Headstock special for airplane body position

By designing a special head frame for the airplane position suitable for infants and young children, the problem of existing head frames being unsuitable for infants and young children has been solved. It enables quick adjustment and stable connection, reduces the discomfort of children, and meets the needs of airplane position surgery.

CN224023855UActive Publication Date: 2026-03-24TONGJI HOSPITAL ATTACHED TO TONGJI MEDICAL COLLEGE HUAZHONG SCI TECH
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-03-27
Publication Date
2026-03-24

AI Technical Summary

Technical Problem

The existing head frame shape and size are not suitable for infants and young children, making the operation cumbersome and unstable during airplane-position surgery, and posing safety hazards.

Method used

A headrest specifically designed for aircraft positioning has been developed, comprising an adjustment rod, a bottom support, and a headrest assembly. The headrest can be flexibly adjusted and fixed through support screws and adjustment kits, and combined with a horseshoe-shaped gel pad to provide comfortable support.

Benefits of technology

It shortens the time for adjusting the body position, reduces the crying and struggling of the child, and provides good adjustability, stable connection and comfortable headrest design to meet the needs of children of different body types.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides a special airplane body position headstock, which comprises an adjusting rod, an adjusting rod, a fixing rod and a fixing rod, wherein the section of the adjusting rod is square; the bottom support comprises a support rod and a support screw, and the adjusting rod is movably connected to the support rod through the support screw; the head support assembly comprises a first head support and a second head support, the first head support is arranged on the adjusting rod in a sleeving mode and is close to one end of the adjusting rod, and the second head support is arranged on the adjusting rod in a sleeving mode and is close to the other end of the adjusting rod. The body position adjusting time can be greatly shortened, the special requirement of an operation is met, the operation risk is reduced, and the operation efficiency is improved.
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Description

TECHNICAL FIELD

[0001] The utility model relates to medical instrument technical field especially, it relates to a special head frame of aircraft body position. BACKGROUND

[0002] When operating the infant patient, the support head frame is often used, and the head frame aims at providing stable support for the head and face of the low age patient, and simultaneously exposing the forehead, the top of the skull and the occiput in all directions, especially being applicable to the whole skull suture reconstruction, so as to fully expose the operation field of view.

[0003] In the traditional operation, adopting the prone position or the prone position to carry out such operation has certain defects, and the forehead, the top of the skull and the occiput cannot be completely exposed. Therefore, on the basis of the traditional neurosurgery prone position, the head is tilted back, and the lower jaw and the cheek are placed on the head frame, and the aircraft body position is adopted, and the head can be tilted upwards, like the aircraft taking off, and the whole head can be exposed, so as to facilitate the doctor to complete the skull reconstruction. However, the shape and size of the existing head frame are not suitable for infants. In actual use, it is necessary to continuously fill the soft pad and the sponge to achieve the required angle and effect of the operation, which is not only complicated to operate, but also poor in stability. The use of the power system such as the milling cutter and the drill in the operation further increases the safety hazard to a certain extent.

[0004] How to provide a special head frame of aircraft body position is a technical problem to be solved by the person skilled in the art. UTILITY MODEL CONTENT

[0005] The technical problem to be solved by the utility model lies in overcoming the defects of the prior art, and providing a special head frame of aircraft body position.

[0006] In order to achieve the above purpose, the utility model adopts the following technical scheme: a special head frame of aircraft body position, comprising: an adjusting rod, the section of the adjusting rod is a square; a bottom support, the bottom support comprises a support rod and a support screw, the adjusting rod is movably connected on the support rod through the support screw; a head support assembly, the head support assembly comprises a first head support and a second head support, the first head support is sleeved on the adjusting rod and close to one end of the adjusting rod, and the second head support is sleeved on the adjusting rod and close to the other end of the adjusting rod.

[0007] Optionally, the special head frame of aircraft body position further comprises an adjusting kit, the adjusting kit comprises an adjusting ring and an adjusting bolt, the adjusting ring is fixedly connected on the operating bed, an adjusting hole is formed in the adjusting ring, and the adjusting bolt is threadedly connected with the adjusting hole.

[0008] Optionally, the first head holder comprises a first head pad, a first sliding block and a first fixing bolt, one side of the first sliding block is sleeved on the adjusting rod and close to one end of the adjusting rod, a first fixing hole is formed on the first sliding block, the first fixing bolt is threadedly connected with the first fixing hole, and the first head pad is arranged on the other side of the first sliding block.

[0009] Optionally, the first head holder further comprises a first horseshoe-shaped gel pad, and the first horseshoe-shaped gel pad is arranged on the first head pad.

[0010] Optionally, the second head holder comprises a second head pad, a second sliding block and a second fixing bolt, one side of the second sliding block is sleeved on the adjusting rod and close to the other end of the adjusting rod, a second fixing hole is formed on the second sliding block, the second fixing bolt is threadedly connected with the second fixing hole, and the second head pad is arranged on the other side of the second sliding block.

[0011] Optionally, the second head holder further comprises a second horseshoe-shaped gel pad, and the second horseshoe-shaped gel pad is arranged on the second head pad.

[0012] Optionally, limit blocks are arranged on both ends of the adjusting rod.

[0013] Optionally, limit blocks are arranged on both ends of the support rod.

[0014] Compared with the prior art, the head holder has the advantages that,

[0015] The application provides a head holder special for an aircraft body position, when the device is used, first, a support screw is threadedly connected with a threaded hole on an adjusting rod, then the adjusting rod is placed on a support rod, and then the support screw is threadedly connected with a threaded hole on the support rod, so that the adjusting rod is fixed on the support rod, when facing children with different body types, first and second head holders on both ends of the adjusting rod can be independently positioned and fixed when being adjusted to appropriate positions, and the head of the child is placed between the two head holders, and the adjustment is completed. The design of the device greatly shortens the body position adjustment time, reduces the crying and struggling of the child due to long-time keeping of an uncomfortable body position, and provides a special head holder with good adjustment performance, stable connection and comfortable head holder design for special requirements of an aircraft body position operation. BRIEF DESCRIPTION OF DRAWINGS

[0016] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiment description. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can also be obtained by those skilled in the art without any creative effort.

[0017] Legend:

[0018] Fig. 1 It is the main body structure schematic diagram of the utility model;

[0019] Fig. 2 It is the structure schematic diagram of head support assembly;

[0020] Fig. 3 It is the structure schematic diagram of adjusting sleeve;

[0021] In the figure: 1, adjusting rod; 2, bottom support; 21, support rod; 22, support screw; 3, head support assembly; 31, first head support; 311, first head pad; 312, first sliding block; 313, first fixed bolt; 32, second head support; 321, second head pad; 322, second sliding block; 323, second fixed bolt; 4, adjusting sleeve; 41, adjusting ring; 42, adjusting bolt. DETAILED DESCRIPTION

[0022] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the utility model.

[0023] It will be understood that, although the terms "first", "second", "third", "fourth" and the like can be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another.

[0024] Embodiment one

[0025] Combined Figs. 1-3 As shown in the figure, the utility model discloses a special head frame for aircraft body position, a special head frame for aircraft body position, comprising: adjusting rod 1, the section of adjusting rod 1 is square;Bottom support 2, the bottom support 2 includes support rod 21 and support screw 22, adjusting rod 1 is movably connected on support rod 21 through support screw 22;Head support assembly 3, the head support assembly 3 includes first head support 31 and second head support 32, the first head support 31 is set on adjusting rod 1 and is close to one end of adjusting rod 1, and the second head support 32 is set on adjusting rod 1 and is close to the other end of adjusting rod 1.

[0026] Specifically, the application provides a head support special for aircraft position, when using the device, first, the support screw 22 is screwed with the threaded hole on the adjusting rod 1, then the adjusting rod 1 is placed on the support rod 21, and then the support screw 22 is screwed with the threaded hole on the support rod 21, so that the adjusting rod 1 is fixed on the support rod 21, when facing children with different body types, the first head support 31 and the second head support 32 on both ends of the adjusting rod 1 can be independently positioned and fixed, and the head of the child is placed between the two head supports, and the adjustment action is completed. The design of the device greatly shortens the position adjustment time, reduces the crying and struggling of the child due to long-time maintaining of an uncomfortable position, and provides a special head support with good adjustment performance, stable connection and comfortable head support design for the special needs of aircraft position surgery.

[0027] In some possible implementation ways, the aircraft position special head support further comprises an adjusting kit 4, the adjusting kit 4 comprises an adjusting ring 41 and an adjusting bolt 42, the adjusting ring 41 is fixedly connected to the operating bed, the adjusting ring 41 is provided with an adjusting hole, and the adjusting bolt 42 is screwed with the adjusting hole.

[0028] Specifically, by rotating the adjusting bolt 42, the relative position and angle between the adjusting rod 1 and the operating bed can be flexibly changed. When the height of the head of the patient needs to be adjusted, the adjusting bolt 42 is loosened, the adjusting rod 1 is moved up and down to the appropriate position, and then the adjusting bolt 42 is tightened, so that the height of the head support is adjusted, and the diversified needs of different surgeries are ensured.

[0029] In some possible implementation ways, the first head support 31 comprises a first head pad 311, a first sliding block 312 and a first fixing bolt 313, one side of the first sliding block 312 is sleeved on the adjusting rod 1 and close to one end of the adjusting rod 1, the first sliding block 312 is provided with a first fixing hole, the first fixing bolt 313 is screwed with the first fixing hole, and the first head pad 311 is arranged on the other side of the first sliding block 312. The first head support 31 further comprises a first horseshoe-shaped gel pad, and the first horseshoe-shaped gel pad is arranged on the first head pad 311.

[0030] Specifically, the first slider 312 can slide freely along the adjusting rod 1, and when facing children of different sizes, the first slider 312 is slid to a suitable position according to the position requirement of the head of the child. Then, the first fixing bolt 313 is screwed into the first fixing hole, and by tightening the first fixing bolt 313, the first slider 312 is stably fixed on the adjusting rod 1 by the friction between the bolt and the fixing hole. The first horseshoe-shaped gel pad arranged on the first head pad 311 can better disperse the pressure on one side of the head of the child and reduce the discomfort of the head of the child during a long surgery process due to its special shape and soft gel material.

[0031] In some possible implementations, the second head support 32 includes a second head pad 321, a second slider 322, and a second fixing bolt 323. One side of the second slider 322 is sleeved on the adjusting rod 1 and close to the other end of the adjusting rod 1. A second fixing hole is formed in the second slider 322, and the second fixing bolt 323 is threadedly connected with the second fixing hole. The second head pad 321 is arranged on the other side of the second slider 322. The second head support 32 further includes a second horseshoe-shaped gel pad arranged on the second head pad 321.

[0032] Specifically, similar to the first head support 31, the second slider 322 can slide on the adjusting rod 1, and its function is to flexibly adjust according to the position requirement of the other side of the head of the child. After being slid to a suitable position, the second fixing bolt 323 is screwed into the second fixing hole and tightened to fix the second slider 322. At this time, the first head support 31 and the second head support 32 together provide an area for placing the head of the child, and in cooperation with the first head support 31, they jointly provide comprehensive, comfortable, and stable support for the head of the child. The second horseshoe-shaped gel pad arranged on the second head pad 321 can better disperse the pressure on one side of the head of the child and reduce the discomfort of the head of the child during a long surgery process.

[0033] In some possible implementations, limit blocks are arranged on both ends of the adjusting rod 1, and limit blocks are arranged on both ends of the support rod 21.

[0034] Specifically, the limit blocks on both ends of the adjusting rod 1 can effectively prevent the first head support 31 and the second head support 32 from being separated from the adjusting rod 1 during sliding. When the first head support 31 or the second head support 32 is slid to the limit position on the adjusting rod 1, the limit blocks will prevent it from continuing to slide. The limit blocks on both ends of the support rod 21 limit the movement range of the support rod 21 so that it will not fall off the adjusting ring 41.

[0035] Finally, it should be noted that the above examples are merely specific embodiments of the present application, and are used to illustrate the technical solutions of the present application, but not to limit the present application. The protection scope of the present application is not limited to this. Although the present application has been described in detail with reference to the foregoing examples, those skilled in the art should understand that any person skilled in the art can modify or easily think of changes to the technical solutions recorded in the foregoing examples, or make equivalent replacements to some of the technical features within the technical range disclosed by the present application. These modifications, changes or replacements do not cause the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of the present application. All should be covered within the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.

[0036] Although the embodiments of the present application have been disclosed as above, they are not limited to the applications listed in the specification and the embodiments, and can be fully applied to various fields suitable for the present application. Those skilled in the art can easily make further modifications, and therefore the present application is not limited to specific details and the figures shown and described herein, without departing from the general concept defined by the claims and the equivalent scope.

Claims

1. A special headframe for aircraft positioning, characterized in that, include: Adjusting rod (1), the cross-section of which is square; The bottom support (2) includes a support rod (21) and a support screw (22), and the adjusting rod (1) is movably connected to the support rod (21) through the support screw (22); The headrest assembly (3) includes a first headrest (31) and a second headrest (32). The first headrest (31) is sleeved on the adjusting rod (1) and close to one end of the adjusting rod (1). The second headrest (32) is sleeved on the adjusting rod (1) and close to the other end of the adjusting rod (1).

2. The aircraft headframe for specific body positioning according to claim 1, characterized in that, The aircraft positioning head frame also includes an adjustment kit (4), which includes an adjustment ring (41) and an adjustment bolt (42). The adjustment ring (41) is fixedly connected to the operating table, and an adjustment hole is provided on the adjustment ring (41). The adjustment bolt (42) is threadedly connected to the adjustment hole.

3. The aircraft headframe for specific body positioning according to claim 2, characterized in that, The first head support (31) includes a first head pad (311), a first slider (312) and a first fixing bolt (313). One side of the first slider (312) is fitted onto the adjusting rod (1) and close to one end of the adjusting rod (1). A first fixing hole is provided on the first slider (312). The first fixing bolt (313) is threadedly connected to the first fixing hole. The first head pad (311) is disposed on the other side of the first slider (312).

4. The aircraft headrest according to claim 3, characterized in that, The first headrest (31) also includes a first horseshoe-shaped gel pad, which is disposed on the first headrest (311).

5. The aircraft headrest according to claim 4, characterized in that, The second head support (32) includes a second head pad (321), a second slider (322), and a second fixing bolt (323). One side of the second slider (322) is fitted onto the adjusting rod (1) and close to the other end of the adjusting rod (1). A second fixing hole is provided on the second slider (322). The second fixing bolt (323) is threadedly connected to the second fixing hole. The second head pad (321) is disposed on the other side of the second slider (322).

6. The aircraft headframe for specific body positioning according to claim 5, characterized in that, The second headrest (32) also includes a second horseshoe-shaped gel pad, which is disposed on the second headrest (321).

7. The aircraft headframe for specific body positioning according to claim 6, characterized in that, Limiting blocks are provided on both ends of the adjusting rod (1).

8. The aircraft headframe for specific body positioning according to claim 7, characterized in that, Limiting blocks are provided at both ends of the support rod (21).