TH76019B - Self-detaching integrated gyro gyro - Google Patents

Abstract

Revised 12/16/2015 The self-detachable gyro top of this invention has The peculiarity that The gyro is made by connecting at least two gyro vertically, and all gyro ends are flexible ends so that the upper gyro in it disengages. It automatically enters the lower gyro when impacted or rotated, it is interrupted during rotation, and the upper gyro is ejected according to the action of the flexible tip to produce the gyro that Two separate spins During the play according to this invention The gyro may be divided into gyro. Two or three during a face-to-face match, greatly increasing the aggressiveness of the gyro and It has a higher win rate, also because the gyro tip is a flexible tip during split and split while playing. The upper gyro is generally divided according to its elastic condition. The end of the said thing And has little impact on the lower gyro. Moreover, when landing, the upper gyro may have the ability to make a gentle landing by using the buffering effect of the condition. Flexibility to help protect the tip and maintain effective rotation stability. -------------------------------------------------- ------ The fully automatic detachment gyro type of this invention has The peculiarity of that: the gyro is made by connecting at least two gyro vertically, and all gyro ends are flexible ends so that the upper gyro in it disengages. It is interrupted during rotation, and the upper gyro is ejected according to the action of the flexible tip to produce a powerful gyro. Two separate spins During the play according to this invention The gyro may be divided into gyro. Two or three during a face-to-face match, which greatly increases the aggressiveness of the gyro and It has a higher win rate, also because the gyro tip is a flexible tip during split and split while playing. The upper gyro is generally divided according to its elastic condition. The end of the said thing And has little impact on the lower gyro. Moreover, when dropped to the upper gyro, it may have the ability to land smoothly using the buffering effect of the condition. Flexibility to help protect the tip and maintain effective rotation stability:

Claims (5)

Disclaimer (all) which will not appear on the advertisement page. : ------ 08/03/2019 ------ (OCR) Page 1 of 4 pages Disclaimer 1. Automatically detachable gyro composite top. Where a composite gyro-composite gyro (1, 2) is connected at least two vertically. Each of them are all flexible ends (11, 21), with gyro (1,2) integrated. Each one consists of a fuselage (12, 22) and a gyro ring (13, 23) encased on the fuselage (12,22). The ends that connect to the lower end of the torso (12, 22) that are interconnected and include springs (14, 24) in the inner cavity of each distal torso. And the elastic tip spring (11) on the upper gyro (1) is in a compressed state when the upper gyro is inserted into the torso axis (22) of the lower gyro (2) to This causes the connection of the upper and lower gyro (1, 2) through the upper gyro (1) in the composite gyro (1, 2) disconnecting the lower gyro. (2) by composing the dimension in the composite gyro (1, 2) When being impacted or rotated, the object is interrupted during rotation. And the upper gyro was ejected from the lower gyro following the action of spring (14) of the elastic tip (11) in the upper gyro (1) to produce the upper gyro (1) at Rotate separately with lower gyro rotation (2) 2. Detachable gyro assembly type with non-dimensional compression according to claim 1, with gyro (1,2) structured. same 3. A modular gyro detachable type as per claim 1. Where the upper and lower gyro distal torso (1,2), upper and lower are arranged with spring soles in the inner cavity of them, and springs (14, 24) are placed on the inner spring sockets. The inner cavity of the distal body, where the upper end of the spring (14, 24) is pressed against the torso axis (12, 22), and when the upper gyro (1) is attached to the lower gyro (2). ) The spring (14) of the elastic tip (11) is compressed and retracted into the torso axis. (12) with the upper body part 4. A modular gyro detachable type as per claim 1. Where, when connected together, the upper gyro (1) and the lower gyro (2) are joined together as one piece in such a way that they can be rotated, upper and part gyro separated. The lower (1, 2) are joined together by a rotatable clamping structure positioned on two gyro rings (13, 23) or the upper and lower gyro (1, 2) are welded. Connected together by clamping two torso axes (12, 22), rotatable 5. gyro detachable assembly type gyro press as per claim 1 Where at the top end of the torso axis (12, 22) of each gyro (1, 2) is provided with 4-side detachable 2-face covers (10, 20), each cover. (10, 20) was provided with a structure for installing the ejector, including the spring. And each gyro (1,2) may be ejected for playing with the ejector by the interaction of the coupling structure and the lower gyro (2) is connected to the upper gyro. (1) After removing the cover (20) of the stand Where the cover mounting position positioned on the quad axis (22) of the lower gyro (2) is provided with a recessed cavity for the upper gyro tip (1) for installation 6. .Automatically detachable composite gyro top according to claim 4. The gyro rings (13, 23) are provided with a locking structure that is arranged for mounting the outer wall of the cabling (12, 22). Autonomous resolution according to the claim that 6 where the locking structure is generally protrusions (15, 25) arranged on the inner wall of the gyro ring (13, 23), the splitter axes (12,22) are assembled with the axle collar (121 , 221) and a clamping ring (122, 222) arranged on a rotatable spindle collar (121, 221), and a clamping ring (122, 222) is arranged with a pin (123, 223) that extends outward. Core sleeve (121, 221), outer wall of core sleeve (121,221) is provided with a corresponding pilot socket (124, 224) that can be penetrated by the latch (123, 223) for horizontal rotation. And barrier structures (125, 225) for protrusions (15, 25) of the gyro ring to slide inward and provide reliable connection of the gyro rings (13, 23) and axial casing (121,221) by means of Press the latch (123, 223), the flexible end (11,21) is attached to the lower part of the spindle casing (121, 221) in such a way that it can slide vertically. When the protrusions (15, 25) on the gyro ring (13, 23) slide into the barrier structure (125, 225), the clamping ring (122, 222) may be rotated with the pin (123, 223) rotated on the side. Above or below the overhang (15, 25), then the overhang (15, 25) is reliably locked between the pin (123, 223) and the tip edge of the barrier (125, 225). This enables the reliable connection of the gyro ring (13, 23) and the torso (12, 22). 8. Automatically detachable gyro-type composite gyro gyroscope, according to claim 7. Where the core sleeve (121,221) is assembled with the upper and lower axle sleeves installed together. Where the upper part of the lower axial casing is drawn in the upper axial casing, the clamping ring (122, 222) is positioned between the upper and lower axial casing, the upper portion of the lower axial casing may be fitted with the cap. The crown is located at the top end of the segment or the lower part of the flexible end of another gyro. And the lower edge, the cover of the cover, or the two sides of the flexible tip, have been placed on the lower axial sheath. 9. Where the upper and lower limiting lines are placed on the inner wall of the lower axial casing and the front 3 of the 4 front axes, the ends may be reliably attached to the lower axial casing in a sliding manner. Vertically by means of hooks (16, 26) placed on such sections And the lower limit of the lower axial casing And the top end of the spring (14, 24), which is located in the body, the end is placed on the upper limit. When two (1,2) gyro are connected vertically Lower part of the tip The elastic (11) of the upper gyro (1) is applied to the upper part of the lower gyro sheath (2), and the force is applied at the top of the lower gyro sheath to compress the pattern tip. Flexible top (11) 1 0. Autonomous gyro detachment type according to claim 9 Where the wall of the upper cavity of the lower axial casing is provided with a rotatable clamping structure where Install the protrusions positioned on the side wall below the cover. And the rotating clamping structure was formed by a flange placed on the wall of the cavity above the lower axial casing. 1 1. Automatically detached gyro gyros, according to the claim that 7 where the gyro ring (13, 23) is composed of a spherical attack ring. (131,231), which has a through hole at the center and a screw ring (132, 232) and a clamping ring (133, 233), which are arranged to install the attack ring (131, 231), the locking structure is positioned. On the screw ring (132, 232), the rotating clamping structure forms the upper and lower edges (134, 234), respectively, which are placed on the facing surfaces of the clamping ring (133, 233) of the upper gyro. And the lower part The upper clamp ring (133) is overlaid on the lower clamp ring. (233) and turning the top edge (134) towards the lower edge of the lower edge. (234) to give the bottom edge (234) overlaps the top edge (134) resulting in a single joint of the upper gyro (1) and the lower gyro (2) in a rotatable detachable manner 1 2. A composite gyro. Each type can be automatically released according to claim 11. By which the screw ring (132,232) consists of a top cover and a bottom ring, which are positioned to fit through the through hole of the attack ring. (131,231), overhang (15,25) in the locking structure is formed by the overlap of the upper and lower flanges, which are arranged accordingly on the Inner wall of the top and bottom cover washers When the body axis of the gyro (12, 22) is encased in the ring hole of the top and bottom cover ring. The top and bottom flanges of the upper and lower cover rings are fitted to the top and bottom ends of the gyro-axial obstruction (12, 22), creating a connection to the body axis. (12, 22) Reliable gyro 1 3. Automatically detached gyro-type composite gyro according to claim 12, with the edges arranged unitary on the inner wall. Of the through holes of the attack ring (131,231), the notches are aligned evenly on the top and bottom cover rings, in the position where the 4 pages of the number 4 align with the edges. The top and bottom cover rings are reliably positioned on the attack ring (131, 231) by creating a notch and edge. 1 4. Automatically detached gyro-type gyro top. Claim 1, 11, 12 or 13, where the direction of the gyro ring is left. (13,23) mounted on the fuselage axis (12,22) may be Vertically inverted ------------ Correction 16/12/58 1. Automatic detachable gyro type integrated gyro. Where the gyro was It is created by connecting at least two (1, 2) gyro vertically and all gyro ends (1, 2) as flexible ends (11, 12) to make the upper gyro ( 1) In the gyro (1, 2), it automatically disconnects the lower gyro (2) when it is knocked out or rotated, it is interrupted in the During rotation And the upper gyro was ejected according to the action of the flexible tip (11) to produce two separate gyros with the lower gyro (2). The gyro (1, 2) has the same structure. 3. The gyro assembled automatically detachable type according to claim 1, where the gyro Each rotor (1, 2) consists of a fuselage (12, 22) and a gyro ring (13, 23) encased on the fuselage (12, 22), a flexible tip (11, 21). It is connected under the torso axis (12, 22) and the flexible end (11) on the upper gyro (1) in a compressed state when it is inserted into the torso (22) of the gyro. Lower (2) to make the interlock of upper and lower gyro (1, 2) 4. Automatic detachable gyro type assembly gyro according to claim 3, where The elastic (11, 21) is formed by the distal torso that is attached to the lower end of the torso axis (12, 22) and provides a spring seat in the inner cavity of the section and a spring (14). , 24) that is placed on the shoulder blades in the inner cavity of the body. A Where the upper end of the spring (14, 24) is pressed against the body axis (12, 22) and when the upper gyro (1) is attached to the lower gyro (2) the spring (14) of the tip. The flexible gyro (11) is pressed and retracted into the torso (12) with the upper end of the body. 5. That, when connected together, the upper gyro (1) and the lower gyro (2) must be joined together as one piece. In such a way that the gyros can be separated, the upper and lower gyro (1, 2) are connected in Together, using a rotating clamp structure, which is placed on two gyro rings (13, 23) or the upper and lower gyro (1, 2) are connected by clamping the body axis. Two (12, 22) rotatable 6. Automatically detached gyro-type composite gyro according to claim 3, with the upper end of the torso axis (12, 22) of each gyro. (1, 2) are provided with detachable covers (10, 20), each cover (10, 20) is provided with a connector structure to install each ejector and gyro (1 , 2) may be ejected for play with the eject By working together the structure The upper gyro (10, 20) and lower gyro ejector (2) are connected to the upper gyro (1) after the cover (20) of that section is removed. Where the cover mounting position positioned on the body axis (22) of the lower gyro (2) was provided with a recessed cavity for the upper gyro tip (1) for installation. The self-detachable gyro gyro is fully assembled according to claim 5, where the gyro ring (13, 23) is provided with an organized locking structure to mount the outer wall of the shaft. Body (12, 22) 8. The gyro assembly, self-detaching type, according to claim 7, where the typical locking structure is a protrusion (15, 25), which is placed on the inner wall. The gyro ring (13, 23), the body axle (12, 22) is composed of a core sleeve (121, 221) and a clamping ring (122, 222), which are placed on the axle collar (121, 221). Swivel and clamping rings (122, 222) are provided with bolts (123, 223) extending outside the spindle casing (121, 221), the outer wall of the spindle casing (121, 221) is provided with a slot. Navigate (124, 224) by corresponding that can be penetrated by the bolt (123, 223) for horizontal rotation. And barrier structure (125, 225) for the protrusions (15, 25) of the gyro ring to slide inward and provide reliable connection of the gyro ring (13, 23) and the axis casing (121, 221). ) By pressing the latch (123, 223), the flexible end (11, 21) is attached to the The lower part of the spindle casing (121, 221) in such a way that it can slide vertically. When the protrusion (15, 25) on the gyro ring (13, 23) slides into the barrier structure (125, 225), the clamping ring (122, 222) may be rotated, provided that the pin (123, 223) is rotated at Above or below the overhang (15, 25), so the overhang (15, 25) is reliably locked between the latch (123, 223) and one end edge of the barrier (125, 225), resulting in Reliable connection of the gyro ring (13, 23) and the fuselage (12, 22) 9. The gyro assembly type is automatically released according to claim 8, where the axle collar (121 , 221), assembled with the upper and lower core sleeves that are installed together. Where the upper portion of the lower axial sleeve is encased in the upper axial casing, the clamping ring (122, 222) is positioned between the upper and lower axial casing, the upper portion of the lower axial sleeve may be fitted with the cap. A cap, which is placed at the top end of that section or the lower part of another gyro flexible end, and the lower edge of the cover, or both sides of the flexible tip, have been placed. The gyro top and bottom are placed on the inner wall of the lower axle casing. And the end body may be reliably attached to the lower axial casing in a vertically sliding manner by Relying on the harvest (16, 26) placed on the part And the lower limit of the lower axis sleeve and the upper end of the spring (14, 24), which are located in the end body, are placed on the upper limit when two gyro (1, 2) are Connect them together vertically. The lower part of the elastic tip (11) of the upper gyro (1) is applied to the upper part of the lower gyro sheath (2) and the force is applied at the top of the lower gyro sheath (2). (11) 1 1. Automatically detachable gyro-coupled gyro according to claim 10, where the wall of the upper cavity of the lower core sheath may be aligned. To have a rotating clamp structure that Install the protrusions positioned on the side wall below the cover. And a rotary clamping structure has been created. It is raised by a flange placed on the wall of the cavity above the lower axle casing 1 2. The gyro assembly type is automatically released according to claim 8, where the gyro ring (13, 23 ) Consists of a spherical assault ring (131, 231) with a through hole at the midpoint and a screw ring (132, 232) and a retaining ring (133, 233) arranged to install the attack ring (131, 233). ), The locking structure is arranged on the screw ring (132, 232), the rotary clamping structure It is the upper and lower edges (134, 234), respectively, placed on the face-to-face surfaces of the clamping rings (133, 233) of the upper and lower gyro. The upper clamping ring (133) is overlayed over the lower clamp ring (233) and the upper edge (134) is rotated towards the lower edge (234) so that the lower edge (234) overlaps the top edge. (134) resulting in a single junction of the upper gyro (1) and the lower gyro (2) in a rotatable detachable manner 1 3. A composite gyro It can be automatically released according to claim 12, where the screw ring (132, 232) consists of the top cover ring and the bottom cover ring. Placed to fit into the through hole of the attack ring (131, 231), overhang (15, 25) in the lock structure. Is created by overlapping flanges of the top and bottom, which are aligned consistently on Inner wall of the top and bottom cover washers When the body axis of the gyro (12, 22) is encased in the hole. Ring of top and bottom cover washers Top and bottom flange of the top cover ring And the bottom is attached to the upper and lower ends of the gyro-axis obstruction (12, 22), resulting in a reliable connection to the gyro axis (12, 22). 4.Automatic detachment type gyro gyro gyro according to claim 13, where the edges are aligned together on the inner wall of the through hole of the attack ring (131, 231), notch. Position them evenly on the top and bottom cover rings in a Consistent with the edges And the top and bottom cover rings are reliably positioned on the attack ring (131, 231) by creating a notch and edge. 1. 5. At 3, 12, 13 or 14 where the direction in which the gyro ring (13, 23) is mounted on the body axis (12, 22) may be reversed vertically. -------------------------------------------------- ----------- 1. Automatic detachable gyro type integrated gyro. Where the gyro was It is created by connecting at least two (1, 2) gyro vertically and all gyro ends (1, 2) as flexible ends (11, 12) to make the upper gyro ( 1) In the gyro (1, 2), it automatically disconnects the lower gyro (2) when holding a bump or turning it is interrupted in the During rotation And the upper gyro was ejected following the action of the flexible tip (11) to produce two separated gyro along with the lower gyro (2). Assembled automatically detachable type according to claim 1, where the gyro (1, 2) have the same structure 3. The gyro assembled automatically detachment type according to claim 1, where Each gyro (1, 2) consists of a fuselage axis (12, 22) and a gyro ring (13, 23) encased on the fuselage (12, 22), a flexible tip (11, 21). ) Is connected under the torso axis (12, 22) and the flexible end (11) on the upper gyro (1) in a compressed state when it is inserted into the torso axis (22) of the gyro. Lower (2) to make the upper and lower gyro interconnection (1, 2) 4. Automatic detachable gyro-type assembly gyro according to claim 3, where the tip The pliable type (11, 21) is formed by the distal torso that is attached to the lower end of the fuselage (12,22) and provides a spring seat in the inner cavity of the section and the spring ( 14, 24) placed on the spring-loaded shoulders in the inner cavity of the upper body. striped Where the upper end of the spring (14, 24) is pressed against the body axis (12, 22) and when the upper gyro (1) is attached to the lower gyro (2) the spring (14) of the tip. The flexible gyro (11) is pressed and retracted into the torso (12) with the upper end of the body. 5. That when connected together, the upper gyro (1) and the lower gyro (2) are joined together as one piece. In such a way that the gyros can be separated, the upper and lower gyro (1, 2) are connected in Together, using a rotating clamp structure, which is placed on two gyro rings (13, 23) or the upper and lower gyro (1, 2) are connected by clamping the body axis. Two (12, 22) rotatable 6. Automatically detached gyro-type composite gyro according to claim 3, with the upper end of the torso axis (12, 22) of each gyro. (1, 2) are provided with detachable covers (10, 20), each cover (10, 20) is provided with a connector structure to install each ejector and gyro (1 , 2) may be ejected to perform the ejection play by the interaction of the structure. The upper gyro (10, 20) and lower gyro ejector (2) are connected to the upper gyro (1) after the cover (20) of that section is removed. Where the cover mounting position positioned on the body axis (22) of the lower gyro (2) was provided with a recessed cavity for the upper gyro tip (1) for installation. The self-detachable gyro gyro is fully assembled according to claim 5, where the gyro ring (13, 23) is provided with an organized locking structure to mount the outer wall of the shaft. Body (12, 22) 8. The gyro assembly, self-detaching type, according to claim 7, where the typical locking structure is a protrusion (15, 25), which is placed on the inner wall. The gyro ring (13, 23), the body axle (12, 22) is composed of a core sleeve (121, 221) and a clamping ring (122, 222), which are placed on the axle collar (121, 221). Swivel and clamping rings (122, 222) are provided with bolts (123, 223) extending outside the spindle casing (121, 221), the outer wall of the spindle casing (121, 221) is provided with a slot. Navigate (124, 224) by corresponding that can be penetrated by the bolt (123, 223) for horizontal rotation. And barrier structure (125, 225) for the protrusions (15, 25) of the gyro ring to slide inward and provide reliable connection of the gyro ring (13, 23) and the axis casing (121, 221). ) By pressing the latch (123, 223), the flexible end (11, 21) is attached to the The lower part of the spindle casing (121, 221) in such a way that it can slide vertically. When another part (15, 25) on the gyro ring (13, 23) slides into the barrier structure (125, 225), the clamping ring (122, 222) may be rotated, provided that the pin (123, 223) is rotated at Above or below the overhang (15, 25), so the overhang (15, 25) is reliably locked between the latch (123, 223) and one end edge of the barrier (125, 225), resulting in Reliable connection of the gyro ring (13, 23) and the fuselage (12, 22) 9. The gyro assembly type is automatically released according to claim 8, where the axle collar (121 , 221), assembled with the upper and lower core sleeves that are installed together. Where the upper portion of the lower axial sleeve is encased in the upper axial casing, the clamping ring (122, 222) is positioned between the upper and lower axial casing, the upper portion of the lower axial sleeve may be fitted with the cap. A cap, which is placed at the top end of that section or the lower part of another gyro flexible end, and the lower edge of the cover, or both sides of the flexible tip, have been placed. The gyro top and bottom are placed on the inner wall of the lower axle casing. And the end body may be reliably attached to the lower axial casing in a vertically sliding manner by It relies on the hooks (16, 26) placed on that section. And the lower limit of the lower axis sleeve and the upper end of the spring (14, 24), which are located in the end body, are placed on the upper limit when two gyro (1, 2) are Connect them together vertically. The lower part of the elastic tip (11) of the upper gyro (1) is applied to the upper part of the lower gyro sheath (2) and the force is applied at the top of the lower gyro sheath (2). To compress the elastic tip above (11) 1 1. Automatic detachment type gyro gyro in accordance with claim 10, whereby the wall of the upper cavity of the lower axial casing may be provided with a rotating clamping structure at Install the protrusions positioned on the side wall below the cover. And a rotary clamping structure has been created. Raised by flanges arranged on the wall of the upper cavity of the lower axial casing 1 2. The gyro detachment type is automatically detached according to claim 8, where the gyro ring (13, 23) is composed of a spherical attack ring (131, 231), through which the tee hole passes at its center. And the scoot ring (132, 232) and the clamp ring (133, 233), which were arranged to install the assault ring (131, 231), the locking structure was placed on the screw ring (132, 232). Rotary clamping structure It is the upper and lower edges (134, 234), respectively, placed on the face-to-face surfaces of the clamping rings (133, 233) of the upper and lower gyro. The upper clamping ring (133) is overlayed over the lower clamp ring (233) and the upper edge (134) is rotated towards the lower edge (234) so that the lower edge (234) overlaps the top edge. (134) resulting in a single joint of the upper gyro (1) and the lower gyro (2) in a rotatable 1 3. The gyro coupling is automatically disengaged according to claim 12, where the screw ring (132, 232) is composed of a top cover ring and a bottom cover ring arranged. Placed to fit into the through hole of the attack ring (131, 231), the overhang (15, 25) in the lock structure was Created by overlap of the top and bottom flanges, which are arranged consistently on Inner wall of the top and bottom cover washers When the body axis of the gyro (12, 22) is encased in the hole. Ring of top and bottom cover washer, Top flange and bottom flange And the bottom is attached to the upper and lower ends of the gyro-axis obstruction (12, 22), resulting in a reliable connection to the gyro axis (12, 22). 4.Automatic detachment type gyro gyro gyro according to claim 13, where the edges are aligned together on the inner wall of the through hole of the attack ring (131, 231), notch. Position them evenly on the top and bottom cover rings in a Consistent with the edges And the top and bottom cover rings are reliably positioned on the attack ring (131, 231) by creating a notch and edge 1. 5. Automatic detachment type gyro coupler according to claim 3, 12, 13 or 14, where the direction in which the gyro ring (13, 23) is located on the torso axis (12 , 22) may be reversed vertically.