CN106564589A - Fixed rotary wing rotary aircraft - Google Patents

Fixed rotary wing rotary aircraft Download PDF

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Publication number
CN106564589A
CN106564589A CN201610679553.3A CN201610679553A CN106564589A CN 106564589 A CN106564589 A CN 106564589A CN 201610679553 A CN201610679553 A CN 201610679553A CN 106564589 A CN106564589 A CN 106564589A
Authority
CN
China
Prior art keywords
wing
thick stick
stick axle
aircraft
rotation
Prior art date
Application number
CN201610679553.3A
Other languages
Chinese (zh)
Inventor
申俊勇
Original Assignee
申俊勇
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
Priority to CN2015106617936 priority Critical
Priority to CN201520793767 priority
Priority to CN201510661793.6A priority patent/CN105346717A/en
Priority to CN2015207937674 priority
Priority to CN2016207954176 priority
Priority to CN2016105909607 priority
Priority to CN201610590960 priority
Priority to CN201620795417 priority
Application filed by 申俊勇 filed Critical 申俊勇
Publication of CN106564589A publication Critical patent/CN106564589A/en

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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

Abstract

The invention relates to a fixed rotary wing rotary aircraft. The fixed rotary wing rotary aircraft comprises an aircraft body, a lever shaft, a rotary hub, and fixed rotary wings, wherein the aircraft body is in a rectangular warehouse structure and is a carrier for supporting and fixing components, structures and systems, a control system is arranged on two side walls of the aircraft body, and structure in which the level shaft and the rotary hub are arranged is arranged at the upper end of the aircraft body; the lever shaft is laterally arranged at the upper ends of the two side walls of the aircraft body and can rotate; the fixed rotary wings are arranged on two sides of the aircraft body and are fixedly connected with the lever shaft and can rotate; and the rotary hub is arranged at a connection part of the upper ends of the two side walls of the aircraft body and the lever shaft, and the rotary hub adjusts and controls the posture of the fixed rotary wings by controlling the rotation of the lever shaft, so that transition and control on the flight attitude of the aircraft can be further realized. The fixed rotary wing rotary aircraft is safe and reliable in the transition process of the flight attitude, and is better than an American Osprey rotary wing transport aircraft.

Description

Gu rotor wing rotation aircraft
Technical field
The present invention relates to the construction and structure of the solid rotor wing rotation aircraft in aircraft field.
Technical background
At present, the osprey rotor transporter in the U.S., has broken traditional design concept, has realized fixed wing airplane and spiral The combination of wing aircraft so as to which bigger than traditional sling load, flight speed is fast;It is bigger than traditional transporter take-off weight, Landing is apart from short.But osprey rotor transporter Frequent Accidents in the transition process of flight attitude;Osprey rotor transporter is consolidated Alar part is determined below its rotor, affect its take-off weight.
The content of the invention
The present invention have developed a kind of solid rotor of the type for the shortcomings and deficiency of U.S.'s osprey rotor transporter Rotation aircraft.Which includes body (1), thick stick axle (2), rotation pivot (3), solid rotor (4).It is characterized in that:1st, U.S. osprey rotor transport Machine is located at the rotary apparatuss of rotor and rotor on the wing tip of fixed-wing, due to position it is special, its rotary apparatus be subject to it is various because The restriction of element, it is not mature enough so far.Osprey rotor transporter still Frequent Accidents in the transition process of flight attitude, its persistent ailment It is difficult to solve.This patent is by the rotary apparatuss of solid rotor (4) --- rotation pivot (3) is located at the weight in the middle of body (1) two side upper end Heart position and the junction of thick stick axle (2).The sidewall area of this body (1) is big relative to the wing tip area of osprey rotor transporter It is many, photoelectricity control system is set on the two side of this body (1) or mechanical manipulation system is easy for much, therefore this consolidates rotor Rotation aircraft is safe and reliable in the transition process of flight attitude, perfectly safe.2nd, the fixed alar part of osprey rotor transporter Below its rotor, take-off weight is affected.The former fixed-wing of the machine both sides is separated by this patent with body (1), former fixed-wing one End is connected and rotatable with thick stick axle (2), is changed into rotary wings from original fixed-wing;Screw wing (or turbofan) electromotor is connected The centre or outer end for being fixed on former fixed-wing is connect, solid rotor (4) is made;Wing edge and screw wing (or turbofan) of former fixed-wing Electromotor is vertical, therefore windage area very little, does not affect take-off weight.3rd, osprey rotor transporter awing, its fixed-wing Lift it is limited, the screw wing must need upwardly and forwardly two gravitation simultaneously, therefore affect flight speed.The spiral shell of this patent Rotor (or turbofan) electromotor is connected and fixed on the centre of former fixed-wing and constitutes solid rotor (4), the length and width of former fixed-wing Degree is unrestricted, can provide enough lift with aircraft.This is consolidated the in-flight screw wing of rotor wing rotation aircraft (or turbofan) and sends out Motivation is only needed to previous gravitation, therefore flight speed is faster.4th, the rotating dress of the rotor and rotor of osprey rotor transporter It is set on the wing tip of fixed-wing, therefore limits the setting quantity of rotor, a frame osprey rotor transporter can only arranges two Screw wing electromotor.Screw wing (or turbofan) electromotor is connected and fixed on this patent the centre position of former fixed-wing, former fixed The chord of the wing is unrestricted, and the setting quantity of screw wing (or turbofan) electromotor is also just unrestricted.Therefore, the solid rotor rotation of a frame Feeder aircraft can arrange Liang Tai, four, six or more multiple stage screw wing (or turbofan) electromotor.5th, this consolidates rotor wing rotation airframe (1) length is unrestricted, can respectively set a row or multi-row solid rotor (4) in the both sides of body (1).6th, this consolidates rotor wing rotation aircraft Can also two kinds of power of dual-purpose screw wing electromotor or fanjet.This consolidate rotor wing rotation aircraft merged transporter, helicopter, The different types of machines such as amphibious aircraft, ground effect wing aircraft, have played the flight advantage and potential of different types of machines, have spanned various machines The flying area of type, adapts to Various Complex flight environment of vehicle.This consolidates rotor wing rotation aircraft safety in the transition process of flight attitude Reliable, perfectly safe, and take-off weight is big, apart from short, flight speed is fast, adapts to spatial domain wide for landing.This is consolidated rotor wing rotation and flies Machine is the aerial basic platform of a tractor serves several purposes, can retrofit fuel charger, early warning plane, reconnaissance plane, antisubmarine plane etc..This is consolidated rotor wing rotation and flies Machine can also fall back and turn-take with original place, be more suitable for complicated ground condition landing narrow and small in aircraft carrier, warship etc..Generally speaking this consolidates rotor rotation Feeder aircraft is better than U.S.'s osprey rotor transporter.
Embodiments of the present invention is further illustrated below in conjunction with the accompanying drawings
Front views of the Fig. 1 for solid rotor wing rotation airframe (1)
Top views of the Fig. 2 for solid rotor wing rotation airframe (1)
Front views of the Fig. 3 for solid rotor wing rotation aircraft thick stick axle (2)
Top views of the Fig. 4 for solid rotor wing rotation aircraft thick stick axle (2)
The front view of Fig. 5 A, B for solid rotor wing rotation aircraft rotation pivot (3)
The top view of Fig. 6 A, B for solid rotor wing rotation aircraft rotation pivot (3)
The front view of Fig. 7 A, B for the solid rotor (4) of solid rotor wing rotation aircraft
The top view of Fig. 8 A, B for the solid rotor (4) of solid rotor wing rotation aircraft
The embodiment of the present invention includes body (1), thick stick axle (2), rotation pivot (3), solid rotor (4).It is characterized in that:Body (1) is Rectangle warehouse is constructed, and is to support, fix each part, structure, the carrier of system, photoelectricity manipulation is set on the two side of body (1) System or mechanical manipulation system, the position of centre of gravity in the middle of body (1) the two side upper end set fixed thick stick axle (2) and rotation pivot (3) Thick stick axle (2) and rotation pivot (3) are connected and rotatable by construction, the construction.Thick stick axle (2) is laterally located on body (1) two side Position of centre of gravity in the middle of end, the position of centre of gravity in the middle of thick stick axle (2) and body (1) the two side upper end set the structure of fixed thick stick axle (2) Make, thick stick axle (2) is connected and rotatable by the construction;Thick stick axle (2) left and right two ends are connected with solid rotor (4);Thick stick axle (2) For tubular type or square-tube type, petroleum pipeline, cable, holding wire in which, are set;Thick stick axle (2) can be set to entire body or two sections, thick stick axle (2) two End sets connecting rod or gear, and the junction of the position of centre of gravity in the middle of thick stick axle (2) and body (1) two side upper end sets rotation pivot (3).Rotation pivot (3) junction of the position of centre of gravity in the middle of body (1) two side upper end and thick stick axle (2) is located at, in thick stick axle (2) and body (1) two The junction of the position of centre of gravity in the middle of sidewall upper sets the construction of fixed rotation pivot (3), and rotation pivot (3) is connected and can by the construction Rotation:Pivot (3) is revolved by thick stick axle (2) and the connecting rod or gear at thick stick axle (2) two ends, with the center of gravity in the middle of body (1) two side upper end Position fix the construction of rotation pivot (3), photoelectricity control system on body (1) two side or mechanical manipulation system connection combination and Into.Gu rotor (4) is located at the both sides of body (1) and is connected with thick stick axle (2);Former fixed-wing is separated with body (1), former fixed Wing one end is connected and rotatable with thick stick axle (2), is changed into rotary wings from original fixed-wing;Screw wing (or turbofan) electromotor The centre or outer end of former fixed-wing are connected and fixed on, solid rotor (4) is made.Gu rotor (4) is fixed by thick stick axle (2) and original The wing, the connection of screw wing (or turbofan) electromotor are combined.Can set on the former fixed-wing of body (1) both sides Liang Tai, four, six Or more multiple stage screw wing (or turbofan) electromotor;Body (1) both sides can respectively set a row or multi-row solid rotor (4).This consolidates rotor rotation Feeder aircraft can also two kinds of power of dual-purpose screw wing electromotor or fanjet.
Specific embodiment
The explanation embodiment of the present invention of Fig. 1,2,3,4,5,6,7,8 includes body (1), thick stick axle (2), rotation pivot (3), solid rotor (4).Its specific embodiment is:Photoelectricity control system or mechanical manipulation system are set on the two side of body (1), in body (1) position of centre of gravity in the middle of the upper end of two side sets the construction of fixed thick stick axle (2) and rotation pivot (3), and the construction is by thick stick axle (2) and revolves pivot (3) it is connected and rotatable.Thick stick axle (2) is laterally located at the position of centre of gravity in the middle of body (1) two side upper end, in thick stick axle (2) The construction of fixed thick stick axle (2) is set with the position of centre of gravity in the middle of body (1) two side upper end, thick stick axle (2) is connected by the construction And it is rotatable;Thick stick axle (2) left and right two ends are connected with solid rotor (4);Thick stick axle (2) is tubular type or square-tube type, sets defeated in which Oil pipe, cable, holding wire;Thick stick axle (2) can be set to entire body or two sections, and thick stick axle (2) two ends set connecting rod or gear, thick stick axle (2) with The junction of the position of centre of gravity in the middle of body (1) two side upper end sets rotation pivot (3).Rotation pivot (3) is located at body (1) two side upper end The junction of middle position of centre of gravity and thick stick axle (2), the position of centre of gravity in the middle of the thick stick axle (2) with body (1) two side upper end Junction sets the construction of fixed rotation pivot (3), and the construction will revolve pivot (3) and be connected and rotatable;Rotation pivot (3) by thick stick axle (2) and Position of centre of gravity in the middle of the connecting rod or gear at thick stick axle (2) two ends, with body (1) two side upper end fixes the construction of rotation pivot (3), machine Photoelectricity control system or mechanical manipulation system connection on body (1) two side is combined.Gu rotor (4) is located at body (1) Both sides are simultaneously connected with thick stick axle (2);Former fixed-wing is separated with body (1), and former fixed-wing one end is connected simultaneously with thick stick axle (2) It is rotatable, rotary wings are changed into from original fixed-wing;Screw wing (or turbofan) electromotor is connected and fixed on the centre of former fixed-wing Or outer end, make solid rotor (4).Gu rotor (4) is connected by thick stick axle (2) and former fixed-wing, screw wing (or turbofan) electromotor Connect and combine.Liang Tai, four, six or more multiple stage screw wing (or turbofan) can be set on the former fixed-wing of body (1) both sides Motivation;Body (1) both sides can respectively set a row or multi-row solid rotor (4).This consolidate rotor wing rotation aircraft can also dual-purpose screw wing start Two kinds of power of machine or fanjet.

Claims (7)

1. a kind of to consolidate rotor wing rotation aircraft, which includes body (1), thick stick axle (2), rotation pivot (3), solid rotor (4);It is characterized in that:Machine Body (1) is that rectangle warehouse is constructed, and is to support, fix each part, structure, the carrier of system;Light is set on the two side of body (1) Electric control system or mechanical manipulation system, the position of centre of gravity in the middle of body (1) two side upper end set fixed thick stick axle (2) and rotation Thick stick axle (2) and rotation pivot (3) are connected and rotatable by the construction of pivot (3), the construction;Thick stick axle (2) is laterally located at body (1) two Position of centre of gravity in the middle of sidewall upper, thick stick axle (2) left and right two ends are connected with solid rotor (4);Rotation pivot (3) is located at body (1) The junction of position of centre of gravity and thick stick axle (2) in the middle of the upper end of two side;Gu rotor (4) is located at the both sides of body (1), with thick stick axle (2) it is connected and rotatable;Multiple stage electromotor can be set on former fixed-wing;A row or multi-row solid rotation can be set in body (1) both sides The wing (4);The machine can two kinds of power of dual-purpose.
2. the solid rotor wing rotation aircraft according to claims 1, is characterized in that:Thick stick axle (2) is laterally located at body (1) both sides Position of centre of gravity in the middle of wall upper end, the position of centre of gravity in the middle of thick stick axle (2) with body (1) two side upper end set fixed thick stick axle (2) Construction, thick stick axle (2) is connected and rotatable by the construction;Thick stick axle (2) left and right two ends are connected with solid rotor (4);Thick stick Axle (2) is tubular type or square-tube type, and petroleum pipeline, cable, holding wire are set in which;Thick stick axle (2) can be set to entire body or two sections, thick stick axle (2) two ends set connecting rod or gear, and thick stick axle (2) sets rotation pivot (3) with body (1) two side upper end junction.
3., according to the solid rotor wing rotation aircraft described in root claims 1, it is characterized in that:Rotation pivot (3) is located on body (1) two side The junction of position of centre of gravity and thick stick axle (2) in the middle of end, the position of centre of gravity in the middle of thick stick axle (2) with body (1) two side upper end Junction set the construction of fixed rotation pivot (3), the construction will revolve pivot (3) and be connected and rotatable;Rotation pivot (3) is by thick stick axle (2) The construction of rotation pivot (3) is fixed with the position of centre of gravity in the middle of the connecting rod or gear at thick stick axle (2) two ends, with body (1) two side upper end, Photoelectricity control system or mechanical manipulation system connection on body (1) two side is combined.
4. the solid rotor wing rotation aircraft according to claims 1, is characterized in that:Gu rotor (4) is located at the both sides of body (1) And be connected with thick stick axle (2);Former fixed-wing is separated with body (1), and former fixed-wing one end is connected and can be revolved with thick stick axle (2) Turn, rotary wings are changed into from original fixed-wing:Screw wing (or turbofan) electromotor is connected and fixed on the centre of former fixed-wing or outer End, makes solid rotor (4);Gu rotor (4) is by thick stick axle (2) and former fixed-wing, screw wing (or turbofan) electromotor connection group Conjunction is formed.
5. the solid rotor wing rotation aircraft according to claims 1, is characterized in that:The wing of the former fixed-wing of body (1) both sides Length is unrestricted, and Liang Tai, four, six or more multiple stage screw wing (or turbofan) can be set on the former fixed-wing of body (1) both sides Electromotor.
6. the solid rotor wing rotation aircraft according to claims 1, is characterized in that:The length of body (1) is unrestricted, in machine The both sides of body (1) can respectively set a row or multi-row solid rotor (4).
7. the solid rotor wing rotation aircraft according to claims 1, is characterized in that:This consolidates rotor wing rotation aircraft can dual-purpose spiral Two kinds of power of wing electromotor or fanjet.
CN201610679553.3A 2015-10-07 2016-08-12 Fixed rotary wing rotary aircraft CN106564589A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
CN2015106617936 2015-10-07
CN201520793767 2015-10-07
CN201510661793.6A CN105346717A (en) 2015-10-07 2015-10-07 Fixed-rotor rotation apparatus
CN2015207937674 2015-10-07
CN2016105909607 2016-07-18
CN2016207954176 2016-07-18
CN201610590960 2016-07-18
CN201620795417 2016-07-18

Publications (1)

Publication Number Publication Date
CN106564589A true CN106564589A (en) 2017-04-19

Family

ID=58532247

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610679553.3A CN106564589A (en) 2015-10-07 2016-08-12 Fixed rotary wing rotary aircraft

Country Status (1)

Country Link
CN (1) CN106564589A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203842313U (en) * 2014-04-22 2014-09-24 江阴市翔诺电子科技有限公司 Novel remote control model with combination of vertical take-off and landing and level fight characteristic of fixed wing
CN104477377A (en) * 2014-12-31 2015-04-01 北京航空航天大学 Composite type multi-mode multi-purpose aircraft
CN204452934U (en) * 2015-02-05 2015-07-08 仉军 The double mode aircraft of rotor, fixed-wing
CN204507265U (en) * 2015-02-12 2015-07-29 中电科(德阳广汉)特种飞机系统工程有限公司 Be with the multi-rotor aerocraft of the fixed-wing that verts

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203842313U (en) * 2014-04-22 2014-09-24 江阴市翔诺电子科技有限公司 Novel remote control model with combination of vertical take-off and landing and level fight characteristic of fixed wing
CN104477377A (en) * 2014-12-31 2015-04-01 北京航空航天大学 Composite type multi-mode multi-purpose aircraft
CN204452934U (en) * 2015-02-05 2015-07-08 仉军 The double mode aircraft of rotor, fixed-wing
CN204507265U (en) * 2015-02-12 2015-07-29 中电科(德阳广汉)特种飞机系统工程有限公司 Be with the multi-rotor aerocraft of the fixed-wing that verts

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