CN216908367U - Detachable stretcher special for helicopter - Google Patents

Detachable stretcher special for helicopter Download PDF

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Publication number
CN216908367U
CN216908367U CN202220588562.2U CN202220588562U CN216908367U CN 216908367 U CN216908367 U CN 216908367U CN 202220588562 U CN202220588562 U CN 202220588562U CN 216908367 U CN216908367 U CN 216908367U
Authority
CN
China
Prior art keywords
helicopter
special
detachable
bottom plate
end inside
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN202220588562.2U
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Chinese (zh)
Inventor
王倩梅
赵威
李俊杰
尹文
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Air Force Medical University of PLA
Original Assignee
Air Force Medical University of PLA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Air Force Medical University of PLA filed Critical Air Force Medical University of PLA
Priority to CN202220588562.2U priority Critical patent/CN216908367U/en
Application granted granted Critical
Publication of CN216908367U publication Critical patent/CN216908367U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a detachable stretcher special for a helicopter, which comprises a bottom plate, wherein jacks are integrally arranged at four corners of the upper end inside the bottom plate, the jacks are through holes, the bottom plate is movably provided with a placing frame inside, the middle side of the lower end inside the placing frame is rotatably provided with a driving mechanism, the four corners of the lower end in the placing rack are movably provided with a moving mechanism, the middle ends of the left side and the right side of the outer wall of the placing rack are fixedly provided with an anti-deviation mechanism, the front side and the rear side of the upper end in the placing rack are integrally provided with abdicating holes which are through holes, the detachable stretcher special for the helicopter can stably connect the stretcher and the helicopter so as to avoid the position deviation of the stretcher in the helicopter, the device still can be convenient and fast with the helicopter separation, from this can know, through using the device in this application, has eliminated the incident of potential safety hazard and has taken place.

Description

Detachable stretcher special for helicopter
Technical Field
The utility model relates to the technical field of stretchers, in particular to a detachable stretcher special for a helicopter.
Background
The rescue helicopter is applied to emergency rescue (120 in the air), can quickly reach the inaccessible operation site of water and land, carries out the work of search rescue, material transportation, air command and the like, and is the most effective emergency rescue commonly adopted in many countries in the world.
The stretcher is one of necessary apparatus for rescuing the helicopter, at present, the traditional stretcher is directly placed in the helicopter, the stretcher cannot be stably connected with the helicopter, so that the position of the stretcher can deviate in the helicopter in the transportation process of the helicopter, and the potential safety hazard is easy to occur.
SUMMERY OF THE UTILITY MODEL
The technical problem to be solved by the utility model is as follows: provides a detachable stretcher special for a helicopter, which solves the problems provided by the background technology.
In order to solve the technical problems, the technical scheme of the utility model is as follows: the detachable stretcher special for the helicopter comprises a base plate, jacks are integrally arranged at four corners of the upper end inside the base plate, the jacks are through holes, a placing rack is movably arranged inside the base plate, a driving mechanism is arranged at the middle side of the lower end inside the placing rack in a rotating mode, a moving mechanism is movably arranged at four corners of the lower end inside the placing rack, an anti-deviation mechanism is fixedly arranged at the middle ends of the left side and the right side of the outer wall of the placing rack, a abdicating hole is integrally formed in the front side and the rear side of the upper end inside the placing rack, and the abdicating hole is a through hole.
Furthermore, the driving mechanism consists of a rotating rod and a conical sleeve.
Further, the lower end in the placing frame is rotatably provided with a rotating rod, a conical sleeve is sleeved at the front end and the rear end of the outer portion of the rotating rod in a threaded mode, and the conical sleeve is connected with the placing frame in a sliding mode.
Furthermore, the conical sleeve at the front end is connected with the left thread of the rotating rod, and the conical sleeve at the rear end is connected with the right thread of the rotating rod.
Furthermore, the moving mechanism consists of a bolt, a spring and a wedge-shaped block.
Furthermore, the four corners of the lower end inside the placing rack are provided with bolts in a sliding mode, and springs are fixedly arranged at the upper end and the lower end of each bolt.
Further, the other end of the spring is fixedly connected with the placing frame, and a wedge-shaped block is fixedly arranged on the inner side of the bolt.
Furthermore, the deviation prevention mechanism consists of an alignment block and a mounting groove.
Further, rack outer wall left and right sides middle-end set firmly and aim at the piece, aim at the piece lower extreme and be equipped with the mounting groove, the mounting groove link to each other with the bottom plate is integrative.
Compared with the prior art, this special stretcher of reassembling type helicopter can stabilize the stretcher and be connected with the helicopter to this avoids the stretcher position skew to appear in the helicopter, and in addition, the device still can be convenient separates with the helicopter, can know from this, through using the device in this application, has eliminated the incident of potential safety hazard and has taken place.
Drawings
Fig. 1 is a front sectional view of a detachable helicopter special stretcher;
figure 2 is an internal cross-sectional view of the rack;
fig. 3 is a top view of a detachable helicopter specific stretcher;
figure 4 is a front view of the rack.
The device comprises a bottom plate 1, a jack 2, a placing frame 3, a driving mechanism 4, a moving mechanism 5, an anti-deviation mechanism 6, a yielding hole 7, a rotating rod 8, a conical sleeve 9, a plug pin 10, a spring 11, a wedge block 12, an alignment block 13 and a mounting groove 14.
The following detailed description will be further described in conjunction with the above-identified drawings.
Detailed Description
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the concepts underlying the described embodiments. It will be apparent, however, to one skilled in the art, that the described embodiments may be practiced without some or all of these specific details. In other instances, well known process steps have not been described in detail.
Example 1
As shown in fig. 1 and 4, the detachable stretcher special for helicopters comprises a base plate 1, four corners of the upper end inside the base plate 1 are integrally provided with jacks 2, the jacks 2 are through holes, a placing frame 3 is movably arranged inside the base plate 1, a driving mechanism 4 is rotatably arranged at the middle side of the lower end inside the placing frame 3, a moving mechanism 5 is movably arranged at the four corners of the lower end inside the placing frame 3, an anti-deviation mechanism 6 is fixedly arranged at the middle ends of the left side and the right side of the outer wall of the placing frame 3, two sides of the upper end inside the placing frame 3 are integrally provided with a yielding hole 7, and the yielding hole 7 is a through hole.
This special stretcher of reassembling type helicopter, at first bottom plate 1 is connected with the helicopter is firm, the patient is in rack 3, first-aid staff places rack 3 in bottom plate 1 together with the patient, effect through skew mechanism 6, the accuracy of moving mechanism 5 and jack 2 coincidence each other has been ensured, first-aid staff passes through the use to actuating mechanism 4 again, insert in jack 2 with moving mechanism 5, and then it is firm to be connected rack 3 with bottom plate 1, after finishing using, again through the use to actuating mechanism 4, separate moving mechanism 5 and jack 2, first-aid staff transports rack 3 to the first aid region together with the patient again can.
Example 2
As shown in figures 1, 2, 3 and 4, the detachable stretcher special for the helicopter comprises a bottom plate 1, jacks 2 are integrally arranged at four corners of the upper end inside the bottom plate 1, the jacks 2 are through holes, a placing frame 3 is movably arranged inside the bottom plate 1, a driving mechanism 4 is rotatably arranged at the middle side of the lower end inside the placing frame 3, moving mechanisms 5 are movably arranged at four corners of the lower end inside the placing frame 3, deviation prevention mechanisms 6 are fixedly arranged at the middle ends of the left side and the right side of the outer wall of the placing frame 3, abdicating holes 7 are integrally arranged at the front side and the rear side of the upper end inside the placing frame 3, the abdicating holes 7 are through holes, the driving mechanism 4 consists of a rotating rod 8 and a conical sleeve 9, a rotating rod 8 is rotatably arranged at the lower end inside the placing frame 3, conical sleeves 9 are threaded at the front end and the rear end outside the rotating rod 8, and the conical sleeve 9 is slidably connected with the placing frame 3, front end the toper cover 9 and 8 left hand threaded connection of bull stick, the rear end toper cover 9 and 8 right hand threaded connection of bull stick, moving mechanism 5 constitute by bolt 10, spring 11 and wedge 12, 3 inside lower extreme four corners departments of rack slide and be equipped with bolt 10, bolt 10 about both ends have set firmly spring 11, the spring 11 other end and 3 fixed connection of rack, 10 inboards of bolt have set firmly wedge 12, prevent inclined to one side mechanism 6 by aiming at piece 13 and mounting groove 14 and form, 3 outer wall left and right sides middle-ends of rack set firmly aim at piece 13, aim at piece 13 lower extreme and be equipped with mounting groove 14, mounting groove 14 link to each other with 1 an organic whole of bottom plate.
Before the detachable stretcher special for the helicopter is used, firstly, the base plate 1 and the inner plane of the helicopter are in a stable connection state, when the detachable stretcher is used, first-aid workers firstly move patients into the placing frame 3, then pass hands through the abdicating hole 7 and then hold the edge of the placing frame 3, so that the placing frame and the patients are moved into the helicopter, namely, the placing frame 3 is moved into the base plate 1, the aligning block 13 and the mounting groove 14 are mutually overlapped, at the moment, the bolt 10 and the jack 2 are mutually overlapped, the first-aid workers use the hand forward rotating rod 8, under the action of the thread transmission of the rotating rod 8 and the conical sleeve 9, the conical sleeves 9 with two numbers are back to back, further, the conical sleeve 9 extrudes the wedge 12 to drive the bolt 10 to move out of the placing frame 3, namely, the bolt 10 is inserted into the jack 2, and synchronously, the spring 11 is deformed, and by the mode, the placing frame 3 and the helicopter are quickly and conveniently connected into a whole, the helicopter transports the device again and shifts together with the patient, shifts the back that finishes, and first-aid staff reuse hand reversal bull stick 8, its operating mode and the aforesaid vice versa, and tapered sleeve 9 moves in opposite directions promptly, and at this moment, tapered sleeve 9 is eliminated the extrusion force of wedge 12, through the effect of spring 11 resilience power for bolt 10 breaks away from jack 2, and the connected state of rack 3 and helicopter is relieved promptly, and first-aid staff holds the edge of hole 7 of stepping down again, with rack 3 together with the patient transportation to first aid region can.

Claims (9)

1. The detachable stretcher special for the helicopter is characterized by comprising a bottom plate, jacks are integrally arranged at four corners of the upper end inside the bottom plate, the jacks are through holes, a placing rack is movably arranged inside the bottom plate, a driving mechanism is arranged at the middle side of the lower end inside the placing rack in a rotating mode, a moving mechanism is movably arranged at four corners of the lower end inside the placing rack, an anti-deviation mechanism is fixedly arranged at the middle ends of the left side and the right side of the outer wall of the placing rack, and abdicating holes are integrally formed in the front side and the rear side of the upper end inside the placing rack and are through holes.
2. The detachable stretcher special for helicopter of claim 1, wherein the driving mechanism is composed of a rotating rod and a conical sleeve.
3. The detachable stretcher special for helicopters according to claim 1, wherein a rotating rod is rotatably arranged at the lower end inside the placing frame, tapered sleeves are respectively sleeved at the front end and the rear end of the outside of the rotating rod through threads, and the tapered sleeves are slidably connected with the placing frame.
4. The detachable stretcher special for a helicopter according to claim 3, wherein the tapered sleeve at the front end is connected with the rotating rod by left threads, and the tapered sleeve at the rear end is connected with the rotating rod by right threads.
5. The detachable stretcher special for helicopter of claim 1, wherein the moving mechanism is composed of a bolt, a spring and a wedge-shaped block.
6. The detachable stretcher special for a helicopter according to claim 1, wherein four corners of the lower end inside the placing frame are slidably provided with pins, and springs are fixedly arranged at the upper and lower ends of each pin.
7. The detachable stretcher special for a helicopter of claim 5, wherein the other end of the spring is fixedly connected with the placing rack, and the wedge-shaped block is fixedly arranged on the inner side of the plug.
8. The detachable helicopter special stretcher according to claim 1, characterized in that the deviation prevention mechanism is composed of an alignment block and an installation groove.
9. The detachable stretcher special for a helicopter according to claim 1, wherein the aligning blocks are fixedly arranged at the middle ends of the left and right sides of the outer wall of the placing frame, the lower ends of the aligning blocks are provided with mounting grooves, and the mounting grooves are integrally connected with the bottom plate.
CN202220588562.2U 2022-03-17 2022-03-17 Detachable stretcher special for helicopter Expired - Fee Related CN216908367U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220588562.2U CN216908367U (en) 2022-03-17 2022-03-17 Detachable stretcher special for helicopter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220588562.2U CN216908367U (en) 2022-03-17 2022-03-17 Detachable stretcher special for helicopter

Publications (1)

Publication Number Publication Date
CN216908367U true CN216908367U (en) 2022-07-08

Family

ID=82227984

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220588562.2U Expired - Fee Related CN216908367U (en) 2022-03-17 2022-03-17 Detachable stretcher special for helicopter

Country Status (1)

Country Link
CN (1) CN216908367U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114642543A (en) * 2022-03-17 2022-06-21 中国人民解放军空军军医大学 Detachable stretcher special for helicopter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114642543A (en) * 2022-03-17 2022-06-21 中国人民解放军空军军医大学 Detachable stretcher special for helicopter

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20220708