CN216603720U - Anticreep autogenous cutting sleeve pipe - Google Patents
Anticreep autogenous cutting sleeve pipe Download PDFInfo
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- CN216603720U CN216603720U CN202122248177.1U CN202122248177U CN216603720U CN 216603720 U CN216603720 U CN 216603720U CN 202122248177 U CN202122248177 U CN 202122248177U CN 216603720 U CN216603720 U CN 216603720U
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Abstract
The utility model relates to an anti-drop autogenous cutting sleeve, comprising: the aircraft wing, the autogenous cutting body, the first sleeve fixing strap, the second sleeve fixing strap and the third sleeve fixing strap; wherein, the aircraft wing includes: the middle part is in an oval shape, and the other parts which are symmetrically arranged at the upper side and the lower side of the middle part and are in a rounded trapezoid shape; a through hole of a gas cutting pipe body is formed in the middle of the middle part of the airplane wing, the gas cutting pipe body penetrates through the through hole of the gas cutting pipe body, and the gas cutting pipe body is fixedly connected with the airplane wing; a plurality of fixing through holes are formed in the two sides of the airplane wing, and one end of the sleeve fixing band penetrates through the fixing through holes of the airplane wing to be fixed. The airplane wing and the three sleeve fixing belts in the anti-falling tracheostomy sleeve disclosed by the utility model are arranged, so that the three sleeve fixing belts are tied at the upper neck of a patient, the tracheostomy tube body is prevented from falling off and shifting, and the degree of tightness between the three sleeve fixing belts and the neck of the patient can be well adjusted by the magic tapes used at the ends of the three sleeve fixing belts.
Description
Technical Field
The utility model relates to the technical field of medical instruments, in particular to an anti-falling tracheostomy cannula.
Background
Tracheotomy is a common operation in which the neck trachea is cut open, and a tracheostomy cannula is inserted into the cut to allow a patient to breathe directly through the tracheostomy tube, thereby solving the problems of dyspnea and respiratory dysfunction caused by retention of laryngeal or lower respiratory secretions. The currently used sleeve fixing band is usually worn for a long time to cause the falling off of the airplane wing and the tracheostomy tube body, which causes pain and some complications for patients.
In order to deal with such problems, clinical nursing staff often fasten the sleeve fixing belt to prevent the sleeve fixing belt from falling off, but the problem of tight feeling, low comfort and the like of a patient is easily caused by the fixing method.
Therefore, an anti-drop tracheostomy cannula is needed.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an anti-drop autogenous cutting sleeve aiming at the defects in the prior art.
In order to achieve the purpose, the utility model adopts the technical scheme that:
an anti-run autogenous cutting cannula comprising: the aircraft wing, the autogenous cutting body, the first sleeve fixing strap, the second sleeve fixing strap and the third sleeve fixing strap;
wherein the aircraft wing includes: the middle part is in an oval shape, and the other parts are symmetrically arranged on the upper side and the lower side of the middle part and are in a circular trapezoid shape;
a through hole of a gas cutting pipe body is formed in the middle of the middle part of the aircraft wing, the gas cutting pipe body penetrates through the through hole of the gas cutting pipe body, and the gas cutting pipe body is fixedly connected with the aircraft wing; a plurality of fixing through holes are formed in two sides of the aircraft wing, one end of the first sleeve fixing band penetrates through one fixing through hole in the middle of the aircraft wing and then is fixed by itself, and the other end of the first sleeve fixing band penetrates through one fixing through hole in the other side of the middle of the aircraft wing and then is fixed by itself; one end of the second sleeve fixing band penetrates through one fixing through hole in the upper half part of the airplane wing and then is fixed by itself, and the other end of the second sleeve fixing band penetrates through one fixing through hole in the other side of the upper half part of the airplane wing and then is fixed by itself; one end of the third sleeve fixing band penetrates through a fixing through hole on the lower half portion of the airplane wing and then is fixed, and the other end of the third sleeve fixing band penetrates through a fixing through hole on the other side of the lower half portion of the airplane wing and then is fixed.
Preferably, the aircraft wing is made of medical aluminum alloy material.
Preferably, the tracheostomy tube body is made of a medical aluminum alloy material.
Preferably, the end parts of the first sleeve fixing band, the second sleeve fixing band and the third sleeve fixing band are all self-fixed through magic tapes.
Preferably, the first sleeve retaining band is made of elastic fiber.
Preferably, the second and third sleeve retaining bands are made of elastane.
Preferably, the outer diameter of the tracheostomy tube body is 9-14 mm.
By adopting the technical scheme, compared with the prior art, the utility model has the following technical effects:
according to the anti-falling autogenous cutting sleeve, the airplane wing and the three sleeve fixing belts are arranged, so that the first sleeve fixing belt, the second sleeve fixing belt and the third sleeve fixing belt are tied at the upper neck of a patient, the autogenous cutting tube body is prevented from falling off and shifting, and the degree of tightness between the three sleeve fixing belts and the neck of the patient can be well adjusted through the magic tapes used at the ends of the three sleeve fixing belts.
Drawings
FIG. 1 is a schematic view of the configuration of an aircraft wing and a sleeve retaining strap of the present invention;
FIG. 2 is a schematic view of the tracheostomy tube of the present invention;
wherein the reference numerals include: aircraft wing 1, autogenous cutting body 2, first sleeve fixed band 3, second sleeve fixed band 4 and third sleeve fixed band 5.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
It should be noted that the embodiments and features of the embodiments may be combined with each other without conflict.
The utility model is further described with reference to the following drawings and specific examples, which are not intended to be limiting.
Examples
As shown in fig. 1-2, the present embodiment provides an anti-loose tracheostomy cannula, comprising: the aircraft wing 1, the autogenous cutting tube body 2, the first sleeve fixing band 3, the second sleeve fixing band 4 and the third sleeve fixing band 5;
wherein the aircraft wing 1 comprises: the middle part is in an oval shape, and the other parts are symmetrically arranged on the upper side and the lower side of the middle part and are in a rounded trapezoid shape;
a through hole of a gas cutting pipe body is formed in the middle of the middle part of the aircraft wing 1, the gas cutting pipe body 2 penetrates through the through hole of the gas cutting pipe body, and the gas cutting pipe body 2 is fixedly connected with the aircraft wing 1; a plurality of fixing through holes are formed in two sides of the aircraft wing 1, one end of the first sleeve fixing band 3 penetrates through one fixing through hole in the middle of the aircraft wing 1 and then is fixed by itself, and the other end of the first sleeve fixing band 3 penetrates through one fixing through hole in the other side of the middle of the aircraft wing 1 and then is fixed by itself; one end of the second sleeve fixing band 4 passes through one fixing through hole on the upper half part of the aircraft wing 1 and then is fixed by itself, and the other end of the second sleeve fixing band 4 passes through one fixing through hole on the other side of the upper half part of the aircraft wing 1 and then is fixed by itself; one end of the third sleeve fixing band 5 passes through a fixing through hole on the lower half part of the airplane wing 1 and then is fixed, and the other end of the third sleeve fixing band 5 passes through a fixing through hole on the other side of the lower half part of the airplane wing 1 and then is fixed.
Preferably, the aircraft wing 1 is made of medical aluminum alloy material.
Preferably, the tracheostomy tube body 2 is made of a medical aluminum alloy material.
Preferably, the ends of the first sleeve fixing band 3, the second sleeve fixing band 4 and the third sleeve fixing band 5 are all self-fixed by a hook and loop fastener.
Preferably, the first sleeve-fixing band 3 is made of elastic fiber.
Preferably, the second 4 and third 5 sleeve fixing strips are made of elastane.
Preferably, the outer diameter of the tracheostomy tube body 2 is 10 millimeters.
In conclusion, the arrangement of the aircraft wing and the three sleeve fixing belts in the anti-drop tracheostomy sleeve ensures that the tracheostomy tube body does not fall off and shift because the first sleeve fixing belt, the second sleeve fixing belt and the third sleeve fixing belt are tied at the neck of a patient, and the tightness degree between the three sleeve fixing belts and the neck of the patient can be well adjusted by the magic tapes used at the ends of the three sleeve fixing belts.
While the utility model has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the utility model.
Claims (7)
1. An anti-run autogenous cutting sleeve, comprising: the aircraft wing fixing device comprises an aircraft wing (1), a tracheostomy tube body (2), a first cannula fixing band (3), a second cannula fixing band (4) and a third cannula fixing band (5);
wherein the aircraft wing (1) comprises: the middle part is in an oval shape, and the other parts are symmetrically arranged on the upper side and the lower side of the middle part and are in a rounded trapezoid shape;
a gas cutting pipe body through hole is formed in the middle of the middle part of the aircraft wing (1), the gas cutting pipe body (2) penetrates through the gas cutting pipe body through hole, and the gas cutting pipe body (2) is fixedly connected with the aircraft wing (1); a plurality of fixing through holes are formed in two sides of the aircraft wing (1), one end of the first sleeve fixing band (3) penetrates through one fixing through hole in the middle of the aircraft wing (1) and then is fixed by itself, and the other end of the first sleeve fixing band (3) penetrates through one fixing through hole in the other side of the middle of the aircraft wing (1) and then is fixed by itself; one end of the second sleeve fixing strap (4) penetrates through a fixing through hole in the upper half part of the aircraft wing (1) and then is fixed by itself, and the other end of the second sleeve fixing strap (4) penetrates through a fixing through hole in the other side of the upper half part of the aircraft wing (1) and then is fixed by itself; one end of the third sleeve fixing band (5) penetrates through a fixing through hole on the lower half portion of the airplane wing (1) and then is fixed, and the other end of the third sleeve fixing band (5) penetrates through a fixing through hole on the other side of the lower half portion of the airplane wing (1) and then is fixed.
2. The anti-run-off autogenous cutting cannula according to claim 1, characterized in that the aircraft wing (1) is made of medical aluminum alloy material.
3. The anti-run-off tracheostomy cannula according to claim 1, characterized in that said tracheostomy tube body (2) is made of a medical aluminum alloy material.
4. The anti-run-off tracheostomy cannula according to claim 1, characterized in that the ends of the first cannula fixation strap (3), the second cannula fixation strap (4) and the third cannula fixation strap (5) are all self-fixed by hook and loop fasteners.
5. The anti-run-off tracheostomy cannula according to claim 1, characterized in that the first cannula fixation strap (3) is made of elastane.
6. The anti-run-off autogenous cutting cannula according to claim 1, characterized in that the second (4) and third (5) cannula fixation bands are made of elastane fiber.
7. The anti-run-off autogenous cutting bushing according to claim 1, characterized in that the autogenous cutting tube body (2) has an outer diameter of 9-14 mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122248177.1U CN216603720U (en) | 2021-09-16 | 2021-09-16 | Anticreep autogenous cutting sleeve pipe |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122248177.1U CN216603720U (en) | 2021-09-16 | 2021-09-16 | Anticreep autogenous cutting sleeve pipe |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216603720U true CN216603720U (en) | 2022-05-27 |
Family
ID=81691782
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122248177.1U Active CN216603720U (en) | 2021-09-16 | 2021-09-16 | Anticreep autogenous cutting sleeve pipe |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216603720U (en) |
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2021
- 2021-09-16 CN CN202122248177.1U patent/CN216603720U/en active Active
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