CN107669387A - A kind of neck apparatus for correcting with controllability - Google Patents
A kind of neck apparatus for correcting with controllability Download PDFInfo
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- CN107669387A CN107669387A CN201711168804.2A CN201711168804A CN107669387A CN 107669387 A CN107669387 A CN 107669387A CN 201711168804 A CN201711168804 A CN 201711168804A CN 107669387 A CN107669387 A CN 107669387A
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- air force
- overload mechanism
- governor motion
- longitudinal screw
- air
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- 230000007246 mechanism Effects 0.000 claims abstract description 194
- 230000033001 locomotion Effects 0.000 claims abstract description 100
- 239000000758 substrate Substances 0.000 claims abstract description 19
- 230000004888 barrier function Effects 0.000 claims description 14
- 239000011148 porous material Substances 0.000 claims description 12
- 238000009434 installation Methods 0.000 claims description 10
- 230000008844 regulatory mechanism Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 5
- 230000005540 biological transmission Effects 0.000 description 2
- 210000000234 capsid Anatomy 0.000 description 2
- 239000003651 drinking water Substances 0.000 description 2
- 235000020188 drinking water Nutrition 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000002560 therapeutic procedure Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61F—FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
- A61F5/00—Orthopaedic methods or devices for non-surgical treatment of bones or joints; Nursing devices; Anti-rape devices
- A61F5/01—Orthopaedic devices, e.g. splints, casts or braces
- A61F5/04—Devices for stretching or reducing fractured limbs; Devices for distractions; Splints
- A61F5/042—Devices for stretching or reducing fractured limbs; Devices for distractions; Splints for extension or stretching
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H1/00—Apparatus for passive exercising; Vibrating apparatus; Chiropractic devices, e.g. body impacting devices, external devices for briefly extending or aligning unbroken bones
- A61H1/008—Apparatus for applying pressure or blows almost perpendicular to the body or limb axis, e.g. chiropractic devices for repositioning vertebrae, correcting deformation
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H2201/00—Characteristics of apparatus not provided for in the preceding codes
- A61H2201/01—Constructive details
- A61H2201/0192—Specific means for adjusting dimensions
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H2201/00—Characteristics of apparatus not provided for in the preceding codes
- A61H2201/16—Physical interface with patient
- A61H2201/1602—Physical interface with patient kind of interface, e.g. head rest, knee support or lumbar support
- A61H2201/1604—Head
- A61H2201/1607—Holding means therefor
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H2201/00—Characteristics of apparatus not provided for in the preceding codes
- A61H2201/16—Physical interface with patient
- A61H2201/1657—Movement of interface, i.e. force application means
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61H—PHYSICAL THERAPY APPARATUS, e.g. DEVICES FOR LOCATING OR STIMULATING REFLEX POINTS IN THE BODY; ARTIFICIAL RESPIRATION; MASSAGE; BATHING DEVICES FOR SPECIAL THERAPEUTIC OR HYGIENIC PURPOSES OR SPECIFIC PARTS OF THE BODY
- A61H2205/00—Devices for specific parts of the body
- A61H2205/04—Devices for specific parts of the body neck
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- Health & Medical Sciences (AREA)
- Animal Behavior & Ethology (AREA)
- Veterinary Medicine (AREA)
- Public Health (AREA)
- General Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Rehabilitation Therapy (AREA)
- Physical Education & Sports Medicine (AREA)
- Pain & Pain Management (AREA)
- Epidemiology (AREA)
- Nursing (AREA)
- Orthopedic Medicine & Surgery (AREA)
- Engineering & Computer Science (AREA)
- Biomedical Technology (AREA)
- Heart & Thoracic Surgery (AREA)
- Vascular Medicine (AREA)
- Transmission Devices (AREA)
Abstract
The invention discloses a kind of neck apparatus for correcting with controllability, including annular substrate, the main through-hole structure for being provided centrally with connecting its both ends of the surface of the annular substrate, the bottom of the annular substrate is bolted multiple connecting plates, the bottom centre of each connecting plate is respectively mounted a first support bar, the bottom of first support bar is installed by one longitudinal screw governor motion, a second support bar is installed in the bottom of longitudinal screw governor motion, and the bottom of second support bar is arranged on the upper surface of a supporting substrate.The present invention utilizes aerodynamic effect driving force, have the function that quickly and efficiently, in addition, the device has longitudinal screw governor motion, can be adjusted according to different heights, improve the applicability of the device, moreover, the device has the anti-overload mechanism of air force, it is capable of the air pressure of driving force, so as to effectively prevent causing the generation of patient's neck injured phenomenon again because power traction is excessive, so as to improve the practicality of the device.
Description
Technical field
The present invention relates to neck correcting technology field, specially a kind of neck apparatus for correcting with controllability.
Background technology
China patent No. CN201710615319.9 discloses a kind of neck apparatus for correcting, including upper frame, Return spring pipe,
Head fixed cover, backboard, power transmission shaft, motor, insulation crust, airway tube, mounting shell, air pump, water pipe, kettle, handrail, seat cushion,
Base, hydraulic stem, support bar, air inlet, fixation balloon, neck protection set, shoulder sleeve, fixing strap of waist, oval ring stand, suction pipe,
Seat cushion installing plate and capsid, the hydraulic stem are fixedly mounted on base, and the top of hydraulic stem is flexibly connected support bar, support bar
Top fix rotary mounting seat pad, between the seat cushion and support bar install seat cushion installing plate, seat cushion installing plate bottom opens up
Circular groove, the neck apparatus for correcting is multiple functional, easy to use, and being improved on the premise of patient outcomes are ensured makes
With comfort level, while medical personnel's workload is alleviated, when patient carries out neck corrective therapy, first opens fixing strap of waist,
The slide fastener that neck protection is put is pulled open, allows patients head to be easily inserted in the fixed cover of head very much, opens air pump, air pump is to fixation
Air bag is inflated, and patients head is fixed after fixation balloon inflation, the fixed performance of fixation balloon is good, adaptability
By force, while head comfort is added, motor and the rotating speed of controlled motor is started by controlling switch, in appropriate speed conditions
Under, the driving wheel of motor, which rotates, drives drive axis, and power transmission shaft is carried out by the rack drives ellipse ring stand on oval ring stand
Leftward or rightward banking motion, so as to carry out head corrective therapy to patient, due to neck inconvenient activity, patient can not be normal
Drinking-water, when patient needs drinking-water, suction pipe is pushed into downwards mouth with hand, this design can make patient in unmanned help
In the case of voluntarily drunk water, it is convenient and practical, while alleviate medical personnel's workload.
Spring and gas are utilized in said apparatus in terms of power drive, power has no problem in terms of driving, but by
Do not have effective and direct control action in above-mentioned power, so its application at work has larger limitation, very
Easily cause the generation of patient's neck injured phenomenon again because power traction is excessive.
The content of the invention
It is an object of the invention to provide a kind of neck apparatus for correcting with controllability, to solve in above-mentioned background technology
The problem of proposition.
To achieve the above object, the present invention provides following technical scheme：A kind of neck apparatus for correcting with controllability, bag
Include annular substrate, the main through-hole structure for being provided centrally with connecting its both ends of the surface of the annular substrate, the annular base
The bottom of plate is bolted multiple connecting plates, and the bottom centre of each connecting plate is respectively mounted a first support bar, institute
The bottom for stating first support bar is installed by one longitudinal screw governor motion, the bottom installation one second of the longitudinal screw governor motion
Support bar, the bottom of the second support bar are arranged on the upper surface of a supporting substrate, and the annular substrate is consolidated by bolt
Surely there are the first hollow housing and the second hollow housing that two opposition are set, in first hollow housing and the second hollow housing
The heart is hollow structure, and first hollow housing and the second hollow housing are respectively mounted a master in hollow structure on its interior
Piston, the center of the main piston upper surface are respectively mounted a main expansion link for running through the first hollow housing and the second hollow housing,
A crossbeam is installed on the top of the two main expansion links, and a head fixed cover, the main piston are installed in the center of the crossbeam bottom
Bottom helical spring is installed, first hollow housing and the second hollow housing are respectively arranged with and one in counter part
The secondary admission line and main exhaust pipeline of body formula structure, and consolidated between the secondary admission line and main exhaust pipeline by a flexible pipe
Fixed connection, the side of first hollow housing and the second hollow housing is respectively arranged with the main exhaust hole with its integral structure
With main air inlet pipe road, the side of first hollow housing is provided with the anti-overload machine of air force of one and its integral structure
Structure, and main exhaust pipeline described in the anti-overload mechanism connection of the air force.
Preferably, the longitudinal screw governor motion includes longitudinal screw governor motion screw shell, longitudinal screw
The governor motion hollow section, threaded rod of longitudinal screw governor motion first, the second threaded rod of longitudinal screw governor motion, vertical
To threaded adjusting mechanism with spacing hole and longitudinal screw governor motion gag lever post.
Preferably, the longitudinal screw governor motion screw shell center is internally provided with longitudinal screw regulation machine
The hollow section of structure, the longitudinal screw governor motion is with screw shell positioned at the longitudinal screw governor motion hollow area
Between internal both ends connect the threaded rod of longitudinal screw governor motion first and the longitudinal screw regulation respectively by helicitic texture
The second threaded rod of mechanism, the second threaded rod of the threaded rod of longitudinal screw governor motion first and longitudinal screw governor motion
The longitudinal screw governor motion spacing hole, and the longitudinal screw governor motion first are provided with the inside of opposite end
Threaded rod and longitudinal screw governor motion with the other end of the second threaded rod respectively with first support bar and second support bar
End is fixedly connected, and the one longitudinal screw governor motion of inside insertion of the two longitudinal screw governor motion spacing holes is used
Gag lever post.
Preferably, the helicitic texture includes being arranged on the threaded rod of longitudinal screw governor motion first and longitudinal spiral shell
Line governor motion is with the external thread structure on the second screw thread club shaft and is arranged in longitudinal screw governor motion screw shell
Female thread structure and the external thread structure on wall are meshed with female thread structure.
Preferably, the longitudinal screw governor motion is limited with spacing hole cross-sectional profile and longitudinal screw governor motion
Position bar cross-sectional profile is triangular structure and the size and longitudinal screw of longitudinal screw governor motion spacing hole cross section
Governor motion is identical with the size of gag lever post cross section.
Preferably, the anti-overload mechanism of air force includes anti-overload mechanism main hollow casing, the sky of air force
The main hollow section of the anti-overload mechanism of aerodynamic force, the anti-overload mechanism air-filled pore of air force, the anti-overload mechanism of air force use
Groove type section, the anti-overload mechanism air admission hole of air force, anti-overload mechanism secondary hollow casing, the air force of air force
The hollow section of anti-overload mechanism pair, the anti-anti- overload mechanism of overload mechanism Inflation door core, air force of air force are used flexible
Connecting rod, air force anti-overload mechanism barrier valve, the anti-overload mechanism piston of air force and the anti-overload machine of air force
Structure steam vent.
Preferably, the anti-overload mechanism of air force is moved with the air that is provided centrally with inside main hollow casing
The main hollow section of the anti-overload mechanism of power, the anti-overload mechanism of air force is with the inside of main hollow casing positioned at the sky
The anti-overload mechanism of aerodynamic force is provided with the anti-overload mechanism air-filled pore of air force, and the air with the side in main hollow section
The anti-overload mechanism of power is provided with the anti-overload mechanism Inflation door core of an air force, the air force with the inside of air-filled pore
Anti- overload mechanism with main hollow casing positioned at the main hollow section of the anti-overload mechanism of the air force be internally provided with and
The secondary hollow casing of the anti-overload mechanism of air force of its integral structure, the anti-overload mechanism of air force are secondary hollow outer
Shell is internally provided with the secondary hollow section of the anti-overload mechanism of the air force, the anti-overload mechanism inflation of air force
The one end in hole connects the secondary hollow section of the anti-overload mechanism of the air force, and the anti-overload mechanism master of air force is hollow
The inside of shell connects air and moved being provided with positioned at the anti-overload mechanism of the air force with the other end in main hollow section
The anti-overload mechanism groove type section of air force in the main hollow section of the anti-overload mechanism of power, the anti-overload machine of air force
Structure is prevented with the air force for being internally provided with the anti-overload mechanism groove type section of the connection air force of main hollow casing
The mechanism that overloads air admission hole, one end connection main exhaust hole of the anti-overload mechanism air admission hole of air force, the air move
The anti-overload mechanism of power is with secondary hollow casing in the inside installation one positioned at the secondary hollow section of the anti-overload mechanism of the air force
An institute is installed at the anti-overload mechanism piston of air force, the end face center of the anti-overload mechanism piston of air force
The flexible connecting rod of the anti-overload mechanism of air force is stated, and the anti-overload mechanism of the air force is passed through with the body of rod of flexible connecting rod
Wear the end of the secondary hollow casing of the anti-overload mechanism of the air force, the flexible connecting rod of the anti-overload mechanism of air force
The one anti-overload machine of air force is being installed with one end outside secondary hollow casing positioned at the anti-overload mechanism of the air force
Structure barrier valve, the anti-overload mechanism of air force are inserted into the anti-overload mechanism groove type of the air force with barrier valve
The inside in section, the anti-overload mechanism of air force are internally provided with the anti-overload mechanism of an air force with main hollow casing
With steam vent, and one end of the anti-overload mechanism steam vent of the air force connects the anti-overload mechanism of the air force with recessed
The end of flute profile section side, the other end of the anti-overload mechanism steam vent of air force, which connects the air force, to be prevented surpassing
The external world of the main hollow casing of mounted mechanism.
Preferably, physical dimension and the air force anti-overload of the anti-overload mechanism of air force with barrier valve
Mechanism is identical with the physical dimension in groove type section.
Compared with prior art, the beneficial effects of the invention are as follows：The present invention utilizes aerodynamic effect driving force, has fast
Speed and efficient effect, in addition, the device has longitudinal screw governor motion, can be adjusted according to different heights, improve
The applicability of the device, moreover, the device has the anti-overload mechanism of air force, is capable of the air pressure of driving force, so as to
Effectively prevent from causing the generation of patient's neck injured phenomenon again because power traction is excessive, so as to improve the reality of the device
The property used.
Brief description of the drawings
Fig. 1 is a kind of structural representation of the neck apparatus for correcting with controllability of the present invention；
Fig. 2 is the structural representation of longitudinal screw governor motion in a kind of neck apparatus for correcting with controllability of the present invention
Figure；
Fig. 3 is the structural representation of the anti-overload mechanism of air force in a kind of neck apparatus for correcting with controllability of the present invention
Figure；
In figure：1, annular substrate, 2, connecting plate, 3, first support bar, 4, longitudinal screw governor motion, 41, longitudinal spiral shell
Line governor motion screw shell, 42, longitudinal screw governor motion hollow section, 43, the spiral shell of longitudinal screw governor motion first
Rasp bar, 44, longitudinal screw governor motion the second threaded rod, 45, longitudinal screw governor motion spacing hole, 46, longitudinal screw
Governor motion gag lever post, 5, second support bar, 6, supporting substrate, 7, main through-hole structure, 8, the first hollow housing, 9, in second
Empty capsid, 10, main piston, 11, helical spring, 12, secondary admission line, 13, main exhaust pipeline, 14, main exhaust hole, 15, master enter
Feed channel, 16, the anti-overload mechanism of air force, 161, anti-overload mechanism main hollow casing, 162 of air force, air force
Anti- the overload hollow section of mechanism master, 163, the anti-overload mechanism air-filled pore of air force, 164, the anti-overload mechanism of air force
It is secondary hollow outer with groove type section, 165, the anti-overload mechanism air admission hole of air force, 166, the anti-overload mechanism of air force
Shell, 167, the secondary hollow section of the anti-overload mechanism of air force, 168, the anti-overload mechanism Inflation door core of air force, 169 are empty
The anti-overload mechanism of aerodynamic force flexible connecting rod, 1610, air force anti-overload mechanism barrier valve, 1611, air force is prevented
The mechanism that overloads piston, 1612, the anti-overload mechanism steam vent of air force, 17, flexible pipe, 18, main expansion link, 19, crossbeam,
20, head fixed cover.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
A kind of referring to Fig. 1, embodiment provided by the invention：Including annular substrate 1, in the annular substrate 1
The heart is provided with the main through-hole structure 7 for connecting its both ends of the surface, and the bottom of the annular substrate 1 is bolted multiple connecting plates
2, the bottom centre of each connecting plate 2 is respectively mounted a first support bar 3, and the bottom installation one of the first support bar 3 is vertical
To threaded adjusting mechanism 4, a second support bar 5, the second support bar 5 are installed in the bottom of the longitudinal screw governor motion 4
Bottom be arranged on a supporting substrate 6 upper surface, the annular substrate 1 be bolted two opposition setting first
The hollow housing 9 of hollow housing 8 and second, the center of the hollow housing 9 of the first hollow housing 8 and second is hollow structure,
The hollow housing 9 of first hollow housing 8 and second is respectively mounted a main piston 10, the master in hollow structure on its interior
The center of the upper surface of piston 10 is respectively mounted a main expansion link 18 for running through the first hollow housing 8 and the second hollow housing 9, described in two
A crossbeam 19 is installed on the top of main expansion link 18, and a head fixed cover 20, the main work are installed in the center of the bottom of crossbeam 19
The bottom of plug 10 is provided with helical spring 11, and the hollow housing 9 of the first hollow housing 8 and second is set respectively in counter part
There are the secondary admission line 12 and main exhaust pipeline 13 with its integral structure, and the secondary admission line 12 and main exhaust pipeline 13
Between be fixedly connected by a flexible pipe 17, the side of the hollow housing 9 of the first hollow housing 8 and second is respectively arranged with and it
The main exhaust hole 14 and main air inlet pipe road 15 of integral structure, the side of first hollow housing 8 are provided with one and its one
The anti-overload mechanism 16 of air force of formula structure, and the anti-overload mechanism 16 of the air force connects the main exhaust pipeline 14.
Referring to Fig. 2, the longitudinal screw governor motion 4 includes longitudinal screw governor motion screw shell 41, longitudinal direction
Threaded adjusting mechanism is with hollow section 42, the first threaded rod of longitudinal screw governor motion 43, longitudinal screw governor motion with second
Threaded rod 44, longitudinal screw governor motion spacing hole 45 and longitudinal screw governor motion gag lever post 46；The longitudinal screw
The center of governor motion screw shell 41 is internally provided with longitudinal screw governor motion hollow section 42, the longitudinal screw
Governor motion screw shell 41 is passing through screw thread positioned at the longitudinal screw governor motion with the both ends inside hollow section 42
Structure connects the second threaded rod 44 of first threaded rod of longitudinal screw governor motion 43 and longitudinal screw governor motion respectively,
First threaded rod of longitudinal screw governor motion 43 and longitudinal screw governor motion are with the second threaded rod 44 in opposite end
Portion is provided with the longitudinal screw governor motion spacing hole 45, and the He of the first threaded rod of longitudinal screw governor motion 43
The longitudinal screw governor motion other end of the second threaded rod 44 end with first support bar 3 and second support bar 5 respectively
It is fixedly connected, the two longitudinal screw governor motions are limited with the one longitudinal screw governor motion of inside insertion of spacing hole 45
Position bar 46；The helicitic texture includes being arranged on the first threaded rod of longitudinal screw governor motion 43 and longitudinal screw the regulation machine
Structure is with the external thread structure on the body of rod of the second threaded rod 44 and is arranged on the inwall of longitudinal screw governor motion screw shell 41
Female thread structure and the external thread structure be meshed with female thread structure；The longitudinal screw governor motion spacing hole
45 cross-sectional profiles are triangular structure with the cross-sectional profile of gag lever post 46 with longitudinal screw governor motion and longitudinal screw is adjusted
It is identical with the size of the cross section of longitudinal screw governor motion gag lever post 46 with the size of the cross section of spacing hole 45 to save mechanism, it is led
Acting on is：Play a part of adjusting height, when rotating longitudinal screw governor motion with screw shell 41, due to the screw thread
Structure includes being arranged on the second threaded rod of first threaded rod of longitudinal screw governor motion 43 and longitudinal screw governor motion
External thread structure on 44 bodies of rod and the female thread structure being arranged on the inwall of longitudinal screw governor motion screw shell 41 and
The external thread structure is meshed with female thread structure；The longitudinal screw governor motion is with the cross-sectional profile of spacing hole 45 with indulging
With the cross-sectional profile of gag lever post 46 it is triangular structure and longitudinal screw governor motion spacing hole 45 to threaded adjusting mechanism
The size of cross section is identical with the size of the cross section of gag lever post 46 with longitudinal screw governor motion, so being adjusted in rotation longitudinal screw
When saving mechanism with screw shell 41, in the presence of helicitic texture, the first threaded rod of longitudinal screw governor motion 43 can be changed
And relative distance of the longitudinal screw governor motion between the second threaded rod 44, and then the height of the device can be adjusted, adapt to
Human height.
Referring to Fig. 3, the anti-overload mechanism 16 of air force includes the main hollow casing of the anti-overload mechanism of air force
161st, the main hollow section 162 of the anti-overload mechanism of air force, the anti-overload mechanism air-filled pore 163 of air force, air force
Anti- overload mechanism groove type section 164, the anti-overload mechanism air admission hole 165 of air force, the anti-overload mechanism of air force use
The secondary hollow section 167 of the anti-overload mechanism of secondary hollow casing 166, air force, the anti-overload mechanism Inflation door core of air force
168th, the anti-overload mechanism of air force flexible connecting rod 169, air force anti-overload mechanism barrier valve 1610, air force
The anti-overload mechanism anti-overload mechanism steam vent 1612 of piston 1611 and air force；The anti-overload mechanism of air force uses
The main hollow section 162 of the anti-overload mechanism of the air force is provided centrally with inside main hollow casing 161, the air moves
The anti-overload mechanism of power is with the inside of main hollow casing 161 positioned at the main hollow section 162 of the anti-overload mechanism of the air force
Side be provided with the anti-overload mechanism air-filled pore 163 of air force, and the anti-overload mechanism air-filled pore 163 of the air force
Inside the anti-overload mechanism Inflation door core 168 of one air force is installed, the anti-overload mechanism of air force leads hollow
Shell 161 is in being internally provided with and its integral structure positioned at the anti-main hollow section 162 of overload mechanism of the air force
The anti-overload mechanism secondary hollow casing 166 of air force, the mechanism that overloads that the air force is anti-is interior with secondary hollow casing 166
Portion is provided with the secondary hollow section 167 of the anti-overload mechanism of the air force, the anti-overload mechanism air-filled pore of air force
163 one end connects the secondary hollow section 167 of the anti-overload mechanism of the air force, the anti-overload mechanism master of air force
The inside of hollow casing 161 is being provided with positioned at the anti-overload mechanism of the air force with the other end in main hollow section 162
The anti-overload mechanism groove type section 164 of air force in the main hollow section 162 of the anti-overload mechanism of air force is connected, it is described
The anti-overload mechanism of air force is internally provided with the anti-overload mechanism groove of the connection air force with main hollow casing 161
The anti-overload mechanism air admission hole 165 of air force in shape section 164, the anti-overload mechanism air admission hole 165 of air force
One end connection main exhaust hole 14, the anti-overload mechanism of air force are prevented with secondary hollow casing 166 positioned at the air force
The anti-overload mechanism piston 1611 of the air force of inside installation one in the secondary hollow section 167 of the mechanism that overloads, the air
The flexible connecting rod of the anti-overload mechanism of the air force of end face center installation one of power anti-overload mechanism piston 1611
169, and the anti-overload mechanism of the air force is used with the body of rod of flexible connecting rod 169 through the anti-overload mechanism of the air force
The end of secondary hollow casing 166, the anti-overload mechanism of air force are prevented with flexible connecting rod 169 positioned at the air force
One end installation one air force anti-overload mechanism barrier valve 1610 of the mechanism that overloads outside secondary hollow casing 166, institute
State the anti-overload mechanism barrier valve 1610 of air force and be inserted into the anti-overload mechanism groove type section 164 of the air force
Inside, the anti-overload mechanism of air force are used with the anti-overload mechanism of an air force that is internally provided with of main hollow casing 161
Steam vent 1612, and the anti-overload mechanism of the air force connects the anti-overload machine of air force with one end of steam vent 1612
The end of the structure side of groove type section 164, the anti-overload mechanism of air force connect institute with the other end of steam vent 1612
State the external world of the main hollow casing 161 of the anti-overload mechanism of air force；Air force anti-overload mechanism barrier valve 1610
Physical dimension and the air force it is anti-overload mechanism it is identical with the physical dimension in groove type section 164, its main function is：
Before use, injecting certain gas to the inside in the secondary hollow section 167 of the anti-overload mechanism of air force by air compressor
Pressure, necessarily notice that the atmospheric pressure value should be less than the maximum bearing value of patient's neck traction, when air pressure once exceeding the nominal pressure
When, the anti-overload mechanism barrier valve 1610 of air force can exit the anti-overload mechanism groove type section 164 of air force, and more
Remaining air can be discharged by the anti-overload mechanism steam vent 1612 of air force, prevent air from overloading.
Specifically used mode：In present invention work, longitudinal screw governor motion 4 is first adjusted so that the device adapts to patient
Height, patient inserts the head into the inside of main through-hole structure 7, then by head fixed cover 20 of the prior art according to doctor
Institute provides the head of immobilized patients, then main air inlet pipe road 15 is connected by air compressor, to the inside in main air inlet pipe road 15
Air is injected, due to the continuous lifting of air pressure, expansion link 18 moves up, when expansion link 18 rises to correct position, due to
The effect of patient's neck, air-pressure stable is caused to be equal to the suitable traction of patient's neck in a stationary value, the stationary value
Value, in the presence of air compressor, air is injected into again, and the atmospheric pressure value once exceedes the anti-overload mechanism 16 of air force
Nominal pressure, unnecessary gas can be discharged by the anti-overload mechanism 16 of air force, once have gas discharge, you can close empty
Air compressor, now, you can form effective draw, after hours, open main air inlet pipe road 15, you can realize air
Outer row.
It is obvious to a person skilled in the art that the invention is not restricted to the details of above-mentioned one exemplary embodiment, Er Qie
In the case of without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, the scope of the present invention is by appended power
Profit requires rather than described above limits, it is intended that all in the implication and scope of the equivalency of claim by falling
Change is included in the present invention.Any reference in claim should not be considered as to the involved claim of limitation.
Claims (8)
1. a kind of neck apparatus for correcting with controllability, including annular substrate (1), it is characterised in that：The annular base
The main through-hole structure (7) for being provided centrally with connecting its both ends of the surface of plate (1), the bottom of the annular substrate (1) pass through bolt
Fixed multiple connecting plates (2), the bottom centre of each connecting plate (2) are respectively mounted a first support bar (3), described first
A longitudinal screw governor motion (4) is installed in the bottom of strut (3), the bottom installation 1 of the longitudinal screw governor motion (4) the
Two support bars (5), the bottom of the second support bar (5) are arranged on the upper surface of a supporting substrate (6), the annular substrate
(1) the first hollow housing (8) and the second hollow housing (9) of the setting of two opposition, first hollow shell are bolted
The center of body (8) and the second hollow housing (9) is hollow structure, first hollow housing (8) and the second hollow housing (9)
A main piston (10) is respectively mounted in hollow structure on its interior, the center of main piston (10) upper surface is respectively mounted always
Wear the main expansion link (18) of the first hollow housing (8) and the second hollow housing (9), the top installation of the two main expansion links (18)
A head fixed cover (20), the bottom peace of the main piston (10) are installed in one crossbeam (19), the center of crossbeam (19) bottom
Equipped with helical spring (11), first hollow housing (8) and the second hollow housing (9) counter part be respectively arranged with and its
The secondary admission line (12) and main exhaust pipeline (13) of integral structure, and the secondary admission line (12) and main exhaust pipeline
(13) it is fixedly connected between by a flexible pipe (17), the side difference of first hollow housing (8) and the second hollow housing (9)
It is provided with and the main exhaust hole of its integral structure (14) and main air inlet pipe road (15), the side of first hollow housing (8)
One and the anti-overload mechanism (16) of the air force of its integral structure are provided with, and the anti-overload mechanism (16) of the air force is even
Lead to the main exhaust pipeline (14).
A kind of 2. neck apparatus for correcting with controllability according to claim 1, it is characterised in that：The longitudinal screw
Governor motion (4) include longitudinal screw governor motion screw shell (41), longitudinal screw governor motion with hollow section (42),
The threaded rod of longitudinal screw governor motion first (43), longitudinal screw governor motion the second threaded rod (44), longitudinal screw regulation
Mechanism spacing hole (45) and longitudinal screw governor motion gag lever post (46).
A kind of 3. neck apparatus for correcting with controllability according to claim 2, it is characterised in that：The longitudinal screw
Governor motion screw shell (41) center is internally provided with longitudinal screw governor motion hollow section (42), the longitudinal direction
Threaded adjusting mechanism is with screw shell (41) positioned at the internal both ends in the hollow section of the longitudinal screw governor motion (42)
The threaded rod of longitudinal screw governor motion first (43) and longitudinal screw governor motion are connected respectively by helicitic texture with
Two threaded rods (44), the second threaded rod of the threaded rod of longitudinal screw governor motion first (43) and longitudinal screw governor motion
(44) the longitudinal screw governor motion spacing hole (45) is provided with the inside of opposite end, and the longitudinal screw is adjusted
The threaded rod of mechanism first (43) and longitudinal screw governor motion are supported with first respectively with the other end of the second threaded rod (44)
Bar (3) is fixedly connected with the end of second support bar (5), and the two longitudinal screw governor motions are inserted with the inside of spacing hole (45)
Enter a longitudinal screw governor motion gag lever post (46).
A kind of 4. neck apparatus for correcting with controllability according to claim 3, it is characterised in that：The helicitic texture
Including being arranged on the second threaded rod of the threaded rod of longitudinal screw governor motion first (43) and longitudinal screw governor motion
(44) external thread structure on the body of rod and the internal thread knot being arranged on longitudinal screw governor motion screw shell (41) inwall
The structure and external thread structure is meshed with female thread structure.
A kind of 5. neck apparatus for correcting with controllability according to claim 3, it is characterised in that：The longitudinal screw
Governor motion is three with spacing hole (45) cross-sectional profile and longitudinal screw governor motion with gag lever post (46) cross-sectional profile
Angular structure and longitudinal screw governor motion are with the size and longitudinal screw governor motion gag lever post of spacing hole (45) cross section
(46) size of cross section is identical.
A kind of 6. neck apparatus for correcting with controllability according to claim 1, it is characterised in that：The air force
Anti- overload mechanism (16) includes the anti-overload mechanism master of the anti-overload mechanism main hollow casing (161) of air force, air force
Hollow section (162), the anti-overload mechanism air-filled pore (163) of air force, the anti-overload mechanism groove type section of air force
(164), the anti-overload mechanism air admission hole (165) of air force, the anti-overload mechanism secondary hollow casing (166) of air force, sky
The secondary hollow section (167) of the anti-overload mechanism of aerodynamic force, the anti-overload mechanism Inflation door core (168) of air force, air force
Anti- overload mechanism flexible connecting rod (169), the anti-overload mechanism barrier valve (1610) of air force, the anti-overload machine of air force
The structure anti-mechanism steam vent (1612) that overloads of piston (1611) and air force.
A kind of 7. neck apparatus for correcting with controllability according to claim 6, it is characterised in that：The air force
Anti- overload mechanism is provided centrally with the main hollow section of the anti-overload mechanism of the air force with main hollow casing (161) inside
(162), the air force it is anti-overload mechanism with the inside of main hollow casing (161) positioned at the anti-overload machine of the air force
Structure is provided with the anti-overload mechanism air-filled pore (163) of air force, and the air force with the side of main hollow section (162)
Anti- overload mechanism is provided with the anti-overload mechanism Inflation door core (168) of an air force, the sky with the inside of air-filled pore (163)
The anti-overload mechanism of aerodynamic force is with main hollow casing (161) positioned at the main hollow section of the anti-overload mechanism of the air force
(162) be internally provided with and anti-overload mechanism secondary hollow casing (166), the air of the air force of its integral structure
The anti-overload mechanism of power is internally provided with the secondary hollow section of the anti-overload mechanism of the air force with secondary hollow casing (166)
(167), the anti-overload mechanism of the air force connects the anti-overload mechanism pair of the air force with one end of air-filled pore (163)
Hollow section (167), the anti-overload mechanism of air force is with the inside of main hollow casing (161) positioned at the air force
Anti- overload mechanism is provided with the main hollow section of the anti-overload mechanism of connection air force with the other end of main hollow section (162)
(162) air force anti-overload mechanism groove type section (164), the main hollow casing of the anti-overload mechanism of air force
(161) the anti-overload of air force for being internally provided with anti-overload mechanism groove type section (164) of the connection air force
Mechanism connects main exhaust hole (14) with air admission hole (165), the anti-overload mechanism of air force with one end of air admission hole (165),
The anti-overload mechanism of air force is with secondary hollow casing (166) positioned at the secondary hollow section of the anti-overload mechanism of the air force
Between (167) the air force anti-overload mechanism piston (1611), the anti-overload mechanism of air force of inside installation one
The one flexible connecting rod (169) of the anti-overload mechanism of air force is installed with the end face center of piston (1611), and it is described
The anti-overload mechanism of air force is secondary hollow outer through the anti-overload mechanism of the air force with the body of rod of flexible connecting rod (169)
The end of shell (166), the anti-overload mechanism of air force is with flexible connecting rod (169) positioned at the anti-overload of the air force
The mechanism outside anti-overload mechanism barrier valve (1610) of one air force of one end installation of secondary hollow casing (166), institute
State the anti-overload mechanism of air force and be inserted into the anti-overload mechanism groove type section of the air force with barrier valve (1610)
(164) inside, the anti-overload mechanism of air force prevent surpassing with the air force that is internally provided with of main hollow casing (161)
Mounted mechanism is with steam vent (1612), and the anti-overload mechanism of the air force connects the air with one end of steam vent (1612)
The end of anti-overload mechanism groove type section (164) side of power, the anti-overload mechanism steam vent of air force
(1612) the other end connects the external world of anti-overload mechanism main hollow casing (161) of the air force.
A kind of 8. neck apparatus for correcting with controllability according to claim 7, it is characterised in that：The air force
Physical dimension and the air force anti-overload mechanism groove type section (164) of the anti-overload mechanism with barrier valve (1610)
Physical dimension is identical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711168804.2A CN107669387A (en) | 2017-11-21 | 2017-11-21 | A kind of neck apparatus for correcting with controllability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711168804.2A CN107669387A (en) | 2017-11-21 | 2017-11-21 | A kind of neck apparatus for correcting with controllability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107669387A true CN107669387A (en) | 2018-02-09 |
Family
ID=61149194
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711168804.2A Pending CN107669387A (en) | 2017-11-21 | 2017-11-21 | A kind of neck apparatus for correcting with controllability |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107669387A (en) |
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| CN108403280A (en) * | 2018-03-20 | 2018-08-17 | 李志慧 | A kind of neck apparatus for correcting with anti-secondary injury function |
| CN110107183A (en) * | 2019-05-16 | 2019-08-09 | 郭丽云 | A kind of revolving door bottom driving type mounting device |
| CN110206982A (en) * | 2019-06-11 | 2019-09-06 | 郭玉卿 | A kind of ballast support device with universal adjustment function |
| CN110419422A (en) * | 2019-08-13 | 2019-11-08 | 耀华园林股份有限公司 | A kind of rock side slope ecological protection greening irrigation device and its working method |
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| CN108403280A (en) * | 2018-03-20 | 2018-08-17 | 李志慧 | A kind of neck apparatus for correcting with anti-secondary injury function |
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| CN110107183A (en) * | 2019-05-16 | 2019-08-09 | 郭丽云 | A kind of revolving door bottom driving type mounting device |
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| CN110419422A (en) * | 2019-08-13 | 2019-11-08 | 耀华园林股份有限公司 | A kind of rock side slope ecological protection greening irrigation device and its working method |
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Application publication date: 20180209 |
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