CN215839973U - Aviation rescue stretcher with alarm function - Google Patents
Aviation rescue stretcher with alarm function Download PDFInfo
- Publication number
- CN215839973U CN215839973U CN202121353596.5U CN202121353596U CN215839973U CN 215839973 U CN215839973 U CN 215839973U CN 202121353596 U CN202121353596 U CN 202121353596U CN 215839973 U CN215839973 U CN 215839973U
- Authority
- CN
- China
- Prior art keywords
- support frame
- horizontal
- main
- mattress
- vertical rod
- 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.)
- Active
Links
Images
Landscapes
- Invalid Beds And Related Equipment (AREA)
Abstract
The utility model discloses an aviation rescue stretcher with an alarm function, which comprises: the bed frame, the soft pad positioned on the bed frame and the moving mechanism positioned below the bed frame; the bed frame comprises a horizontal support frame and an inclined support frame; the inclined support frame and the horizontal support frame form an obtuse angle; the soft pad comprises a horizontal mattress and an inclined mattress; the inclined mattress and the horizontal mattress form an obtuse angle; the inclined mattress protrudes upwards to form a pillow part, a collapse groove is formed in the center of the pillow part, and a pressure sensor, a single chip microcomputer and an alarm are arranged in the collapse groove; the single chip microcomputer is electrically connected with the pressure sensor and the alarm. The utility model has the beneficial effects that: the pressure sensor is used for detecting the pressure of the head of the patient to obtain a pressure signal, and the single chip microcomputer is used for judging and analyzing and then controlling the alarm to work. The alarm can be a sound alarm or a vibration alarm.
Description
Technical Field
The utility model relates to the field of nursing, in particular to an aviation rescue stretcher with an alarming function.
Background
An aviation rescue stretcher is often a device equipped in a helicopter, and is convenient for a patient and a wounded person to lie down in order to meet the requirements of illness. In the process of transporting patients, the conditions of the patients are very complicated, and some patients always have head movement and leave without permission, so that the health of the patients is not facilitated. When moving the rescue stretcher, a nurse or a doctor often cannot look at the head of the patient completely to see whether the head of the patient leaves the stretcher.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an aviation rescue stretcher with an alarm function, which can automatically alarm and relieve nursing pressure when the head of a patient leaves the stretcher.
In order to solve the technical problem, the utility model provides an aviation rescue stretcher with an alarm function, which comprises: the bed frame, the soft pad positioned on the bed frame and the moving mechanism positioned below the bed frame; the bed frame comprises a horizontal support frame and an inclined support frame; the inclined support frame and the horizontal support frame form an obtuse angle; the soft pad comprises a horizontal mattress and an inclined mattress; the inclined mattress and the horizontal mattress form an obtuse angle; the inclined mattress protrudes upwards to form a pillow part, a collapse groove is formed in the center of the pillow part, and a pressure sensor, a single chip microcomputer and an alarm are arranged in the collapse groove; the single chip microcomputer is electrically connected with the pressure sensor and the alarm.
The utility model has the beneficial effects that:
the pressure sensor is used for detecting the pressure of the head of the patient to obtain a pressure signal, and the single chip microcomputer is used for judging and analyzing and then controlling the alarm to work. The alarm can be a sound alarm or a vibration alarm.
In one embodiment, the length of the angled support is less than the length of the horizontal support, the length of the horizontal support is four to five times the length of the angled support, the length of the angled mattress is less than the length of the horizontal mattress, and the length of the horizontal mattress is four to five times the length of the angled mattress.
In one embodiment, the horizontal support frame is provided with an armrest mechanism, the armrest mechanism comprises a first armrest and a second armrest, the first armrest and the second armrest are symmetrically arranged around the horizontal support frame, and the first armrest and the second armrest are close to the inclined support frame.
In one embodiment, the first handrail and the second handrail are identical in structure and each comprise a first vertical rod, a horizontal rod and a second vertical rod; the two ends of the horizontal holding rod are respectively fixedly connected with the first vertical holding rod and the second vertical holding rod.
In one embodiment, the first vertical bar and the horizontal support frame are perpendicular to each other, the second vertical bar and the horizontal support frame are perpendicular to each other, and the first vertical bar, the horizontal bar and the second vertical bar are arranged in Contraband type.
In one embodiment, the length of the first vertical rod is the same as that of the second vertical rod, the first vertical rod, the horizontal rod and the second vertical rod are integrally formed, and the diameters of the first vertical rod, the horizontal rod and the second vertical rod are the same.
In one embodiment, the movement mechanism comprises a primary rolling assembly; the main rolling assembly comprises a main front wheel unit and a main rear wheel unit; the main front wheel unit comprises a main front wheel bracket and two main front rollers arranged on the main front wheel bracket; the main rear wheel unit comprises a main rear wheel bracket and two main rear rollers arranged on the main rear wheel bracket; the main front wheel support is hinged with the horizontal support frame, and the main rear wheel support is hinged with the horizontal support frame.
In one embodiment, the diameter of the main front roller is the same as that of the main rear roller, two main front rollers are symmetrically distributed about the main front wheel bracket, and two main rear rollers are symmetrically distributed about the main rear wheel bracket.
In one embodiment, the moving mechanism further comprises a secondary rolling assembly; the secondary rolling assembly comprises a secondary front wheel unit and a secondary rear wheel unit; the secondary front wheel unit comprises a secondary front wheel bracket and two secondary front rollers arranged on the secondary front wheel bracket; the secondary rear wheel unit comprises a secondary rear wheel bracket and two secondary rear rollers arranged on the secondary rear wheel bracket.
In one embodiment, the diameter of the secondary front roller is the same as that of the secondary rear roller, two secondary front rollers are symmetrically distributed about the secondary front wheel bracket, and two secondary rear rollers are symmetrically distributed about the secondary rear wheel bracket.
Drawings
Fig. 1 is a schematic structural diagram of an aviation rescue stretcher with an alarm function.
Fig. 2 is a schematic structural diagram of the middle pillow part of the aviation rescue stretcher with the alarm function.
Fig. 3 is a structural block diagram of the middle pillow part of the aviation rescue stretcher with the alarm function.
The reference numbers are as follows: 110. a horizontal support frame; 120. inclining the support frame; 130. a horizontal mattress; 140. tilting the mattress; 210. a pillow part; 220. collapsing the groove; 230. a pressure sensor; 240. a single chip microcomputer; 250. an alarm; 310. a first erection bar; 320. a horizontal holding rod; 330. a second vertical support rod; 410. a main front wheel support; 420. a main front roller; 430. a main rear wheel support; 440. a main rear roller; 510. a secondary front wheel support; 520. a secondary front roller; 530. a secondary rear wheel support; 540. and then the roller.
Detailed Description
The present invention is further described below in conjunction with the following figures and specific examples so that those skilled in the art may better understand the present invention and practice it, but the examples are not intended to limit the present invention.
Referring to fig. 1 to 3, an aviation rescue stretcher with an alarm function includes: the bed frame, the soft pad positioned on the bed frame and the moving mechanism positioned below the bed frame; the bed frame comprises a horizontal support frame 110 and an inclined support frame 120; the inclined support 120 and the horizontal support 110 form an obtuse angle; the cushions include a horizontal mattress 130 and a tilted mattress 140; the tilted mattress 140 and the horizontal mattress 130 form an obtuse angle; the inclined mattress 140 protrudes upwards to form a pillow part 210, a collapse groove 220 is formed in the center of the pillow part 210, and a pressure sensor 230, a single chip microcomputer 240 and an alarm 250 are arranged in the collapse groove 220; the single chip microcomputer 240 is electrically connected with the pressure sensor 230 and the alarm 250.
The head of the patient is placed in the collapse groove 220, the pressure sensor 230 detects the pressure of the head of the patient to obtain a pressure signal, and the alarm 250 is controlled to work after the pressure signal is judged and analyzed by the single chip microcomputer 240. The alarm 250 may be an audible alarm or a vibratory alarm.
Specifically, the length of the tilt frame 120 is less than the length of the horizontal frame 110, the length of the horizontal frame 110 is four to five times the length of the tilt frame 120, the length of the tilt mattress 140 is less than the length of the horizontal mattress 130, and the length of the horizontal mattress 130 is four to five times the length of the tilt mattress 140.
It will be appreciated that the specific proportions of the horizontal support 110 and the inclined support 120 may be set as appropriate, as may the specific proportions of the horizontal mattress 130 and the inclined mattress 140.
In order to facilitate the rising of the patient, the horizontal support frame 110 is provided with an armrest mechanism, the armrest mechanism includes a first armrest and a second armrest, the first armrest and the second armrest are symmetrically disposed with respect to the horizontal support frame 110, and the first armrest and the second armrest are close to the inclined support frame 120.
The specific structure of the first handrail and the second handrail, which are the same in structure and each include a first vertical rod 310, a horizontal rod 320 and a second vertical rod 330; the two ends of the horizontal handrail 320 are respectively and fixedly connected with the first vertical handrail 310 and the second vertical handrail 330. The first vertical rod 310 and the horizontal support frame 110 are perpendicular to each other, the second vertical rod 330 and the horizontal support frame 110 are perpendicular to each other, and the first vertical rod 310, the horizontal rod 320 and the second vertical rod 330 are arranged in Contraband type.
The length of the first vertical rod 310 is the same as that of the second vertical rod 330, the first vertical rod 310, the horizontal rod 320 and the second vertical rod 330 are integrally formed, and the diameters of the first vertical rod 310, the horizontal rod 320 and the second vertical rod 330 are the same.
The specific structure of the moving mechanism is described below:
in one embodiment, the movement mechanism comprises a primary rolling assembly; the main rolling assembly comprises a main front wheel unit and a main rear wheel unit; the main front wheel unit includes a main front wheel bracket 410 and two main front rollers 420 provided on the main front wheel bracket 410; the main rear wheel unit includes a main rear wheel bracket 430 and two main rear rollers 440 provided on the main rear wheel bracket 430; the main front wheel bracket 410 is hinged to the horizontal support frame 110, and the main rear wheel bracket 430 is hinged to the horizontal support frame 110. The diameter of the main front roller 420 is the same as that of the main rear roller 440, two main front rollers 420 are symmetrically distributed about the main front wheel bracket 410, and two main rear rollers 440 are symmetrically distributed about the main rear wheel bracket 430.
It will be appreciated that the main rolling assembly is mainly used for the pushing of the stretcher at regular times, in order to facilitate the pushing of the stretcher into the helicopter.
The moving mechanism further comprises a secondary rolling assembly; the secondary rolling assembly comprises a secondary front wheel unit and a secondary rear wheel unit; the secondary front wheel unit includes a secondary front wheel bracket 510 and two secondary front rollers 520 provided on the secondary front wheel bracket 510; the sub rear wheel unit includes a sub rear wheel bracket 530 and two sub rear rollers 540 provided on the sub rear wheel bracket 530. The diameter of the secondary front roller 520 is the same as that of the secondary rear roller 540, two of the secondary front rollers 520 are symmetrically distributed about the secondary front wheel support 510, and two of the secondary rear rollers 540 are symmetrically distributed about the secondary rear wheel support 530.
The above-mentioned embodiments are merely preferred embodiments for fully illustrating the present invention, and the scope of the present invention is not limited thereto. The equivalent substitution or change made by the technical personnel in the technical field on the basis of the utility model is all within the protection scope of the utility model. The protection scope of the utility model is subject to the claims.
Claims (10)
1. The utility model provides an aviation rescue stretcher with alarming function which characterized in that includes: the bed frame, the soft pad positioned on the bed frame and the moving mechanism positioned below the bed frame; the bed frame comprises a horizontal support frame and an inclined support frame; the inclined support frame and the horizontal support frame form an obtuse angle; the soft pad comprises a horizontal mattress and an inclined mattress; the inclined mattress and the horizontal mattress form an obtuse angle; the inclined mattress protrudes upwards to form a pillow part, a collapse groove is formed in the center of the pillow part, and a pressure sensor, a single chip microcomputer and an alarm are arranged in the collapse groove; the single chip microcomputer is electrically connected with the pressure sensor and the alarm.
2. The aviation rescue stretcher with alarm function as in claim 1, wherein the length of the inclined support frame is less than the length of the horizontal support frame, the length of the horizontal support frame is four to five times the length of the inclined support frame, the length of the inclined mattress is less than the length of the horizontal mattress, and the length of the horizontal mattress is four to five times the length of the inclined mattress.
3. An aviation rescue stretcher with an alarm function as in claim 1, wherein the horizontal support frame is provided with an armrest mechanism, the armrest mechanism comprises a first armrest and a second armrest, the first armrest and the second armrest are symmetrically disposed about the horizontal support frame, and the first armrest and the second armrest are adjacent to the inclined support frame.
4. The rescue stretcher with alarm function as in claim 3, wherein the first handrail and the second handrail are identical in structure and each comprise a first vertical rod, a horizontal rod and a second vertical rod; the two ends of the horizontal holding rod are respectively fixedly connected with the first vertical holding rod and the second vertical holding rod.
5. The aviation rescue stretcher with alarm function as in claim 4, wherein the first vertical rod and the horizontal support frame are perpendicular to each other, the second vertical rod and the horizontal support frame are perpendicular to each other, and the first vertical rod, the horizontal rod and the second vertical rod are arranged in Contraband type.
6. The aviation rescue stretcher with alarm function of claim 4, wherein the length of the first vertical rod is the same as that of the second vertical rod, the first vertical rod, the horizontal rod and the second vertical rod are integrally formed, and the diameters of the first vertical rod, the horizontal rod and the second vertical rod are the same.
7. The aviation rescue stretcher with alarm function of claim 1, wherein the moving mechanism comprises a main rolling assembly; the main rolling assembly comprises a main front wheel unit and a main rear wheel unit; the main front wheel unit comprises a main front wheel bracket and two main front rollers arranged on the main front wheel bracket; the main rear wheel unit comprises a main rear wheel bracket and two main rear rollers arranged on the main rear wheel bracket; the main front wheel support is hinged with the horizontal support frame, and the main rear wheel support is hinged with the horizontal support frame.
8. An aviation rescue stretcher with an alarm function as in claim 7, wherein the diameter of the main front rollers and the diameter of the main rear rollers are the same, two of the main front rollers are symmetrically distributed about the main front wheel support, and two of the main rear rollers are symmetrically distributed about the main rear wheel support.
9. An aviation rescue stretcher with alarm function as in claim 7, wherein the moving mechanism further comprises a secondary rolling assembly; the secondary rolling assembly comprises a secondary front wheel unit and a secondary rear wheel unit; the secondary front wheel unit comprises a secondary front wheel bracket and two secondary front rollers arranged on the secondary front wheel bracket; the secondary rear wheel unit comprises a secondary rear wheel bracket and two secondary rear rollers arranged on the secondary rear wheel bracket.
10. An aviation rescue stretcher with an alarm function as in claim 9, wherein the diameter of the secondary front rollers and the diameter of the secondary rear rollers are the same, two of the secondary front rollers are symmetrically distributed about the secondary front wheel bracket, and two of the secondary rear rollers are symmetrically distributed about the secondary rear wheel bracket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121353596.5U CN215839973U (en) | 2021-06-17 | 2021-06-17 | Aviation rescue stretcher with alarm function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121353596.5U CN215839973U (en) | 2021-06-17 | 2021-06-17 | Aviation rescue stretcher with alarm function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215839973U true CN215839973U (en) | 2022-02-18 |
Family
ID=80334183
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121353596.5U Active CN215839973U (en) | 2021-06-17 | 2021-06-17 | Aviation rescue stretcher with alarm function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215839973U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115231222A (en) * | 2022-07-25 | 2022-10-25 | 燕山大学 | Method for avoiding secondary damage in dragging and transporting process of injured person |
-
2021
- 2021-06-17 CN CN202121353596.5U patent/CN215839973U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115231222A (en) * | 2022-07-25 | 2022-10-25 | 燕山大学 | Method for avoiding secondary damage in dragging and transporting process of injured person |
| CN115231222B (en) * | 2022-07-25 | 2024-01-09 | 燕山大学 | Method for avoiding secondary damage in dragging and transporting process suitable for injured personnel |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2301429B1 (en) | Apparatuses for supporting and monitoring a condition of a person | |
| US8683626B1 (en) | Hospital bed with conveyor mattress | |
| KR101932212B1 (en) | Medical bed for preventing fall | |
| CN215839973U (en) | Aviation rescue stretcher with alarm function | |
| US20110296607A1 (en) | System and method for bed height adjustment | |
| US20060278771A1 (en) | Load carrying apparatus with security detection system | |
| CN106214385A (en) | Multiposition supports equipment | |
| CN206151739U (en) | Novel prevent sideslipping multi -functional nursing bed | |
| CN107080625A (en) | Infusion support wheelchair | |
| CN204864312U (en) | Transfusion chair with adjustable safety | |
| CN204766388U (en) | A multi -functional chair for activity of leaving bed of ICU patient | |
| CN110152101A (en) | A kind of paediatrics multifunction nursing transfusion chair | |
| US20200397635A1 (en) | Multipurpose person relocation device | |
| CN211186545U (en) | Multifunctional aisle chair | |
| CN213465673U (en) | Pediatric emergency treatment device | |
| CN208229056U (en) | A kind of safe wheelchair | |
| CN212880424U (en) | Safety seat for pediatric infusion | |
| CN219579264U (en) | Induction sickbed | |
| CN218869935U (en) | Adjustable nursing pillow that helps dormancy | |
| US11318057B1 (en) | Bed side support structure | |
| KR20200076459A (en) | wheelchair with bedsore monitoring apparatus | |
| CN213994447U (en) | Infusion chair suitable for nursing branch of academic or vocational study medical treatment | |
| CN209751309U (en) | Gastroenterology feed nursing device | |
| CN109091719A (en) | A kind of paediatrics special nursing chair | |
| CN211326257U (en) | Old person's nursing bed of posture is adjusted according to actual conditions |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220511 Address after: No. 28 Fuxing Road, Haidian District, Beijing 100089 Patentee after: CHINESE PLA GENERAL Hospital Address before: The third medical center of the General Hospital of the Chinese people's Liberation Army, No. 69 Yongding Road, Haidian District, Beijing 100089 Patentee before: Third Medical Center, General Hospital of the Chinese PLA |
|
| TR01 | Transfer of patent right |