Long-cylinder parking rack for aircrafts on aircraft carrier

Long-cylinder parking rack for aircrafts on aircraft carrier

  • CN 106,586,019 A
  • Filed: 12/12/2016
  • Published: 04/26/2017
  • Est. Priority Date: 12/12/2016
  • Status: Active Application
First Claim
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1. the long cylinder stand of a kind of aircraft carrier, comprising frame body (1);

  • It is characterized in that:

    The long cylinder stand of the aircraft carrier also includes axle bed, motor, actuating device;

    Frame body (1) is by front plectane (3), middle plectane (20), rear plectane (4), cylinder (6), ball (7), rotating shaft (9), sleeve(10) constitute;

    Front plectane (3), middle plectane (20), rear plectane (4) are identical plectane, their dead in line, middle plectane (20) positionIn the front plectane (3) and the centre of the rear plectane (4);

    The front plectane (3), the middle plectane (20), the rear plectane(4) there are a central shaft hole (8), multiple identical circular holes (5), the front plectane (3), the middle plectane (20), the rear circle onThe internal diameter of the central shaft hole (8) on plate (4) is equal, the circular hole (5) on the middle plectane (20) and the front plectane (3) or describedCircular hole (5) specular on plectane (4) afterwards;

    The internal diameter of circular hole (5) is more than the maximum transversal width after aircraft carrier wing-foldingDegree, there is circle hole groove (5a), the axis of circle hole groove (5a) groove bottom and the axis weight of the circular hole (5) on its circumferential surfaceClose;

    Each Nidus Vespae in Nidus Vespae mathematical model is surrounded by 6 Nidus Vespae faces, and the Nidus Vespae on the Nidus Vespae mathematical model transverse section is horizontalSection is all size identical regular hexagon;

    During frame body (1) is gone forward on plectane (3) or middle plectane (20) or rear plectane (4)Arbor hole (8) and circular hole (5) are arranged according to Nidus Vespae mathematical model:

    After the front plectane (3) or the middle plectane (20) or describedThere is the virtual Nidus Vespae mathematical model transverse section of identical to illustrate (2) on plectane (4), the front plectane (3) or the middle plectane(20) or the rear plectane (4) axis it is horizontal by the central Nidus Vespae in the diagram of virtual Nidus Vespae mathematical model transverse section thereon (2)The center of section, central Nidus Vespae of the central shaft hole (8) in virtual Nidus Vespae mathematical model transverse section diagram (2) is horizontalIn section, and the center that its axis passes through the central Nidus Vespae transverse section;

    The Nidus Vespae being located around the central shaft hole (8) is cross-sectionThere is the individual Nidus Vespae transverse section of N=3n (n+1) in face, and the n is positive integer, similarly hereinafter;

    In the individual Nidus Vespae transverse section of the N=3n (n+1)In each Nidus Vespae transverse section on have a circular hole (5), have N=3n (n+1) individual circular holes (5), the axis of circular hole (5) passes throughThe center of the Nidus Vespae transverse section that the circular hole (5) is located, the diameter of the circular hole (5) less than in Nidus Vespae transverse section toward each other andThe distance between two parallel sides;

    In the individual circular hole (5) of the N=3n (n+1), 6 ×

    1=6 circular hole (5) is located at respectively centerIn one of 6 Nidus Vespae transverse section on the outside of the Nidus Vespae transverse section of axis hole (8) place and adjacent, this 6 circular hole (5) compositions the 1st are enclosed;

    6 ×

    2=12 circular hole (5) is located at respectively on the outside of 6 circular hole (5) places Nidus Vespae transverse section of the described 1st circle and adjacent 12In one of individual Nidus Vespae transverse section, this 12 circular hole (5) compositions the 2nd are enclosed;

    6 ×

    3=18 circular hole (5) is respectively positioned at the described 2nd circle12 circular hole (5) places Nidus Vespae transverse section on the outside of and in one of adjacent 18 Nidus Vespae transverse section, this 18 circular hole (5) groupsInto the 3rd circle;

    6n circular hole (5) is located at respectively on the outside of individual circular hole (5) the place Nidus Vespae transverse section of 6 (n-1) of (n-1) circle and phaseIn one of 6n adjacent Nidus Vespae transverse section, this 6n circular hole (5) composition n-th is enclosed;

    The internal diameter of sleeve (10) is equal to the external diameter of front plectane (3) or middle plectane (20) or rear plectane (3), and its axial length is more than boat2 times of female aircraft longitudinal length;

    The circumferential surface of the front plectane (3) is fastened with the inner circumferential surface of the sleeve (10) and connectedConnect, and the front disc of the front plectane (3) is flushed with the front end face of the sleeve (10);

    The circumferential surface of the middle plectane (20)Fasten with the inner circumferential surface of the sleeve (10) and be connected, its be located at axially central and its axis of the sleeve (10) with it is describedThe dead in line of sleeve (10);

    The circumferential surface of the rear plectane (4) is fastened with the inner circumferential surface of the sleeve (10) and is connected,And the rear disc of the rear plectane (4) is flushed with the rear end face of the sleeve (10);

    Have on cylinder (6) shutdown plate (11), stop annulus (12), fagging (13), air purifier (14), front shroud (15), afterCover plate (16), guide rod plate (17), arresting lever (18);

    The external diameter of cylinder (6) less than on plectane (3) before frame body (1) or middle plectane (20) or rear plectane (4) circular hole (5) it is interiorFootpath, the axial length of the cylinder (6) is more than the axial length of the frame body (1) upper bush (10);

    The middle plectane (20)Each circular hole (5) in have a cylinder (6), the front end of the cylinder (6) is from the circular hole with the middle plectane (20)(5) pass in the circular hole (5) of the described front plectane (3) of specular, the rear end of the cylinder (6) from the middle plectane (20)Circular hole (5) specular described rear plectane (3) circular hole (5) in pass;

    Circle hole groove (5a) and corresponding positions on circular hole (5)Have multiple balls (7) between the external peripheral surface of the cylinder (6) in the circular hole (5) put, one of this multiple ball (7) both with phaseAnswer the groove bottom movable contact of the circle hole groove (5a) of position, but with the external peripheral surface of the cylinder (6) of relevant positionMovable contact;

    The internal diameter of one of two stop annulus (12) is equal to the external diameter of cylinder (6), and its external diameter is more than front plectane (3) or middle plectane(20) internal diameter of circular hole (5) or on rear plectane (4);

    The two stop annulus (12) be set in the close two ends of cylinder (6) itOn one external peripheral surface, and it is connected with external peripheral surface fastening of relevant position, near the cylinder (6) front endThe front disc movable contact of the rear anchor ring of the stop annulus (12) and the described front plectane (3) of relevant position, positioned at the circleThe front anchor ring of the stop annulus (12) near cylinder (6) rear end is movable with the rear disc of the described rear plectane (4) of relevant positionContact;

    The shutdown plate (11) for parking aircraft carrier is rectangular slab, and its longitudinal length is equal to the axial length of cylinder (6), and its is laterally wideDegree is less than the internal diameter of the cylinder (6) and more than the distance between trailing wheel of aircraft carrier two, and it is shelved on circle described in relevant positionOn the inner circumferential surface of cylinder (6), the diameter parallel of the longitudinal midline (11c) on its upper surface and the cylinder (6), its front end faceFlush with the front end face of the cylinder (6), thereafter end face is flushed with the rear end face of the cylinder (6), the shape of one of its two sidesShape is corresponding with the shape of the inner circumferential surface of the cylinder (6) of contact and fastening connects;

    Shutdown plate (11) upper surfaceOne of both sides fasten two pieces of horizontal guide rod plates (17) of connection, and one piece of guide rod plate (17) is positioned at the longitudinal direction of shutdown plate (11)Middle part, Jie Jin the front end of shutdown plate (11), the bottom of the guide rod plate (17) has one to another piece of guide rod plate (17)Longitudinal circular hole, the upper surface that the circular hole shuts down plate (11) with relevant position is tangent, and external diameter is equal to the cylinder of the bore inner diameter to be stoppedLever (18) is in the circular hole of one of this two pieces of guide rod plates (17) and can move axially forward, the arresting lever (18)Axial length is more than distance between this two pieces of guide rod plates (17) and less than shutdown plate (11) longitudinal length;

    Two front pores(11a) one of described shutdown plate (11) front upper surface both sides are located at respectively and and positioned at the interior of relevant position arresting lever (18)Side, the lateral center at shutdown plate (11) rear portion has vertical posterior spiracle (11b);

    When two frame aircraft carriers are parked in the shutdown plate(11) when on, the front-wheel Jie Jin the aircraft carrier of shutdown plate (11) rear end is located at the front of the posterior spiracle (11b), is close toTwo trailing wheels of the aircraft carrier for shutting down plate (11) front end are located between the two front pores (11a).Shut down in cylinder (6) and have below plate (11) polylith fagging (13), one of fagging (13) is close to shuts down plate (11)Front end, remaining fagging (13) is scattered in the middle part of shutdown plate (11);

    One of this polylith fagging (13) be cambered plate, its levelThe transverse width of upper surface is equal to the transverse width of shutdown plate (11) lower surface, and its lower surface is cambered surface;

    Stop positioned at describedFagging (13) in the middle part of machine plate (11), its upper surface is fastened with the lower surface of the shutdown plate (11) of relevant position and is connected, itsCambered surface is in close contact with the inner circumferential surface of the cylinder (6) bottom of relevant position, has longitudinal fagging on these faggings (13)Pore (13a);

    Under shutdown plate (11) Jie Jin the fagging (13) of shutdown plate (11) front end, its upper surface and relevant positionSurface fastens connection, and its cambered surface is fastened with the inner circumferential surface of the cylinder (6) bottom of relevant position and is connected, the shutdown plate(11) front port of cavity is in sealing state between lower surface and the inner circumferential surface of the opposed cylinder (6) bottom;

    The upper end of front shroud (15) is movably connected in the top of the inner circumferential surface of the close front end of cylinder (6) by secure fit deviceOn, it stretches out in the outer front of the cylinder (6) when being in horizontality, and it is located at the cylinder (6) when being in vertical stateClose in the interior cavity for shutting down the close front end in plate (11) top and by the cavity;

    The code name (19) of the cylinder (6) is written on instituteState on the front surface of front shroud (15);

    Back shroud (16) is circular slab, and its external diameter is more than the external diameter of cylinder (6);

    After the rear end face of cylinder (6) and relevant positionThe front disc of cover plate (16) fastens connection, the axis of the cylinder (6) and the dead in line of the back shroud (16), the cylinder(6) rear end face of plate (11) is shut down in and is fastened with the front disc of the back shroud (16) of relevant position and be connected;

    Air purifier (14) is fastened and is connected in cylinder (6) cylinder shut down on plate (11) immediately below posterior spiracle (11b)(6) on inner circumferential surface;

    Rotating shaft (9) is described in the central shaft hole (8) that frame body (1) goes forward plectane (3), middle plectane (20), rear plectane (4)Front plectane (3), the middle plectane (20), the rear plectane (4) are snugly arranged in the rotating shaft (9), Huo ZheyuThe rotating shaft (9) is fixed together;

    The two ends of the rotating shaft (9) are respectively from one of described frame body (1) two ends to overhangingGo out;

    There is rectangular indentation the close edge of type aircraft carrier deck, and the length of side on the long side of the breach is outer more than frame body (1) upper bush (10)Footpath, the length of side of the breach minor face is more than the axial length of cylinder (6) on the frame body (1);

    Frame body (1) is installed in the breachIt is interior, on the frame body (1) in the breach front end face of cylinder (6) towards the type aircraft carrier deck middle part and with it is correspondingThe side movable contact of position breach;

    One of two ends of rotating shaft (9) are arranged on axle bed, the axis of the rotating shaft (9) and the relative altitude of type aircraft carrier deck upper surfaceSo select:

    The axis of arbitrarily cylinder (6) is located at the surface of rotating shaft (9) axis on the frame body (1) in the 1st circle on frame body (1)When, the upper surface of upper surface and type aircraft carrier deck that plate (11) is shut down in the cylinder (6) is located at same level, the rotating shaft(9) axis place horizontal plane is the relative altitude upper limit level face of the rotating shaft (9) axis and the type aircraft carrier deck upper surface;

    The axis of arbitrarily cylinder (6) is located at the lower section of rotating shaft (9) axis on the frame body (1) in the 1st circle on frame body (1)When, the upper surface of upper surface and type aircraft carrier deck that plate (11) is shut down in the cylinder (6) is located at same level, and from describedShut down critical state of the aircraft carrier of plate (11) upper surface turnover in not hindered by axle bed, the axis institute of the rotating shaft (9)In the relative altitude threshold level face that horizontal plane is the rotating shaft (9) axis and the type aircraft carrier deck upper surface;

    The relative altitude of rotating shaft (9) axis is selected between the upper limit level face and the threshold level face;

    On frame body (1) axis of any one cylinder (6) with the axis of rotating shaft (9) on the frame body (1) in same levelWhen on face, the upper surface of upper surface and type aircraft carrier deck that plate (11) is shut down in the cylinder (6) is located at same level, described turnAxle (9) axis is optimal relative altitude with the relative altitude of the type aircraft carrier deck upper surface;

    For this purpose, the bottom surface of two axle beds fastens respectively the aircraft carrier for being connected to one of long side of breach two central lateral in type aircraft carrier deckOn the upper surface on deck;

    Rotating shaft (9) from frame body (1) go forward plectane (3) external part be arranged on the type aircraft carrier deck on be close toOn axle bed in the middle part of the aircraft carrier, the rotating shaft (9) external part of rear plectane (4) from the frame body (1) is arranged on describedIn type aircraft carrier deck on the axle bed at close aircraft carrier edge, one of the rotating shaft (9) and this two axle bed are fastened and are connected, or with this two axleOne of seat is fixed together;

    The axis of the axis of any one cylinder (6) and the rotating shaft (9) on the frame body (1)When in same level, the upper surface of upper surface and the type aircraft carrier deck that plate (11) is shut down in the cylinder (6) is located at togetherOne horizontal plane;

    The frame body (1) can rotate around the axis of the rotating shaft (9) in the breach of the type aircraft carrier deck;

    Motor is fastened in the fixed platform on the aircraft carrier of frame body (1) lower section, or is fastened installed in frame body (1) sideType aircraft carrier deck on;

    Actuating device is made up of tooth annulus, power output gear;

    The internal diameter of the tooth annulus being formed by connecting by polylith arc-shaped rack is equal to the external diameter of frame body (1) upper bush (10), its suitIn the axially central authorities of the sleeve (10) external peripheral surface, it fastens with the external peripheral surface of sleeve described in relevant position (10) and connectsConnect;

    Power output gear is fastened on the axle of motor;

    The power output gear is nibbled with the tooth annulus on sleeve (10)Close.

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