CN2732622Y - Wing panel top/bottom fan separated type flight device - Google Patents

Wing panel top/bottom fan separated type flight device Download PDF

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Publication number
CN2732622Y
CN2732622Y CN 200420000892 CN200420000892U CN2732622Y CN 2732622 Y CN2732622 Y CN 2732622Y CN 200420000892 CN200420000892 CN 200420000892 CN 200420000892 U CN200420000892 U CN 200420000892U CN 2732622 Y CN2732622 Y CN 2732622Y
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China
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wing
wing plate
plate
separated type
air
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Expired - Fee Related
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CN 200420000892
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Chinese (zh)
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张凤林
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Individual
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Individual
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Abstract

The utility model discloses a wing panel top/bottom separated type flight device designed by imitating bird flying skill. The manufacture technical proposal of the wing panel top/bottom separated type flight device is dreamed up after people observe the failing conclusion that west people develop ornithopters for a century. Wing plate surface is made to be a structure which has one way ventilation function, and the wing plates are divided into an upper wing plate and a lower wing plate to become bionic wings, one bionic wing can open, one bionic wing can close, the continuous fan force can be obtained by top/bottom separated fans. A wind channel is arranged below an operator cabin base, and is provided with a gear and blades; when the blades are turned; resisting air which is positioned head on absorbed into the wind channel and is discharged backward to form power which is equivalent to the power to run up and to boost. The wing panel top/bottom separated type flight device designed by imitating bird flying skill mainly comprises an upper wing plate (1), a lower wing plate (2), a pole (3), driving push rods (9) and (10), wind channels (7) (25) and (33), a gear, blades (35), a bottom wheel (30), shaft and pole members for connecting and fixing, etc. The wing panel top/bottom separated type flight device designed by imitating bird flying skill can be developed and used for the items of the industries of sports, agriculture and forestry, low altitude traffic, etc.

Description

Wing plate is the fan separated type aircraft up and down
1) technical field under
The utility model relates to a kind of aircraft, and especially set upward bottom wing can divide the aircraft of fan up and down.
2) technical background
Can allow the wing of aircraft agitate up and down? this is the dream that mankind attempt realization since ancient times and fail to realize.This can see from the human aerospace books books and periodicals of present publication: human century-old many flight heuristic process, although the mankind have grasped aerospace ability, but do not make a successful trial flight so far at mockingbird and the contemplated flapping wing aircraft of insect flying skill, it regarded as by west aircraft expert " even be can not realize and might be also can do to such an extent that very hugely do not have a realization meaning because of wing ".Yet people are told in aerodynamic research, take the mode of flapping flight more laborsaving, if the present aircraft of deciding wing flight can be made into the aircraft of flapping flight, that just can save the aircraft desired power greatly, but because the principle of flapping flight and phenomenon are quite complicated, people also do not have the on top of rule and the technology of this respect now.; can atmospheric envelope be upset by it along with the increasing wide model of the jet-propelled aircraft of modern fuel oil of maturation uses? can the waste gas that it sprays in the air at height form the more gross pollution to sky? does the frequent use of green-house effect and aerospace vehicle have that it doesn't matter? or the like these queries and worried also harass and disturb the mankind day by day because of the generation repeatedly of global natural climate disaster.Therefore, from environmental protection with energy-conservationly have in mind, meaning, value and the responsibility of grinding the wound flapping wing aircraft are very huge and urgent.
3) summary of the invention
For lighting the enthusiasm that people grind the wound flapping wing aircraft once again, the utility model proposes a kind of wing plate fan separated type aircraft up and down, the wing plate of this aircraft not only divides up and down and can divide fan up and down, and the people can drive it with the strength of oneself, realizes the hope that flies up and fly as bird.
Realize that the technical scheme that this purpose adopts is: agitate mechanism according to my bird's wing of comprehension, about wing is divided into, make and can one open one and close ground and divide bionical " wing " that fan obtains to continue fan power promptly up and down: when upper limb to lower fan at present the wing promptly upwards lift, bottom wing is to lower fan when upper limb is upwards lifted.Because the wing of bird is rearranged by many feathers, this structure can make bird when the Back stroke wing, and feather is loose shape, is beneficial to seeing through of upper end air, plays the effect that reduces air resistance, obtains the power of ascending to heaven and saving muscle power.When bird lower fan wing, its feather can be sealed shape, stops air to see through, and can obtain bigger air resistance and fan power.The air resistance difference that this Back stroke lower fan forms promptly forms the power of ascending to heaven of bird.This mechanism also becomes makes the technical scheme that this wing is taked: the wing plate face is made the structure with one-way ventilating function.Bird has " run-up " behavior when taking off, the technical scheme that is formed by the behavior is: will be transformed into the air channel under the operator's compartment seat, establish gear and flabellum in the air channel, the part resistance air that will head on during the flabellum rotation sucks the air channel and discharges backward and can form the thrust that is equivalent to run-up.Instigate this aircraft wing plate and agitate can adopt electric power or manpower with the method for flabellum rotation, I advocate the machine driven system that elder generation adopts manpower to instigate, and it is to use mechanics of machinery principles such as bent lever secondary reinforcement and gear change to make.
The beneficial effects of the utility model are: make simply, and floor area little (4 * 5 * 2.5 meters), the flapping flight mode is more laborsaving, can save the needed energy material of aircraft, the noise that flies is little, the discharging of environmentally safe thing, the atmosphere structure is not had injury, help air environment and restore calm.In industries such as sports, agriculture and forestry and low latitude traffic is that using value is arranged very much.
4) description of drawings
Describe in detail below in conjunction with accompanying drawing.But this scheme should not form restriction to improvement of the present utility model.
Fig. 1 is a positive over glaze cutaway view of implementing a design plan scheme drawing of the present utility model.
Fig. 2 is the side cutaway view of aircraft shown in Figure 1.
Among the figure on lath 6. sliding sleeves 7. air intake stomatodeum housings 8. air port protecting wire nets 9. flabellum push rods 10. wing plate push rods 11. side plates 12. of 1. upper flanges, 2. lower wing plates, 3. poles, 4. trip bolts 5. location 21. times V-arrangement arms of V-arrangement arm 13. thumb wheels 14. air-valve boxes 15. thumb wheel axles 16. screws 17. wing plate skeletons 18. boxes gear pad 19. sleeve pipes, 20. bearing pins, 22. escapement bars, 23. connecting rods, 24. fulcrum shafts, 25. air channel housings, 26. change-speed gearings, 27. base plates 28. ride seat 29. foot-operated steering linkage 30. return pulleys 31. side plates and connect column sleeve pipe clamp 32. thumb wheel chutes 33. exhausting duct housings 34. flabellum bracing struts 35. flabellums 36. Caudad mouths 37. soft 38. knuckles 39. that connect and turn to backguy 40. bevel gears 41. pitman shafts 42. helical gears.
5) specific embodiments
At a kind of plate wing shown in Figure 1 up and down in the scheme of fan separated type aircraft, flying wing is the whole plate shape that the one-way ventilating function is arranged, it is divided into upper flange (1) and lower wing plate (2), last dress sliding sleeve (6), and make guide pillar by four poles (3) and support, it is fixing with location lath (5) and tightening screw (4), dress return pulley (30) at the bottom of the post.Upper and lower wing plate is connected with thumb wheel (13) by bearing pin (20) by the V-arrangement arm (12) (21) that is welded on the sliding sleeve (6), thumb wheel axle (15) passes sleeve pipe (19), side plate (11) is affixed with escapement bar (22), and the escapement bar other end is connected with wing plate push rod (10) through connecting rod (23).When pulling wing plate push rod (10), the V-arrangement arm is done the lifting slip along thumb wheel chute (32) with thumb wheel in 90 degree scopes are back and forth stirred up and down, and last lower wing plate then is to divide up and down agitates to do.Establish operator's compartment at the middle part that is made of four poles, it is made of base plate (27) and side plate (11), and connects column sleeve pipe clamp (31) with side plate and be connected and fixed.The seat of riding of operator's compartment is an air channel under (28), it is by air intake stomatodeum housing (7), air channel housing (25), air exhausting duct housing (33) and Caudad mouth (36) are formed, flabellum (35) and gear (26) (40) parts such as (42) are housed in the air channel, flabellum push rod (9) is through connecting rod (23), pitman shaft (41) is connected with helical wheel (42), when pulling flabellum push rod (9), promptly stirring helical wheel rotates, after what gear change, can make the flabellum high speed rotating generate stronger suction wind-force amount, the part that will head on resistance air sucks the air channel and discharges backward, produce forward propulsion, play the effect of run-up boosting.Ride steering track rod (29), steering swivel (38) and turn to backguy (39) by attaching below base plate (27), the air draft direction of controlling Caudad mouth (36) reaches steering-effecting.First fulcrum of its thrust is located and become to wing plate push rod (10) and flabellum push rod (9) by being fixed in fulcrum shaft (24) between air channel housing (25) and the side plate (11).
The flying wing of this scheme is whole plate shape, and the scheme of the suitable one-way ventilating structure that adopts can have multiple, and shown here is a preferred version.It is made of the wing plate skeleton (17) that is trapezoidal lattice, places and the trapezoidal air-valve box (14) that matches in trapezoidal lattice, and with box retaining pad (18) and bail (16) it is confined interior, or adopt the method for establishing net on the two sides of wing plate to confine the air-valve box.When lifting on the wing, the air-valve box is met wind and is fallen, and produces the slit and allows top wind see through, and can reduce the air resistance that runs into when lifting on the wing plate; When wing during to lower fan, the air-valve box is held up by wind, and wind saw through below gap sealing was stoped, and obtained the power of ascending to heaven to increase air resistance.
When driving this aircraft, will from the afterbody to operator's compartment, after occupying stably, both feet step on controlling party to pedal on, the both hands branch holds push rod (9) and (10) alternately promote, the upper and lower wing just can upper flange wing plate is just to rising at present to lower fan, upper flange just interlocks to lower fan ground to the wing plate that rises at present and agitates.When wing plate was agitated, flabellum (35) rotated, and the wind-force of discharging produces the propulsive force that moves ahead backward, under the synergy of two power, flew up.Should draw with hand push and instigate the mode that wing plate agitates to rotate with flabellum and can have other to instigate mode, as: with the mode of hand traverse or by motor-driven mode (as at the gear position of Fig. 2 signal repacking electric driver) or the like.At this mode of instigating that pulls is only proposed.

Claims (2)

1, fan separated type aircraft about a kind of wing plate, it is characterized in that: its flying wing is the whole plate shape that the one-way ventilating function is arranged, it is divided into upper flange (1) and lower wing plate (2), last dress sliding sleeve (6), and make guide pillar by four poles (3) and support, it is fixing with location lath (5) and tightening screw (4), dress return pulley (30) at the bottom of the post; Upper and lower wing plate is connected with thumb wheel (13) by bearing pin (20) by the V-arrangement arm (12) (21) that is welded on the sliding sleeve (6), thumb wheel axle (15) passes sleeve pipe (19), side plate (11) is affixed with escapement bar (22), and the escapement bar other end is connected with wing plate push rod (10) through connecting rod (23); Establish operator's compartment at the middle part that is made of four poles, it is made of base plate (27) and side plate (11), and connects column sleeve pipe clamp (31) with side plate and be connected and fixed; The seat of riding of operator's compartment is an air channel under (28), it is made up of air intake stomatodeum housing (7), air channel housing (25), air exhausting duct housing (33) and Caudad mouth (36), flabellum (35) and gear (26) (40) parts such as (42) are housed in the air channel, and flabellum push rod (9) is connected with helical wheel (42) through connecting rod (23), pitman shaft (41); Attaching is ridden steering track rod (29), steering swivel (38) and is turned to backguy (39) below base plate (27); First fulcrum of its thrust is located and become to wing plate push rod (10) and flabellum push rod (9) by being fixed in fulcrum shaft (24) between air channel housing (25) and the side plate (11).
2, fan separated type aircraft about the wing plate according to claim 1, it is characterized in that: the wing plate with one-way ventilating function is to be made of the wing plate skeleton (17) that is trapezoidal lattice, and in trapezoidal lattice, place and the trapezoidal air-valve box (14) that matches, and with box retaining pad (18) and bail (16) it is confined interior, or net is established in employing on the two sides of wing plate method is confined the air-valve box.
CN 200420000892 2004-01-20 2004-01-20 Wing panel top/bottom fan separated type flight device Expired - Fee Related CN2732622Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200420000892 CN2732622Y (en) 2004-01-20 2004-01-20 Wing panel top/bottom fan separated type flight device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200420000892 CN2732622Y (en) 2004-01-20 2004-01-20 Wing panel top/bottom fan separated type flight device

Publications (1)

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CN2732622Y true CN2732622Y (en) 2005-10-12

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CN 200420000892 Expired - Fee Related CN2732622Y (en) 2004-01-20 2004-01-20 Wing panel top/bottom fan separated type flight device

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102107733B (en) * 2009-12-23 2013-12-18 姚金玉 Bionic aircraft
CN104443383A (en) * 2014-12-15 2015-03-25 佛山市神风航空科技有限公司 Flat flapping wing lifting device with servo motor
CN110920882A (en) * 2019-05-05 2020-03-27 王三保 Water-air dual-purpose helicopter
CN112389646A (en) * 2020-12-04 2021-02-23 邓辉平 Single-pass composite wing suitable for flapping wing aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102107733B (en) * 2009-12-23 2013-12-18 姚金玉 Bionic aircraft
CN104443383A (en) * 2014-12-15 2015-03-25 佛山市神风航空科技有限公司 Flat flapping wing lifting device with servo motor
CN110920882A (en) * 2019-05-05 2020-03-27 王三保 Water-air dual-purpose helicopter
CN112389646A (en) * 2020-12-04 2021-02-23 邓辉平 Single-pass composite wing suitable for flapping wing aircraft

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C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee