltage high potential takes place and automatic guidance is the basis, by repelling the heavy ion that is ionized air in the dish body upper surface layer, produce vacuum thin layer, on the dish body, the lower surface pressure difference produces lift and thrust, its weak point is: it is put down and all need by air with lifting to fly, and the energy power system cost is higher.

The utility model content

The utility model purpose provide a kind of do not have propeller, balance quality good, can self governing speed, do not need by air lift force, aircraft simple in structure.

The technical solution of the utility model is:

A kind of aircraft, have driving compartment, landing pad, and balance, steering hardware and lifting, propulsive mechanism, described balance, steering hardware are dish-like swivel, its outer ring is the spin balancing device, inner ring is interior swivel mount, be fixed mount between spin balancing device and the interior swivel mount, the bearing set by fixed mount is connected with spin balancing device, interior swivel mount respectively, and the spin balancing device is provided with gear-driven internally toothed annulus, interior swivel mount is provided with gear-driven external toothing, and driving compartment is fixed on the interior swivel mount; Described lifting, propulsive mechanism comprise be installed in swivel mount bottom surface, downward jet lifting jet engine, swivel mount end face in being installed on, make progress the decline jet engine jet, and bottom the swivel mount or top, the jet in the same way propelling jet engine of level in being installed on.

The utility model can add dish, column type or ball-type shell, and bag balance, steering hardware and lifting, propulsive mechanism and driving compartment are connected with interior swivel mount in it; Described lifting can be 1～3 group with jet engine, and is 3～6 every group, uniform; Described bearing set can be installed on the upper/lower terminal or the centre of fixed mount; Described bearing set can roller set, magnetcisuspension or air cushion replace; The drive motor of described spin balancing device is the space flight high-speed electric expreess locomotive; The drive motor of swivel mount is the space flight motor in described.

The beneficial effects of the utility model are:

1. do not have propeller, vertical takeoff and landing, energy self governing speed, do not need by air lift force.Spin balancing device of the present utility model is done power by the space flight high-speed electric expreess locomotive, reaches spin balancing device high speed revolution with the gear driven internally toothed annulus, produces momentum, makes it stabilized flight; Interior swivel mount can planar rotate arbitrarily angled, it has made things convenient for cosmonaut's driving, any original place change of direction (planar) in the middle of flight, by space flight motor, gear driven external toothing, swivel mount rotation in making, change to advance jet direction, be implemented in and arbitrarily angledly turn to, travel in the air with jet engine; In addition, lifting can produce the lift of vertical direction or fall power with jet engine with jet engine and decline, can make aircraft be parked in aerial or lifting, does not need by air lift force, and balance quality is good, and is safe and reliable.

2. the utility model manufacturing simple in structure, easy, cost are lower, can be applicable to fields such as space transportation, space flight detection.

Description of drawings

Fig. 1 is the utility model structural representation.

Fig. 2 is the A-A cutaway view of Fig. 1.

Fig. 3 is embodiment 2 structural representations.

Fig. 4 is the B-B cutaway view of Fig. 3.

The specific embodiment

Embodiment 1

Shown in Fig. 1～2, the utility model comprises balance, steering hardware 1 and lifting, propulsive mechanism 2, driving compartment 3, landing pad 4, described balance, steering hardware 1 is dish-like swivel, divide three circles from outside to inside, its outer ring is a spin balancing device 11, inner ring is interior swivel mount 16, be fixed mount 15 between spin balancing device 11 and the interior swivel mount 16, on fixed mount 15, the bearing set 151 at following two ends, 152 respectively with spin balancing device 11, interior swivel mount 16 connects, spin balancing device 11 is provided with the internally toothed annulus 12 of gear 14 transmissions, interior swivel mount 16 is provided with the external toothing 19 of gear 18 transmissions, and driving compartment 3 is fixed on the interior swivel mount 16; Described lifting, propulsive mechanism 2 comprise be installed in swivel mount 16 bottom surfaces, jet lifting downwards with jet engine 22, the decline jet engine 21 that be installed on interior swivel mount 16 end faces, makes progress jet, and being installed on interior swivel mount 16 bottoms, the jet in the same way propelling jet engine 23 of level, landing pad 4 is installed on interior swivel mount 16 bottoms.

Spin balancing device 11 of the present utility model provides power by the space flight high-speed electric expreess locomotive 13 that is fixed in fixed mount 15, gear 14 is fixed on the space flight high-speed electric expreess locomotive 13, internally toothed annulus 12 is fixed on the spin balancing device 11, gear 14 drives internally toothed annulus 12 and reaches spin balancing device 11 high speed revolutions, produces momentum, makes it stabilized flight, need the momentum size to decide according to the weight of aircraft, the rotating speed and the quality of spin balancing device 11 match each other, and rotating speed generally is located at about 1000 rev/mins, and be both economical reasonable;

Fixed mount 15 is main support framves of the present utility model, with it is core, spin balancing device 11 and interior swivel mount 16 connect by bearing 151,152, because the rotating speed of spin balancing device 11 is very high, it there is very big application force, also have two space flight high-speed electric expreess locomotives 13 and two space flight motors 17 to be fixed on the support body, so fixed mount 15 need have very big intensity;

Interior swivel mount 16 provides power by the space flight motor 17 that is fixed in fixed mount 15, gear 18 is fixed on the space flight motor 17, gear 18 drives external toothing 19, the planar anglec of rotation and speed rotation arbitrarily of swivel mount 16 in making, change the jet direction that advances with jet engine 23, so with regard to change of flight device thrust direction, so just changed the heading of aircraft, swivel mount 16 forward and backwards and fast, slow-speed in space flight motor 17 can drive are so that turn to during flight flexible;

Lifting is divided into two groups with jet engine 22 by eight jet engines, and one group standby, and one group is used when taking off, also can two groups use simultaneously, its thrust is greater than gravity during aircraft takeoff, and thrust is parked in less than gravity that thrust equals gravity when aerial during landing, when flying speed is slow, for anti-aircraft falls, do not allow aircraft fall for certain thrust, so aircraft just can take off vertically, land, its spout stretches out outside face when using automatically, and the time spent is not recoverable to;

Descend and form by four jet engines with jet engine 21, its spout stretches out outside face when using, the time spent is not recoverable to, its thrust is equal to or greater than gravity and all can, its effect is under the situation of no gravitation, makes the aircraft usefulness of landing downwards, if lifting all is out of order with jet engine during landing, can use demifacet to descend and aircraft be turned, restart whole driving engines and make the aircraft security landing with jet engine;

Advance with jet engine 23 and produce horizontal thrust, can make aircraft reach certain speed per hour, spout stretches out outside face when using, and the time spent is not recoverable to;

Landing pad 4 is made up of totally four cylindrical telescopic outriggers, and every load-carrying capacity must reach the weight of aircraft, puts down during landing, regains during flight;

The utility model aircraft gangway 5 below, after the import and export door was opened, elevator 6 can drop to ground, conveniently to take advantage of people and carrying goods and materials, can establish safety door above the utility model in addition, in case unexpected, driving compartment 3 top projections are installed clear glass, so that increase driver vision, but glass light color, prevent that in the strong illumination operator's compartment, glass need have certain intensity, in case in universe, broken by meteor stone;

Should design Aeronautics and Astronautics instrument and meter, button, switch and spanner on the operator's station 31 in the driving compartment 3, and computer automatic steering facility, chair lift 32 is provided with peace and makes protection such as band facility, the space flight motor can design two above circuit of cover and master cocies, can control motor forward and backward and turning velocity speed; Every group of button that master cock and engine thrust size are all arranged of jet engine, every button that master cock and engine thrust size also will be arranged is like this so that awing and when landing controlling aircraft better of taking off.

In addition, fuel chambers, radar, communication apparatus, pick up camera, solar cell, various lamp, oxygenerator, lounge, sanitary accomodation etc. are according to the space actual placement.

Embodiment 2

Shown in Fig. 3～4, difference from Example 1 is that aircraft skin adopts ball-type, be connected with interior swivel mount 16, bag balance, steering hardware 1 and lifting, propulsive mechanism 2 and driving compartment are in it, ball-type impact resistance power is strong, air resistance is also little, and it advances the upper and lower both sides that are installed on interior swivel mount 16 with jet engine 23, and jet direction is identical; The bearing set 151,152 that is used to connect spin balancing device 11 and interior swivel mount 16 is installed in the middle of the fixed mount 15.

In addition, the utility model shell can also be dish, and its outward flange is thin, thick middle wraps in the inside advancing with jet engine, and like this, air resistance is little when taking off and flying; Shell also can be column type.

When very big, the coupling bearing of spin balancing device and fixed mount can't be processed, and can use replacements such as roller, magnetcisuspension, air cushion as the aircraft manufacturing; Lifting can specifically be chosen with the quantity of jet engine with jet engine, propelling as required with jet engine, decline.

Claims

1. aircraft, has driving compartment (3), landing pad (4), it is characterized in that also comprising balance, steering hardware (1) and lifting, propulsive mechanism (2), described balance, steering hardware (1) is dish-like swivel, its outer ring is spin balancing device (11), inner ring is interior swivel mount (16), be fixed mount (15) between spin balancing device (11) and the interior swivel mount (16), bearing set by fixed mount (15) respectively with spin balancing device (11), interior swivel mount (16) connects, spin balancing device (11) is provided with gear-driven internally toothed annulus (12), interior swivel mount (16) is provided with gear-driven external toothing (19), and driving compartment is fixed on the interior swivel mount (16); Described lifting, propulsive mechanism (2) comprise and are installed on interior swivel mount (16) bottom surface, jet lifting downwards with jet engine (22), the decline that be installed on interior swivel mount (16) end face, makes progress jet is with jet engine (21), and is installed on the jet in the same way propelling of interior swivel mount (16) bottom or top, level with jet engine (23).

2. according to the described aircraft of claim 1, it is characterized in that adding dish, column type or ball-type shell, bag balance, steering hardware (1) and lifting, propulsive mechanism (2) and driving compartment are connected with interior swivel mount (16) in it.

3. according to the described aircraft of claim 1, it is characterized in that described lifting is 1～3 group with jet engine (22), 3～6 every group, uniform.

4. according to the described aircraft of claim 1, it is characterized in that described bearing set is installed on the upper/lower terminal or the centre of fixed mount (15).

5. according to claim 1 or 4 described aircraft, it is characterized in that described bearing set replaces with roller set, magnetcisuspension or air cushion.

6. according to the described aircraft of claim 1, the drive motor that it is characterized in that described spin balancing device (11) is space flight high-speed electric expreess locomotive (13).

7. according to the described aircraft of claim 1, it is characterized in that the drive motor of described interior swivel mount (16) is space flight motor (17).