CN204699301U - Power-assisted horizontal bar & parallel bars training airplane - Google Patents
Power-assisted horizontal bar & parallel bars training airplane Download PDFInfo
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- CN204699301U CN204699301U CN201520377236.7U CN201520377236U CN204699301U CN 204699301 U CN204699301 U CN 204699301U CN 201520377236 U CN201520377236 U CN 201520377236U CN 204699301 U CN204699301 U CN 204699301U
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Abstract
A kind of power-assisted horizontal bar & parallel bars training airplane, comprises main body rack and power-assisted unit; Described main body rack is " door " font; The side of " door " font support is provided with holding rod, and described power-assisted unit is at the opposite side of " door " font support; Described power-assisted unit comprises balancing weight unit, leverage and transmission mechanism; Balancing weight unit comprises balancing weight, framework and lifting arm; Balancing weight has multiple, and they slide up and down in the space that framework surrounds, and each balancing weight and lifting arm removably connect; The fulcrum of leverage is connected with frame member; The resistance arm of leverage connects described lifting arm by transmission mechanism; The holding rod side of power arm reaches " door " font support, and the end of power arm is provided with and scrunches bar; Scrunch bar identical with the distance of two columns of " door " font support; Described transmission mechanism comprises pulley and connecting band; The two ends of connecting band connect resistance arm and lifting arm respectively, and pulley has multiple, and pulley is located on framework, and connecting band is around on pulley.
Description
Technical field
The utility model relates to a kind of health and fitness facilities, specifically a kind of power-assisted horizontal bar & parallel bars training airplane.
Background technology
The training of the bicipital muscle of arm, the triceps muscle of arm, rhomboideus, latissimus dorsi and cucullaris, generally can adopt horizontal bar & parallel bars to train.In use find, for the user of different phase, its strength is different, and the pure effective exercise relying on the strength of self may not necessarily complete above-mentioned muscle, even can muscle injury.
Summary of the invention
In order to solve the above-mentioned problems in the prior art, the utility model proposes a kind of power-assisted horizontal bar & parallel bars training airplane, comprising main body rack and power-assisted unit;
Described main body rack is " door " font; The side of " door " font support is provided with holding rod, and described power-assisted unit is at the opposite side of " door " font support;
Described power-assisted unit comprises balancing weight unit, leverage and transmission mechanism;
Balancing weight unit comprises balancing weight, framework and lifting arm; Balancing weight has multiple, and they slide up and down in the space that framework surrounds, and each balancing weight and lifting arm removably connect;
The fulcrum of leverage is connected with frame member; The resistance arm of leverage connects described lifting arm by transmission mechanism; The holding rod side of power arm reaches " door " font support, and the end of power arm is provided with and scrunches bar; The distance scrunched between bar and two columns of " door " font support is identical;
Described transmission mechanism comprises pulley and connecting band; The two ends of connecting band connect resistance arm and lifting arm respectively, and pulley has multiple, and pulley is located on framework, and connecting band, around on pulley, under scrunching bar pressed status, lifting arm is carried.Trainer stands in and scrunches bar, by holding holding rod to draw, supportting self.
Described holding rod is symmetrically located on two columns of " door " font support; Two columns of " door " font support are also fixed with pedal.
Two column place planes of described framework are set to face a, and two column place planes of " door " font support are set to face b, and face a is mutually vertical with face b;
The fulcrum of described leverage is connected on a column of framework, and this column is away from " door " font support.
Middle part and the bottom of described " door " font support are connected to cross bar, and the top of described framework is fixedly connected with two cross bars respectively with bottom.
The framework of described " door " font support, balancing weight unit, and the cross bar between the framework of balancing weight unit and main body rack, the shape of their radial section is all the shape that two evagination circular arcs and two parallel lines surround.
Described balancing weight is built from bottom to top in the space that framework surrounds; Described lifting arm has the pin-and-hole corresponding with each balancing weight, and each balancing weight is removably connected by latch and lifting arm.
Described balancing weight unit also comprises transparent PVC case, and this case covers on outside space, balancing weight place, and case cover has the space corresponding with described latch (can accomplish good security protection, and easy to use).
The base of frame of described balancing weight unit is provided with cushion pad (can absorbing vibration).
Anti-slip veins is carved with on the described bar surface that scrunches.
Compared with prior art, the security of this training airplane is higher, easy to use, and the specific aim being suitable for the bicipital muscle of arm of different phase user, the triceps muscle of arm, rhomboideus, latissimus dorsi and cucullaris is taken exercise, and avoids the strain of other muscle group.
Accompanying drawing explanation
Fig. 1 is structural principle schematic diagram of the present utility model;
Fig. 2 is appearance schematic diagram of the present utility model (PVC-free cover);
In figure: fulcrum and the frame member tie point 7 of " door " font support 1, power-assisted unit 2, holding rod 3, leverage 4, framework 5, balancing weight 6, leverage, scrunch bar 8, connecting band 9, pedal 10, cross bar 11, latch 12, cushion pad 13.
Detailed description of the invention
The technical program is further illustrated as follows below in conjunction with accompanying drawing and detailed description of the invention:
As Fig. 1 and 2, a kind of power-assisted horizontal bar & parallel bars training airplane, comprises main body rack and power-assisted unit;
Described main body rack is " door " font; The side of " door " font support is provided with holding rod, and described power-assisted unit is at the opposite side of " door " font support;
Described power-assisted unit comprises balancing weight unit, leverage and transmission mechanism;
Balancing weight unit comprises balancing weight, framework and lifting arm; Balancing weight has multiple, and they slide up and down in the space that framework surrounds, and each balancing weight and lifting arm removably connect;
The fulcrum of leverage is connected with frame member; The resistance arm of leverage connects described lifting arm by transmission mechanism; The holding rod side of power arm reaches " door " font support, and the end of power arm is provided with and scrunches bar; The distance scrunched between bar and two columns of " door " font support is identical;
Described transmission mechanism comprises pulley and connecting band; The two ends of connecting band connect resistance arm and lifting arm respectively, and pulley has multiple, and pulley is located on framework, and connecting band, around on pulley, under scrunching bar pressed status, lifting arm is carried.
Described holding rod is symmetrically located on two columns of " door " font support; Two columns of " door " font support are also fixed with pedal.
Two column place planes of described framework are set to face a, and two column place planes of " door " font support are set to face b, and face a is mutually vertical with face b;
The fulcrum of described leverage is connected on a column of framework, and this column is away from " door " font support.
Middle part and the bottom of described " door " font support are connected to cross bar, and the top of described framework is fixedly connected with two cross bars respectively with bottom.
The framework of described " door " font support, balancing weight unit, and the cross bar between the framework of balancing weight unit and main body rack, the shape of their radial section is all the shape that two evagination circular arcs and two parallel lines surround.
Described balancing weight is built from bottom to top in the space that framework surrounds; Described lifting arm has the pin-and-hole corresponding with each balancing weight, and each balancing weight is removably connected by latch and lifting arm.
Described balancing weight unit also comprises transparent PVC case, and this case covers on outside space, balancing weight place, and case cover has the space corresponding with described latch.
The base of frame of described balancing weight unit is provided with cushion pad.
Anti-slip veins is carved with on the described bar surface that scrunches.
Claims (9)
1. a power-assisted horizontal bar & parallel bars training airplane, is characterized in that comprising main body rack and power-assisted unit;
Described main body rack is " door " font; The side of " door " font support is provided with holding rod, and described power-assisted unit is at the opposite side of " door " font support;
Described power-assisted unit comprises balancing weight unit, leverage and transmission mechanism;
Balancing weight unit comprises balancing weight, framework and lifting arm; Balancing weight has multiple, and they slide up and down in the space that framework surrounds, and each balancing weight and lifting arm removably connect;
The fulcrum of leverage is connected with frame member; The resistance arm of leverage connects described lifting arm by transmission mechanism; The holding rod side of power arm reaches " door " font support, and the end of power arm is provided with and scrunches bar; Scrunch bar identical with the distance of two columns of " door " font support;
Described transmission mechanism comprises pulley and connecting band; The two ends of connecting band connect resistance arm and lifting arm respectively, and pulley has multiple, and pulley is located on framework, and connecting band, around on pulley, under scrunching bar pressed status, lifting arm is carried.
2. power-assisted horizontal bar & parallel bars training airplane according to claim 1, is characterized in that described holding rod is symmetrically located on two columns of " door " font support; Two columns of " door " font support are also fixed with pedal.
3. power-assisted horizontal bar & parallel bars training airplane according to claim 1, it is characterized in that two column place planes of described framework are set to face a, two column place planes of " door " font support are set to face b, and face a is mutually vertical with face b;
The fulcrum of described leverage is connected on a column of framework, and this column is away from " door " font support.
4. power-assisted horizontal bar & parallel bars training airplane according to claim 1, it is characterized in that the middle part of described " door " font support and bottom are connected to cross bar, the top of described framework is fixedly connected with two cross bars respectively with bottom.
5. power-assisted horizontal bar & parallel bars training airplane according to claim 4, it is characterized in that the framework of described " door " font support, balancing weight unit, and the cross bar between the framework of balancing weight unit and main body rack, the shape of their radial section is all the shape that two evagination circular arcs and two parallel lines surround.
6. power-assisted horizontal bar & parallel bars training airplane according to claim 1, is characterized in that described balancing weight is built from bottom to top in the space that framework surrounds; Described lifting arm has the pin-and-hole corresponding with each balancing weight, and each balancing weight is removably connected by latch and lifting arm.
7. power-assisted horizontal bar & parallel bars training airplane according to claim 6, it is characterized in that described balancing weight unit also comprises transparent PVC case, this case covers on outside space, balancing weight place, and case cover has the space corresponding with described latch.
8. power-assisted horizontal bar & parallel bars training airplane according to claim 1, is characterized in that the base of frame of described balancing weight unit is provided with cushion pad.
9. power-assisted horizontal bar & parallel bars training airplane according to claim 1, scrunches bar surface and is carved with anti-slip veins described in it is characterized in that.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520377236.7U CN204699301U (en) | 2015-06-03 | 2015-06-03 | Power-assisted horizontal bar & parallel bars training airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520377236.7U CN204699301U (en) | 2015-06-03 | 2015-06-03 | Power-assisted horizontal bar & parallel bars training airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204699301U true CN204699301U (en) | 2015-10-14 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520377236.7U Expired - Fee Related CN204699301U (en) | 2015-06-03 | 2015-06-03 | Power-assisted horizontal bar & parallel bars training airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204699301U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108348801A (en) * | 2015-10-28 | 2018-07-31 | 卡洛斯·阿图罗·埃斯特拉达·埃斯特拉达 | Modular construction for physical exercise |
| CN109173176A (en) * | 2018-11-12 | 2019-01-11 | 陈都 | A kind of energy saving chin-up training device with assist function |
-
2015
- 2015-06-03 CN CN201520377236.7U patent/CN204699301U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108348801A (en) * | 2015-10-28 | 2018-07-31 | 卡洛斯·阿图罗·埃斯特拉达·埃斯特拉达 | Modular construction for physical exercise |
| CN109173176A (en) * | 2018-11-12 | 2019-01-11 | 陈都 | A kind of energy saving chin-up training device with assist function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151014 Termination date: 20180603 |