CN205569615U - Ware of kicking one's legs - Google Patents
Ware of kicking one's legs Download PDFInfo
- Publication number
- CN205569615U CN205569615U CN201620329231.1U CN201620329231U CN205569615U CN 205569615 U CN205569615 U CN 205569615U CN 201620329231 U CN201620329231 U CN 201620329231U CN 205569615 U CN205569615 U CN 205569615U
- Authority
- CN
- China
- Prior art keywords
- sleeve pipe
- main body
- fuselage main
- tread plate
- plate seat
- 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.)
- Expired - Fee Related
Links
Landscapes
- Rehabilitation Tools (AREA)
Abstract
The utility model discloses a ware of kicking one's legs, it includes fuselage main part, bearing diagonal pole, horizontal pole, left sleeve pipe, right casing pipe, left telescopic link, right telescopic rod, left pedal seat, right pedal seat, left foot footboard, right crus of diaphragm footboard, haulage rope, traction wheel, fuselage main part foot pipe and bearing diagonal pole foot pipe, calorimeter scale. When time spent not, through swing bearing diagonal pole, can be close to the fuselage main part earlier with left foot footboard and the upswing respectively of right crus of diaphragm footboard, take and fold the bolt of horizontal pole out horizontal pole again, the fuselage main part is laminated with the support frame for the machine is folding to be packed up, and area is little, convenient to use.
Description
Technical field
This utility model relates to a kind of health and fitness facilities, particularly relates to one and kicks one's legs device.
Background technology
Current device of kicking one's legs mostly is sitting posture and kicks one's legs device, and what it was mainly trained is leg muscle, and the upper limb almost place when training
In without kinestate, in order to take into account the exercise of upper limb while meeting effective leg exercising muscle, this utility model provides
A kind of novel device of kicking one's legs..
Utility model content
The purpose of this utility model is to provide a kind of function more complete, especially to machine construction safety, the life-span be greatly improved with
The device of kicking one's legs improved
For achieving the above object, technical solution of the present utility model is:
The utility model discloses one to kick one's legs device, it include fuselage main body, inclined support bar, cross bar, left sleeve pipe, right sleeve pipe,
Left expansion link, right expansion link, left-hand tread plate seat, right-hand tread plate seat, Vehicular left pedal, right steps, pull rope, traction wheel, fuselage
Main body foot tube and inclined support bar foot tube, calorie gauge table,
Described left sleeve pipe and right sleeve pipe are slipped in fuselage main body by left-hand tread plate seat and right steps respectively, and can be along fuselage master
The both sides of body move up and down；Described left expansion link and one end of right expansion link are nested with respectively in left sleeve pipe and right sleeve pipe, and it is another
One end is stretched out outside left conduit and right conduit, is vertically provided with handle on its external part；Install on the top of fuselage main body
Pulley, is provided with bearing in pulley, the middle part of described pulling rope is articulated in pulley chute, and the two ends of pulling rope are respectively and fixedly connected with
On left-hand tread plate seat and right-hand tread plate seat so that left-hand tread plate seat and right-hand tread plate seat together with affixed left sleeve pipe thereon and right sleeve pipe along fuselage
The both sides of main body form upper and lower adverse movement；Described left expansion link has adjustable spring hoodle with the bottom of right expansion link,
Offering hole, multiple location on the tube wall of left sleeve pipe and right sleeve pipe, left expansion link and right expansion link are packing into left sleeve pipe and right set respectively
It is stuck in the adjustment hole of sleeve pipe by the spring hoodle in expansion link in pipe, makes user can find comfortable use highly.
Preferably, described left and right pedal is respectively mounted on left-hand tread plate seat and right-hand tread plate seat；The upper end of described inclined support bar
Being hinged on the upper end of fuselage main body, one end of cross bar is hinged on the lower end of fuselage main body, and the other end of cross bar is hinged on inclined support bar
Lower end, fuselage main body foot tube and inclined support bar foot tube are respectively and fixedly connected to the bottom of fuselage main body and inclined support bar；
Preferably, described cross bar is made up of square tube and channel bar, and described channel bar is offered multiple tune for regulating cross bar length
Knothole, one end of square tube is hinged on the lower end of fuselage main body, and first hole of the other end of square tube is hinged on the length of one end of channel bar
In circular hole, second hole of the other end of square tube is connected with the adjustment hole of channel bar by latch, and the other end of channel bar is connected to tiltedly prop up
The lower end of strut.Described fuselage main body, inclined support bar, cross bar constitute a stable triangle.
Preferably, with inclined support bar by latch fixed fold shape after described cross bar having individual stator to fold for machine storage
State.
Preferably, described left-hand tread plate seat and right-hand tread plate seat are along fuselage bulk motion, fuselage main body lower end limited location shock-damping structure.
Preferably, described fuselage main body upper end constitutes left sleeve pipe and the track of right sleeve pipe up and down motion equipped with three pulleys.
Preferably, being mounted on three pulleys in described left-hand tread plate seat and left-hand tread plate seat, composition is stepped on seat and is transported up and down along fuselage main body
Dynamic track.
Preferably, described calorie quantifier is arranged on the face shield of fuselage main body, at the back side of face shield equipped with sensor,
The correspondence position of left and right sleeve pipe is equipped with Magnet, and Magnet following left sleeve pipe moves up and down can be through sensor, and calorie quantifier is with regard to energy
The number of times that work recorder move up and down.
Preferably, described pedal is hinged on pedal base, pedal balance be provided with between pedal base plastic mattress play spacing with protect
Protect and do use.
Preferably, behind inclined support bar top with fuselage main body, it is provided with Set of bolt for restricting displacement.
Preferably, between inclined support bar top and fore-stock, spacing rubber blanket it is provided with.
Use after such scheme, this utility model main body main body, inclined support bar, left sleeve pipe, right sleeve pipe, left expansion link,
Right expansion link, left-hand tread plate seat, right-hand tread plate seat, pedal, traction wheel, calorie quantifier etc. form.When not, pass through
Swing inclined support bar, can first Vehicular left pedal and right steps be swung up respectively, near fuselage main body, then by the latch of cross bar
Extracting out and folding cross bar, fuselage main body is fitted with bracing frame so that machine foldable is packed up, and floor space is little, easy to use.
Accompanying drawing explanation
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is that this utility model is kicked one's legs the axonometric drawing of device；
Fig. 2 is Fig. 1 partial enlarged drawing at A；Wherein (a) is the Matching Relation of inclined support bar and limited block 18, and (b) is A
Side view after place's partial enlargement；
Fig. 3 is the axonometric drawing after this utility model pedal folding；Wherein (a) is front view, and (b) is rear view；
Fig. 4 is the axonometric drawing that this utility model struts process；
Fig. 5 is the axonometric drawing after this utility model folds.
Detailed description of the invention
As it is shown in figure 1, of the present utility model kick one's legs device by fuselage main body 1, inclined support bar 2, cross bar 3, left sleeve pipe 4, right sleeve pipe 5,
Left expansion link 6, right expansion link 7, left-hand tread plate seat 8, right-hand tread plate seat 9, Vehicular left pedal 10, right steps 11, pull rope 12, lead
Running wheel 13, fuselage main body foot tube 14 and inclined support bar foot tube 15, calorie gauge table 16 form.
Described fuselage main body 1 is the rectangular elements with two longitudinal long tubes, and the upper end thereof of inclined support bar 2 is in fuselage main body 1
Upper end, between inclined support bar 2 top and fuselage main body 1, be provided with limited block 18,19 (as shown in Figure 2).Described horizontal stroke
Bar is made up of square tube 301 and channel bar 302, and described channel bar 302 is offered multiple adjustment hole for regulating cross bar length, square tube
One end is hinged on the lower end of fuselage main body 1, in the slotted hole of one end that first hole of the other end of square tube is hinged on channel bar, and side
Second hole of the other end of pipe is connected with the adjustment hole of channel bar by latch, and the other end of channel bar is connected to the lower end of inclined support bar.
Described fuselage main body, inclined support bar, cross bar constitute a stable triangle, and described cross bar 3 has individual stator for machine
Device storage passes through latch fixed fold state with inclined support bar after folding.
The top of fuselage main body 1 is the most outwards respectively symmetrically and is provided with handle 201,202.Described fuselage main body foot tube
14 and inclined support bar foot tube 15 be respectively and fixedly connected to fuselage main body 1 and the bottom of bearing diagonal frame 2, rise Stabilization,
Described left sleeve pipe 4 and right sleeve pipe 5 slip in fuselage main body 1 by left-hand tread plate seat 8 and right-hand tread plate seat 9 respectively, fuselage
Three pulleys of the upper end thereof of main body 1 constitute the tracks of left sleeve pipe 4 and right sleeve pipe 5, and left sleeve pipe 4 can be along fuselage master with right sleeve pipe 5
Two longitudinal long tubes of body 1 move up and down；Described left expansion link 6 and one end of right expansion link 7 are nested with respectively at left sleeve pipe 4
With in right sleeve pipe 5, the top of the left expansion link 6 being nested with in left sleeve pipe 4 and right sleeve pipe 5 and right loop bar 7 is provided with elasticity
Buckle, along longitudinally offering multiple positioning through hole on the tube wall of left sleeve pipe 4 and right sleeve pipe 5, Elastic buckle can be determined at this in holding
In the through hole of position, press this Elastic buckle that left expansion link 6 and right expansion link 7 just can be made to move in left sleeve pipe 4 and right sleeve pipe 5 by top
Dynamic, reach the purpose of collapsing length；The other end of left expansion link 6 and right expansion link 7 stretches out outside left sleeve pipe 4 and right sleeve pipe 5,
Handle 203,204 is vertically installed on its external part.
Install pulley 13 on fuselage main body 1 top, the middle part of described pulling rope 12 is articulated in pulley 13 chute, pulling rope 12
Two ends be respectively and fixedly connected on left-hand tread plate seat 8 and right-hand tread plate seat 9, the two ends of described pulling rope 12 are fixed in by bolt respectively
On left-hand tread plate seat 8 and right-hand tread plate seat 9.As it is shown on figure 3, described Vehicular left pedal 10, right steps 11 the inner are respectively hinged at
On left-hand tread plate seat 8 and right-hand tread plate seat 9, each hinged three pulleys in left-hand tread plate seat 8 and right-hand tread plate seat 9, three pulleys are constituted
The track moved up and down along fuselage main body, is provided with spacing block set 801, this spacing block set 801 on the swinging track of left-hand tread plate seat 8
Make Vehicular left pedal 8 swing horizontal level time, the most no longer swung downward, in order to practitioner scrunches.Right steps 9 and left foot
Pedal 8 structure is identical.
Described left-hand tread plate seat and right-hand tread plate seat are along fuselage bulk motion, fuselage main body lower end limited location shock-absorbing sleeve 101,102.
During as it is shown on figure 3, take exercise, foot steps on Vehicular left pedal 10 and right steps 11, drive left-hand tread plate seat 8 and right-hand tread plate seat 9 together with
Affixed left sleeve pipe 4 thereon and right sleeve pipe 5 form upper and lower adverse movement along two longitudinal long tubes of fuselage main body, i.e. left-hand tread plate
Seat 8 upwards, downwards, take exercises by right-hand tread plate seat 9.
The face shield of device of kicking one's legs is mounted with calorie quantifier 16, at the back side of face shield equipped with sensor, right at left and right sleeve pipe
Answering position equipped with Magnet, Magnet following left sleeve pipe moves up and down can be through sensor, and calorie quantifier just can work and logging machine
The number of times that device moves up and down.
Operation principle of the present utility model:
As shown in Figure 4, during use, inclined support bar 2 puts down, and is strutted by the cross bar of folding and plugs latch.
Shown in Fig. 5, the not used time, Vehicular left pedal 8 and right steps 9 are swung up respectively, near fuselage main body 1,
Again latch 17 extracted out and cross bar is folded up, making fuselage main body 1 fit with inclined support bar 2, after laminating, cross bar is solid
Bottom stator and brace, draw-in groove is fixed to receive by latch.
The above, only this utility model preferred embodiment, depending on the adjustment hole quantity on sleeve pipe can be according to needs,
Therefore can not limit, with this, the scope that this utility model is implemented, i.e. made according to this utility model claim and description
Equivalence change with modify, all should still belong in the range of this utility model patent contains.
Claims (10)
1. a device of kicking one's legs, it includes fuselage main body, inclined support bar, cross bar, left sleeve pipe, right sleeve pipe, left expansion link, right expansion link, left-hand tread plate seat, right-hand tread plate seat, Vehicular left pedal, right steps, pull rope, traction wheel, fuselage main body foot tube and inclined support bar foot tube, calorie gauge table
Described left sleeve pipe and right sleeve pipe are slipped in fuselage main body by left-hand tread plate seat and right steps respectively, and can move up and down along the both sides of fuselage main body；Described left expansion link and one end of right expansion link are nested with respectively in left sleeve pipe and right sleeve pipe, and its other end stretches out outside left conduit and right conduit, is vertically provided with handle on its external part；Pulley is installed on the top of fuselage main body, bearing is installed in pulley, the middle part of described pulling rope is articulated in pulley chute, the two ends of pulling rope are respectively and fixedly connected on left-hand tread plate seat and right-hand tread plate seat so that left-hand tread plate seat and right-hand tread plate seat form upper and lower adverse movement together with affixed left sleeve pipe thereon and right sleeve pipe along the both sides of fuselage main body；Described left expansion link has adjustable spring hoodle with the bottom of right expansion link, offering hole, multiple location on the tube wall of left sleeve pipe and right sleeve pipe, left expansion link and right expansion link are stuck in the adjustment hole of sleeve pipe by the spring hoodle in expansion link in left sleeve pipe and right sleeve pipe packing into respectively.
Device of kicking one's legs the most according to claim 1, it is characterised in that described left and right pedal is respectively mounted on left-hand tread plate seat and right-hand tread plate seat；The upper end thereof of described inclined support bar is in the upper end of fuselage main body, one end of cross bar is hinged on the lower end of fuselage main body, the other end of cross bar is hinged on the lower end of inclined support bar, and fuselage main body foot tube and inclined support bar foot tube are respectively and fixedly connected to the bottom of fuselage main body and inclined support bar.
Device of kicking one's legs the most according to claim 1, it is characterized in that described cross bar is made up of square tube and channel bar, multiple adjustment hole for regulating cross bar length is offered on described channel bar, one end of square tube is hinged on the lower end of fuselage main body, in the slotted hole of one end that first hole of the other end of square tube is hinged on channel bar, second hole of the other end of square tube is connected with the adjustment hole of channel bar by latch, the other end of channel bar is connected to the lower end of inclined support bar, and described fuselage main body, inclined support bar, cross bar constitute a stable triangle.
Device of kicking one's legs the most according to claim 1, it is characterised in that described cross bar is provided with after stator folds for machine storage and passes through latch fixed fold state with inclined support bar.
Device of kicking one's legs the most according to claim 1, it is characterised in that described left-hand tread plate seat and right-hand tread plate seat are along fuselage bulk motion, fuselage main body lower end limited location shock-damping structure.
Device of kicking one's legs the most according to claim 1, it is characterised in that described fuselage main body upper end constitutes left sleeve pipe and the track of right sleeve pipe up and down motion equipped with three pulleys.
Device of kicking one's legs the most according to claim 1, it is characterised in that be mounted on three pulleys in described left-hand tread plate seat and left-hand tread plate seat, constitutes and steps on the track that seat moves up and down along fuselage main body.
Device of kicking one's legs the most according to claim 1, it is characterized in that described calorie quantifier is arranged on the face shield of fuselage main body, at the back side of face shield equipped with sensor, at the correspondence position of left and right sleeve pipe equipped with Magnet, Magnet following left sleeve pipe moves up and down can be through sensor, the number of times that calorie quantifier just can work and recorder moves up and down.
Device of kicking one's legs the most according to claim 1, it is characterised in that described pedal is hinged on pedal base, pedal is balanced and is provided with plastic mattress between pedal base and plays and spacing do use with protection.
Device of kicking one's legs the most according to claim 1, it is characterised in that be provided with Set of bolt for restricting displacement behind inclined support bar top with fuselage main body, be provided with spacing rubber blanket between inclined support bar top and fore-stock.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620329231.1U CN205569615U (en) | 2016-04-18 | 2016-04-18 | Ware of kicking one's legs |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620329231.1U CN205569615U (en) | 2016-04-18 | 2016-04-18 | Ware of kicking one's legs |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205569615U true CN205569615U (en) | 2016-09-14 |
Family
ID=56863264
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620329231.1U Expired - Fee Related CN205569615U (en) | 2016-04-18 | 2016-04-18 | Ware of kicking one's legs |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205569615U (en) |
-
2016
- 2016-04-18 CN CN201620329231.1U patent/CN205569615U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205759430U (en) | A kind of multifunctional massage chair | |
| CN210355853U (en) | Ligament stretching device for track and field training | |
| CN206454173U (en) | A kind of foldable multifunctional combined trainer | |
| CN201052379Y (en) | Body-building equipment | |
| CN108579004A (en) | A kind of automatic training device of deep-knee-bend for wushu training | |
| CN205569615U (en) | Ware of kicking one's legs | |
| CN208511781U (en) | A kind of high machine drawing | |
| CN106730588A (en) | A kind of foldable multifunctional combined trainer | |
| CN207532702U (en) | A kind of multi-functional apparatus for developing muscle | |
| CN104147752B (en) | A kind of shank and back exercising apparatus | |
| CN206275976U (en) | A kind of track and field physical training device | |
| CN204260307U (en) | Body-building office chair | |
| CN203060707U (en) | Simulated rock climbing machine | |
| CN108888912A (en) | A kind of health and fitness facilities that sitting posture is kicked one's legs obliquely and its application method | |
| CN212282703U (en) | Waist and abdomen core training frame | |
| CN203724707U (en) | Roller coaster | |
| CN201394310Y (en) | Rock climbing analog machine | |
| CN211836077U (en) | Rowing machine convenient to adjust | |
| CN207445469U (en) | A kind of multi-functional barre | |
| CN203634723U (en) | Lower-limb strength training device with counter | |
| CN208356027U (en) | A kind of deep-knee-bend machine | |
| CN203342280U (en) | Foldable leg-beautifying machine capable of rotating at 360 degrees | |
| CN203370247U (en) | Multifunctional abdominal curl machine | |
| CN207085198U (en) | A kind of resistive drag force tuck hang combined trainer | |
| CN206518814U (en) | A kind of treadmill |
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: 20160914 Termination date: 20200418 |