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CN107097947A - Flight palace - Google Patents

Flight palace Download PDF

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Publication number
CN107097947A
CN107097947A CN201710253125.9A CN201710253125A CN107097947A CN 107097947 A CN107097947 A CN 107097947A CN 201710253125 A CN201710253125 A CN 201710253125A CN 107097947 A CN107097947 A CN 107097947A
Authority
CN
China
Prior art keywords
vertical rod
seat
palace
handlebar
connecting plate
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
CN201710253125.9A
Other languages
Chinese (zh)
Inventor
曹世善
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 CN201710253125.9A priority Critical patent/CN107097947A/en
Publication of CN107097947A publication Critical patent/CN107097947A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • B64C27/10Helicopters with two or more rotors arranged coaxially
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Toys (AREA)

Abstract

Flight palace belongs to aircraft, easily transatmospheric vehicle, convenient trip, alleviate traffic above-ground pressure, the spherical shell of vertical rod lower end one, seat is interior in hanging the seat of the ball-type on the top plate of palace, can arbitrarily it tilt, rod end fixed base plate, Plane Installation vertical DC motor on seat board, arbor is upper, connect concentric double-shaft reverse fold formula DCB Specimen, torque reaction is eliminated each other, reduce rotor blade length, the danger of his thing is collided during rotor wing rotation, the space taken when ground is parked, vertical rod lower semisection, top plate and the handlebar for being respectively parallel to vertical rod and top plate, horizon bar constitutes four-bar linkage, four mechanisms of hinge can be rotated around vertical rod, handlebar, which is extended to, to be hung in utero, there is handle sleeve its end, it is axially movable, inject or exit the hole on web plate, vertical rod is set to position or conjugate, turning joint four-bar mechanism, and control crank bar, vertical rod can be tilted arbitrarily, change of flight direction, flying speed and flying height, there is speed control crank on handlebar, the rotating speed of motor and rotor can be changed, hang the flying speed and height in palace, hanging in utero has seat, seat transfers battery.

Description

Flight palace
Technical field:The present invention relates to aircraft.
Background technology:Existing aircraft is of all kinds, such as all kinds of aircrafts, space shuttle, airship, spaceship, dirigible, Balloon or even rocket, guided missile, close with the present invention is to carry the rotor in people's back on the back, and rotor wing rotation is driven by compact internal combustion engine, Buoyancy is produced, makes one to fly up, this aircraft can only be used as exercise, the vehicles should not be used as, because body burden is too heavy, There is sense of discomfort, and human body is exposed outside, it is impossible to wind sheltering rain cover, operation is also inconvenient.
The content of the invention:The purpose of the present invention is a kind of easily transatmospheric vehicle of design, and convenient trip is alleviated ground and handed over Logical pressure, and sports movement apparatus can be also served as.
The object of the present invention is achieved like this:There is a spherical shell one vertical rod lower end, and seat is in hanging the ball-type on the top plate of palace In seat, rod end fixes a seat board, vertical with vertical rod, Plane Installation vertical DC motor on seat board, and arbor is in upper, its axle Line is overlapped with vertical rod axis, arbor connection concentric double-shaft reverse fold formula DCB Specimen, and upper folding rotor with motor shaft by being connected Star-disc, with connecting plate that star-disc is hinged, the blade being fixed on connecting plate and being fixed on corresponding connecting plate in star-disc Block constitute, star-disc is connected with internal gear, and internal gear is sleeved on vertical rod by the gear on idle pulley drive pivoted housing, pivoted housing Outside, with vertical rod coaxial line, pivoted housing lower end, which is hinged at the uniform connecting plate of several circumferences, and correspondence connecting plate, block, connecting plate Upper dress blade, above-mentioned another part constitutes rotor, vertical rod hypomere, top plate and the hand for being respectively parallel to vertical rod and top plate under reverse fold formula Shank, horizon bar constitute four-bar linkage, and the lower hinge of handlebar is in sliding seat, and sliding seat can be along in being with ball-type seat The hinge of the arc guide rail movement of the heart, horizon bar and vertical rod can be rotated around vertical rod, and handlebar hypomere extends to through top plate and hangs palace Interior, its end, which is set with handle sleeve, handle jacket wall, long spire hole, and a pin is fixed on handlebar through threaded hole, handle Handlebar above set, which has below speed control crank, handle sleeve, a web plate, and hole is covered with thereon, and aperture is slightly larger than handle sleeve, web plate It is connected to and is hung on the framework of palace by ball-type hinge, hanging in utero has seat, seat decentralization battery is battery and speed control crank, electronic Electro-mechanical force is connected.
Start motor, under the action of the centrifugal force, around hinge expansion is spacing horizontal by block for folding rotor blade State, the rotation of rotor produces buoyancy, and palace and human body lift-off are hung in drive, are manipulated the handlebar and sliding seat of four-bar linkage, are made A direction is inclined in vertical rod, and flight palace is flown to the direction, the gradient of regulation and control speed control crank and vertical rod, you can adjustment flight Speed and lift-off height.
The Social benefit and economic benefit object of invention is used as transatmospheric vehicle, and flight space is infinitely broad, in length and breadth side To that can expand to the whole world, depth direction can run through whole atmosphere, and such broad space " will not block up ", and can walk Straight line distance most short between two stations, convenient trip, its implementation can alleviate the traffic pressure and traffic jam on ground significantly, Traffic accident, casualties and property loss are reduced, mitigates the medical burden of society, and people's trip can be greatlyd save and is wasted in Time on road, the time is valuable wealth, and flight palace can be used to the new projects developed athletics, enriches the life of people, The enterprise implement project, supply domestic market and international market demand, can obtain abundant economic benefit and huge foreign exchange, And can partly solve the problem of employment of society.
The brief description of the drawings present invention has the following drawings:
Fig. 1 flights palace assembly schematic diagram.
A-A profiles in Fig. 2 Fig. 1.
B-B profiles in Fig. 3 Fig. 1.
C-C profiles in Fig. 4 Fig. 1.
Fig. 5 flights palace electrical system schematic diagram.
1. blade, 2. connecting plate, 3. block, 4.4 jiaos of seats of honour of 7. motor of astrolabe 5. adjusting pad, 6. round pin 8. in figure The ball 16. of 14. times seat boards of plate 9. adapter sleeve, 10. circlip, 11. bearing cap, 12. bearing, 13. central gear 15. is protected Cover the round pin of 17. blade, 18. block, 19. bearing block, 20. bearing cap, 21. hinge sleeve, 22. flap, 23. adjusting pad 24. 25. pushing hands is the steel of 26. bearing, 27. bearing cap, 28. sliding seat, 29. framework, 30. valve, 31. seat, 32. battery 33. The spherical shell of 39. instrument case of bar 34. wheel, 35. electric part box, 36. web plate, 37. handle sleeve, 38. speed control crank 40. 41. the internal gear 49. of 47. shield of ball-type seat 42. top plate, 43. horizon bar, 44. handlebar, 45. bearing, 46. connecting plate 48. The spiral shell of 56. pivoted housing of pallet 50. idle pulley, 51. bearing, 52. idler shaft, 53. inner gear housing, 54. bearing block, 55. splicing sleeve 57. The back light 65. of 58. vertical rod of bolt, 59. 63. controller of short 60. spring washer of pin 61. charger, 62. power lock 64. is in utero The headlight 68. of 66. instrument panel lamp of illuminating lamp 67. switchs the voltage meter of 69. converter 70.
Embodiment with round pin (24) as shown in figure 1, in vertical rod (58) lower end insertion spherical shell (40), connected Connect, spherical shell (40) seat is in ball-type seat (41), and ball-type seat (41) and flap (22) are fixed on top plate (42) by bolt, seat There is annular groove at the nearly place suitable for reading of lid (22) inner face, and groove built-in ball has adjusting pad (23), adjusts ball between ball-type seat (41) and flap (22) The rotation flexibility of shell body (40), vertical rod (58) tilts 30 ° from upright position to any direction, should not be suitable for reading with flap (22) Interference, vertical rod (58) top is screwed upper base plate (8), and is connected with round pin (6), prevents thread looseness, upper base plate (8) Upper Plane Installation vertical DC motor (7), and positioned with bore, motor (7) axis is overlapped with vertical rod (58) axis, position Motor (7) axle in top connects 4 jiaos of astrolabes (4), and 4 jiaos of astrolabes (4) answer well-balanced smooth, and each angle is hinged a connecting plate (2), And have block (3) (see Fig. 2) per correspondence connecting plate (2) on angle, when connecting plate (2) by horizontal level goes to upright position upwards When, just contradicted with block (3), the inclination angle of rotor blade (1) on request is welded on connecting plate (2), above-mentioned 4 jiaos of astrolabes (4), Connecting plate (2), blade (1), block (3) constitute collapsible upper rotor, and each blade of rotor (1) branch should have equal center of gravity power Square, to ensure not rock during rotor wing rotation, 4 jiaos of astrolabes (4) have an adapter sleeve (9) to be threadedly coupled with inner gear housing (53) below, Adapter sleeve (9) top surface has window, beneficial to motor (7) ventilation and heat, has big window, loss of weight, internal tooth on inner gear housing (53) wall Wheel case (53) lower end is internal gear (48), and lower seat board (14) is linked into an integrated entity, had therebetween by 4 bolts (57) with upper base plate (8) Support set (55) is separated, and pivoted housing (56) upper end being sleeved in vertical rod (58) is supported by bearing (12), and bearing (12) seat is in lower seat In bearing block (54) on plate (14), sealed by bearing cap (11), pivoted housing (56) upper end dress circlip (10) prevents from, Pivoted housing (56) lower end connection bearing block (19), wherein dress bearing (45), and add bearing cap (20) to seal, pivoted housing (56) Shang Zhuan centers Gear (13), two symmetrical idle pulleys (50) have bearing (51), idle pulley (50) and central gear (13) therebetween on idler shaft (52) With internal gear (48) engagement, side steering is constituted, lower rotor is reversely rotated with upper rotor, cancel each other out torque reaction, due to The rotating speed of lower rotor is higher than the rotating speed of upper rotor, and is 6 blades (17), therefore blade (17) is short compared with blade (1), unsuitable during rotation Meet other objects, security is good, two semi-circular guards (16,47) are fixed on idler shaft (52), cover gear chamber, idle pulley Axle (52) head end has pallet (49), prevents central gear (13) and idle pulley (50) from coming off, and there is ring on internal gear (48) upper surface periphery Shape groove, the built-in ball of groove (15), bearing block (19) is hinged on 6 uniform connecting plates of circumference (46), connecting plate (46) by certain Tilting each connecting plate (46) of correspondence on welded corner joint blade (17), bearing block (19) has block (18) (see Fig. 3), works as connecting plate (46) plumbness is gone to by horizontality, block (18) is spacing to its, bearing block (19) and hinge, connecting plate thereon (46), blade (17), block (18) etc. constitute the lower rotor of reversion, have adjusting pad (5) between adapter sleeve (9) and motor (7), adjust The rotation flexibility of internal gear (48), vertical rod (58) hypomere and is respectively parallel to vertical rod (58) and top plate (42) at top plate (42) Handlebar (44) and horizon bar (43) constitute four-bar linkage, and handlebar (44) extends downwardly into through top plate (42) and hangs palace Interior, its lower end, which is set with handle sleeve (37), handle sleeve (37), long spire hole, and pin is fixed on handlebar (44) through threaded hole On, turning handle gloves (37), in the presence of threaded hole and pin, handle sleeve (37) axial slip on handlebar (44) changes Become the length of handlebar (44), the hole be easy to inject or exited on web plate (36), handlebar (44) lower hinge axle is mounted in sliding seat (28) on, thrust bearing (26) is filled between sliding seat (28) and top plate (42), bearing (26) is fixed on sliding seat by bearing cap (27) (28) on, sliding seat (28) can be rotated along the arc guide rail centered on ball-type seat (41), as shown in figure 4, horizon bar (43) one The jaw at end is stuck on the hinge sleeve (21) in vertical rod (58), and the end of thread of two short pins (59) is fixed on hinge by the hole on jaw On chain case (21), spring washer (60) prevents short pin (59) from releasing, during control crank bar (44), and the jaw of horizon bar (43) is around short (59) are sold to rotate, movable sleeve (28) along arc guide rail rotate when, hinge sleeve (21) is rotated around vertical rod (58), and vertical rod (58) can be to Any direction is tilted, when hanging palace stabilized flight, on handle sleeve (37) insertion web plate (36) in corresponding hole, needs change of flight shape Condition, the hole that turning handle gloves (37) are exited on web plate (36) makes sliding seat (28) be slid along guide rail, and control crank bar (44) passes through Four-bar linkage, makes vertical rod (58) be tilted to a direction, hangs palace and flies in the direction, the gradient of vertical rod (58), certainly Determine to fill speed control crank (38) on flying speed and rise, handlebar (44), adjust the rotating speed of motor (7) and two rotors, also The adjustable flying speed and flying height for hanging palace, web plate (36) is articulated with ball-type hinge to be hung on palace framework (29), Ke Yizhuan To space arbitrary orientation, it is easy to hole thereon and handle sleeve (37) centering, makes in handle sleeve (37) patchhole, handlebar (44) is fixed Position, hangs palace framework (29) top and top plate (42) connection, and two parallel arciform spring steel bars (33), steel bar (33) end are fixed in bottom surface Volume is filled in circular hole into circular hole, two parallel axles, and four wheels (34) are mounted in axle end, when hanging palace landing, spring steel bar (33) energy Play cushioning effect, wheel (34) is easy to hang palace to be moved on the ground, and the interior rear end connecting chair (31) of framework (29), its top is hung Pushing hands is connected outside palace (25), framework (29) outer packing lightweight transparent cover is easy to externally viewing, and cover side has above door, door and had There is valve (30) below window, the rear of cover, open valve (30), can be toward picking and placeing battery (32), electric power storage under seat (31) The connecting wire of pond (32) and motor (7) passes through vertical rod (58) inner chamber, and instrument case (39), left and right sides are installed in framework (29) front end Mirror after dress, front dress headlight (67), rear dress back light (64), the built-in instrument panel lamp of instrument case (66) hangs in utero dress illuminating lamp (65) (being omitted in the Fig. 1 such as cover, door, window, rear mirror, headlight (67), back light (64), illuminating lamp (65), instrument panel lamp (66)), framework (29) It is electric component case (35) at the inferior horn of front end, electrical system schematic diagram following part as shown in figure 5, be made up of:Charger (61), Power lock (62), controller (63), speed control crank (38), in utero back light (64), illuminating lamp (65), instrument panel lamp (66), headlight (67), switch (68), converter (69), voltage meter (70), battery (32).

Claims (1)

1. flight palace is a kind of aircraft, there is concentric double-shaft reverse fold formula DCB Specimen, it is characterized in that:There is a ball one vertical rod lower end Shell body, seat is in hanging in the seat of the ball-type on the top plate of palace, and rod end fixes a seat board, vertical with vertical rod, Plane Installation on seat board Vertical DC motor, arbor is upper, and its axis is overlapped with vertical rod axis, arbor connection concentric double-shaft reverse fold formula bispin The wing, upper folding rotor is by the star-disc being connected with motor shaft, the connecting plate being hinged with star-disc, the leaf being fixed on connecting plate Piece and the block composition for being fixed on correspondence connecting plate in star-disc, star-disc are connected with internal gear, and internal gear is driven by idle pulley Gear on pivoted housing, pivoted housing is sleeved on outside vertical rod, with vertical rod coaxial line, and pivoted housing lower end is hinged the uniform connecting plate of several circumferences, And have blade is filled on block, connecting plate at correspondence connecting plate, above-mentioned another part constitutes rotor under reverse fold formula, vertical rod hypomere, top Plate and handlebar, the horizon bar composition four-bar linkage for being respectively parallel to vertical rod and top plate, the lower hinge of handlebar is mounted in work On dynamic seat, sliding seat can be moved along the arc guide rail centered on ball-type seat, and the hinge of horizon bar and vertical rod can be rotated around vertical rod, Handlebar hypomere is extended to through top plate and hung in utero, its end dress handle sleeve, has speed control crank on the handlebar above handle sleeve, There is a web plate below handle sleeve, hole is covered with thereon, aperture is slightly larger than handle sleeve, and web plate is articulated with by ball-type hinge hangs palace framework On, hanging in utero has seat, and seat decentralization battery, battery is connected with speed control crank, motor power.
CN201710253125.9A 2017-04-11 2017-04-11 Flight palace Pending CN107097947A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710253125.9A CN107097947A (en) 2017-04-11 2017-04-11 Flight palace

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710253125.9A CN107097947A (en) 2017-04-11 2017-04-11 Flight palace

Publications (1)

Publication Number Publication Date
CN107097947A true CN107097947A (en) 2017-08-29

Family

ID=59656608

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710253125.9A Pending CN107097947A (en) 2017-04-11 2017-04-11 Flight palace

Country Status (1)

Country Link
CN (1) CN107097947A (en)

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2192881A (en) * 1937-12-30 1940-03-12 Helicopter Corp Of America Helicopter device
US2461347A (en) * 1945-10-17 1949-02-08 Horace T Pentecost Helicopter adapted to be attached to a pilot
US3933324A (en) * 1974-08-02 1976-01-20 Stanislaw Ostrowski Helicopter with opposite rotating torque cancelling horizontal propeller
GB1498997A (en) * 1975-10-16 1978-01-25 Ostrowski S Rotor assembly for a helicopter
CN2207997Y (en) * 1993-09-04 1995-09-20 许静峰 Single helicopter
JP2000072095A (en) * 1998-09-02 2000-03-07 Engineering System Kk Co-axial twin-rotor type helicopter
RU2226480C1 (en) * 2002-09-12 2004-04-10 ООО "Мидера-К" Flying vehicle
US20050211826A1 (en) * 2001-02-07 2005-09-29 Pai Bhaskar R Lightweight helicopter
JP2009137319A (en) * 2007-12-03 2009-06-25 Engineering System Kk Fixed pitch type coaxial double contra-rotating helicopter
CN102211663A (en) * 2011-05-11 2011-10-12 王略 Gear tilting type coaxial machine
CN102490900A (en) * 2011-12-07 2012-06-13 陈拥隽 Small individual aircraft with folding rotor wings
CN203581382U (en) * 2013-11-05 2014-05-07 廖欣 Small-size coaxial twin-rotor manned helicopter

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2192881A (en) * 1937-12-30 1940-03-12 Helicopter Corp Of America Helicopter device
US2461347A (en) * 1945-10-17 1949-02-08 Horace T Pentecost Helicopter adapted to be attached to a pilot
US3933324A (en) * 1974-08-02 1976-01-20 Stanislaw Ostrowski Helicopter with opposite rotating torque cancelling horizontal propeller
GB1498997A (en) * 1975-10-16 1978-01-25 Ostrowski S Rotor assembly for a helicopter
CN2207997Y (en) * 1993-09-04 1995-09-20 许静峰 Single helicopter
JP2000072095A (en) * 1998-09-02 2000-03-07 Engineering System Kk Co-axial twin-rotor type helicopter
US20050211826A1 (en) * 2001-02-07 2005-09-29 Pai Bhaskar R Lightweight helicopter
RU2226480C1 (en) * 2002-09-12 2004-04-10 ООО "Мидера-К" Flying vehicle
JP2009137319A (en) * 2007-12-03 2009-06-25 Engineering System Kk Fixed pitch type coaxial double contra-rotating helicopter
CN102211663A (en) * 2011-05-11 2011-10-12 王略 Gear tilting type coaxial machine
CN102490900A (en) * 2011-12-07 2012-06-13 陈拥隽 Small individual aircraft with folding rotor wings
CN203581382U (en) * 2013-11-05 2014-05-07 廖欣 Small-size coaxial twin-rotor manned helicopter

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
柯热夫尼柯夫: "《机构参考手册》", 31 March 1981, 机械工业出版社 *

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Application publication date: 20170829