CN109436333A - It is mounted on the stretcher station on aircarrier aircraft - Google Patents
It is mounted on the stretcher station on aircarrier aircraft Download PDFInfo
- Publication number
- CN109436333A CN109436333A CN201811349382.3A CN201811349382A CN109436333A CN 109436333 A CN109436333 A CN 109436333A CN 201811349382 A CN201811349382 A CN 201811349382A CN 109436333 A CN109436333 A CN 109436333A
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- CN
- China
- Prior art keywords
- dovetail groove
- pin
- stretcher
- ejector pin
- aircarrier aircraft
- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Abstract
The present invention relates to a kind of stretcher stations being mounted on aircarrier aircraft, including at least one layer of stretcher, each stretcher is mounted on from beginning to end on two support arms, ipsilateral support arm is height-adjustable to be mounted on the same column, by being connected by the fixed support rod of lock after retractable and flexible between two columns, column is fixed on the base, pedestal is respectively provided on adjacent two across aircarrier aircraft sliding rail by two adjustment seats, pedestal is equipped with locating slot, it is equipped with the upper dovetail groove being slidably matched with base bottom at the top of adjustment seat and is able to cooperate the ejector pin for being caught in locating slot and being capable of resetting, bottom, which is equipped with the sliding block being slidably matched with the lower dovetail groove of aircarrier aircraft sliding rail and is able to cooperate the circular hole position being caught on lower dovetail groove and the bottom being capable of resetting, sells, the arrangement of locating slot guarantees that two adjustment seats on pedestal adapt to the span of aircarrier aircraft sliding rail.Stretcher station handling are quick and convenient, and versatility is good, can more transport the wounded.
Description
Technical field
The present invention relates to a kind of stretcher stations, and in particular to a kind of stretcher station being mounted on aircarrier aircraft.
Background technique
In war or non-war, them are given treatment in time using the aircarrier aircraft shipping bulk amount wounded and very must
It wants, is also of great significance to the emergency system construction of country.Currently, the vehicle equipment institute of domestic and international existing AIRLINE & AIRPORT machine
Rescue stretcher station is less, and a general stretcher station can only lie down a people, rescue when for passenger's burst disease, cannot be compared with
It is large batch of to be used to transport the wounded.When needing the aircarrier aircraft bulk transport wounded, it is necessary first to be reorganized and outfit to aircraft, usually
In the case of, it is desirable that it answers simple and fast to reorganizing and outfit for aircraft, due to the particularity of AIRLINE & AIRPORT, has sternly to any change of aircraft
The examination and approval procedures of lattice and requirement, therefore, the content reorganized and outfit are as few as possible, this, which just needs to design a kind of stretcher station, both may be implemented
Fast Installation and disassembly can carry the more sick and wounded again on common aircarrier aircraft sliding rail.
As shown in Figure 1, common aircarrier aircraft slide rail body is dovetail groove, circle is equipped with along dovetail groove top opening two sides
Arc notch, two arc gaps of face form circular hole position, are straight line position between two adjacent arc gaps.
Summary of the invention
The object of the present invention is to provide a kind of stretcher station being mounted on aircarrier aircraft, stretcher station handling are quick and convenient,
Versatility is good, can more transport the wounded.
The technical scheme adopted by the invention is that:
A kind of stretcher station being mounted on aircarrier aircraft, including at least one layer of stretcher, each stretcher are mounted on two from beginning to end
On a support arm, ipsilateral support arm is height-adjustable to be mounted on the same column, is passed through retractable between two columns and is stretched
It is connected after contracting by the fixed support rod of lock, column is fixed on the base, and pedestal is respectively provided at adjacent two by two adjustment seats
On across aircarrier aircraft sliding rail, pedestal is equipped with locating slot, is equipped with the upper dovetail groove being slidably matched with base bottom at the top of adjustment seat
And be able to cooperate the ejector pin for being caught in locating slot and being capable of resetting, bottom is equipped with and is slidably matched with the lower dovetail groove of aircarrier aircraft sliding rail
Sliding block and the bottom pin for being able to cooperate the circular hole position being caught on lower dovetail groove and being capable of resetting, the arrangement of locating slot guarantee on pedestal
Two adjustment seats adapt to the span of aircarrier aircraft sliding rail.
Further, locating slot is located at base edge, and base edge cooperates in upper dovetail groove, and ejector pin is located at upper dovetail groove
It is interior and can with locating slot cooperate side be inside, outside upper dovetail groove and expose adjustment seat outer surface of cupular part it is another
Side is outside, and ejector pin bottom is always by ejector pin spring top clamping, and when ejector pin inside cooperates with open slot, ejector pin inside top is against
On dovetail groove, hereafter, upper dovetail groove or less can will be brought on the inside of ejector pin when pressing on the outside of ejector pin.
Further, adjustment seat bottom surface is equipped with knock hole, top surface is equipped with ejector pin handle hole, and dovetail is protruded into knock hole side
In slot, the other side and ejector pin handle hole penetrate through, ejector pin outside top is located at that ejector pin handle hole is interior, rest part is located at knock hole
Interior, knock hole bottom opening is capped closing, and ejector pin Spring Card is between ejector pin and capping.
Further, an adjustment seat is fixed there are two sliding block, and a sliding block is fixed sliding block, another sliding block is that can rise
The floating slider of drop, fixed sliding block and floating slider are located at the two sides of bottom pin, and fixed sliding block and floating slider are directed at lower swallow
Lower dovetail groove and the cooperation of lower dovetail groove can be protruded into when circular hole position on stern notch simultaneously and floating slider can be under by lifting
Dovetail groove generates gap, cannot be de- from lower dovetail groove when the circular hole position on fixed sliding block and floating slider and lower dovetail groove is staggered
Out, the circular hole portion when circular hole position that pin cooperation in bottom is caught on lower dovetail groove, on fixed sliding block and floating slider and lower dovetail groove
Dislocation is opened.
Further, floating slider cooperation is in floating slider hole and top and bottom end are all exposed, floating slider top hinge
It is connected to thrust handle, the side of the hinge joint of thrust handle is bent into arc-shaped, and the extrados of arc-shaped is pressed in adjustment seat.
Further, bottom, which is sold, is cased with bottom pin spring, and under original state, bottom sells spring compression bottom pin and is in extended position,
Bottom pin top is connected with carrying handle, and carrying handle is exposed at outside the top of adjusting seat, when lifting carrying handle, bottom pin retract and
It compresses bottom and sells spring.
Further, adjustment seat bottom surface is equipped with bottom pin hole, top surface is equipped with carrying handle slot, and bottom pin hole and carrying handle slot are logical
The connecting hole connection for being narrower than bottom pin hole is crossed, bottom pin lower part is wide portion and is narrow portion with the cooperation of bottom pin hole, top and is cased with bottom pin bullet
Spring Card is sold between bottom pin hole inner face and width portion in spring, bottom, and carrying handle a part is connect with narrow portion, and another part, which is located at, to be mentioned
It draws in handle groove and connecting hole cannot be protruded into.
Further, support rod includes horizontal support rod and tilting support rod, the side that support rod is socketed by multistage
Formula realizes flexible and realizes multiposition locking by multiple jacks and Quick-release pin cooperation, the both ends of support rod respectively with two columns
Hingedly.
Further, stretcher tail portion is equipped with two-point belt restraint system, stem equipped with four point seat belt constraint system
It unites and stem can be lifted up certain angle.
Further, column is equipped with several waist type grooves, and support arm is mounted in waist type groove, the waist of support arm and different location
Type groove cooperation realize height it is adjustable, so as to adjust stretcher layer away from.
The beneficial effects of the present invention are:
Stretcher station handling are quick and convenient, and versatility is good --- and adjustment seat is moved along the cooperation of lower dovetail groove between capable of adjusting column
Away from and position, and bottom lock is fixed quick and convenient, and adjustment seat is moved along pedestal adapts to aircarrier aircraft sliding rail span, versatility
It is good, and ejector pin locking is quick and convenient, and support rod is flexible with the change of column spacing, and lock is fixed quick and convenient；The load
Frame station can more transport the wounded --- and stretcher is arranged by support arm along column, and multiple stretchers can be set, and current civil aviaton flies
Machine, such as B737-200, A320, it is contemplated that luggage compartment is closer apart from airplane floor, therefore arranges that two layers of stretcher is relatively rationally, most
It can mostly arrange three layers of stretcher, and support arm is height-adjustable is mounted on column, phase stretcher spacing can be adjusted, certainly with not
The increase for carrying out aircarrier aircraft size has an opportunity that four layers of stretcher are arranged, even more.
Detailed description of the invention
Fig. 1 is the schematic diagram of aircarrier aircraft sliding rail (the present embodiment is using sliding rail made in Great Britain).
Fig. 2 is the schematic diagram that the embodiment of the present invention is mounted on aircarrier aircraft.
Fig. 3 is the schematic diagram of the embodiment of the present invention.
Fig. 4 is the structural schematic diagram of adjustment seat in the embodiment of the present invention.
Fig. 5 is the stereogram exploded view of adjustment seat in the embodiment of the present invention.
Fig. 6 is the perspective view of the ontology of adjustment seat in the embodiment of the present invention.
Fig. 7 is the connection schematic diagram of adjustment seat and pedestal in the embodiment of the present invention.
In figure: dovetail groove under 1-；2- thrust handle；3- fixes sliding block；4- floating slider；5- tabletting；The bottom 6- pin；7- lifting
Handle；8- ejector pin；9- capping；10- nylon spacer；Sell spring in the bottom 11-；12- sunk screw；13- cover type nut；14- stretcher；
15- articulated shaft；16- adjustment seat；17- pedestal；18- column；19- support arm；20- two-point belt restraint system；21- four-point
Safety belt restraining system；22- Transfusion hanging stand；23- support rod；The upper dovetail groove of 24-；25- locating slot；26- knock hole；27- ejector pin
Handle hole；28- connecting hole；29- carrying handle slot；30- ejector pin spring.
Specific embodiment
The present invention is further illustrated with reference to the accompanying drawings and examples.
As shown in Figures 2 to 7, a kind of 14 station of stretcher being mounted on aircarrier aircraft, including at least one layer of stretcher 14, each
Stretcher 14 is all mounted on from beginning to end on two support arms 19, and ipsilateral support arm 19 is height-adjustable to be mounted on the same column 18
(18 top of column is removably equipped with Transfusion hanging stand 22), by fixed by lock after retractable and flexible between two columns 18
Support rod 23 connect, column 18 is fixed on pedestal 17 that (column 18 and pedestal 17 are main bearing members, and column 18 uses
" day " font opening profile, pedestal 17 use I-shaped cross section, and pedestal 17 is connect with column 18 by bolt and nut), pedestal
17 are respectively provided on adjacent two across aircarrier aircraft sliding rail by two adjustment seats 16, and pedestal 17 is equipped with locating slot 25, adjustment seat
16 tops are equipped with the upper dovetail groove 24 cooperated with 17 basal sliding of pedestal and are able to cooperate the top for being caught in locating slot 25 and being capable of resetting
Pin 8, bottom are equipped with the sliding block being slidably matched with the lower dovetail groove 1 of aircarrier aircraft sliding rail and are able to cooperate and be caught on lower dovetail groove 1
Circular hole position and the bottom pin 6 that is capable of resetting, the arrangement of locating slot 25 guarantee that two adjustment seats 16 on pedestal 17 adapt to civil aviaton
The span of aircraft sliding rail.14 station of stretcher handling are quick and convenient, and versatility is good --- and adjustment seat 16 is moved along the cooperation of lower dovetail groove 1
18 spacing of column and position can be adjusted, and bottom pin 6 locks quick and convenient, adjustment seat 16 is moved along pedestal 17 to be adapted to civil aviaton and fly
Machine sliding rail span, versatility is good, and ejector pin 8 locks quick and convenient, and support rod 23 is flexible with the change of 18 spacing of column, and
And lock is fixed quick and convenient；14 station of stretcher can more transport the wounded --- and stretcher 14 is arranged by support arm 19 along column 18,
Multiple stretchers 14, current aircarrier aircraft, such as B737-200, A320 can be set, it is contemplated that luggage compartment is apart from airplane floor
It is relatively close, therefore arrange that two layers of stretcher 14 is that relatively rationally, can at most arrange three layers of stretcher 14, and the height-adjustable peace of support arm 19
On column 18,14 spacing of phase stretcher can be adjusted, certainly with the increase of the following aircarrier aircraft size, have an opportunity four layers of setting
Stretcher 14, it is even more.
As shown in Figures 4 to 7, in the present embodiment, locating slot 25 is located at 17 edge of pedestal, and 17 edge mate of pedestal is upper
In dovetail groove 24, ejector pin 8 is located at side that is in upper dovetail groove 24 and can cooperating with locating slot 25 and is inside, is located at upper dovetail groove
The other side that is outside 24 and exposing 16 outer surface of cupular part of adjustment seat is outside, and 8 bottom of ejector pin is held out against by ejector pin spring 30 always, is pushed up
When the inside of pin 8 cooperates with open slot, 8 inside top of ejector pin is against on dovetail groove 24, hereafter, when pressing 8 outside of ejector pin can will
Bring 24 or less dovetail groove on the inside of ejector pin 8 into.The setting structure of ejector pin 8 and locating slot 25 is compact, and adjustment seat 16 is sliding along pedestal 17
When moving locating slot 25, ejector pin 8 ejects naturally under the effect of ejector pin spring 30, and lock is realized with the cooperation of locating slot 25 in 8 inside of ejector pin
It is fixed, 8 outside of ejector pin is hereafter pressed, will bring upper 24 or less dovetail groove on the inside of ejector pin 8 into can be realized unlock.
As shown in Figures 4 to 7, in the present embodiment, 16 bottom surface of adjustment seat is equipped with knock hole 26, top surface is operated equipped with ejector pin
Hole 27,26 side of knock hole is protruded into dovetail groove 24, the other side and ejector pin handle hole 27 penetrate through, and 8 outside top of ejector pin is located at
Ejector pin handle hole 27 is interior, rest part is located in knock hole 26, and 26 bottom opening of knock hole is capped 9 closings, ejector pin spring 30
It is stuck between ejector pin 8 and capping 9.The structure facilitates processing and fabricating and installation, it is therefore prevented that ejector pin 8 is deviate from.
As shown in Figures 4 to 6, in the present embodiment, an adjustment seat 16 (passing through counterbore land) is fixed there are two sliding block,
One sliding block is fixed sliding block 3, another sliding block is the floating slider 4 that can be gone up and down, and fixed sliding block 3 and floating slider 4 distinguish position
In the two sides of bottom pin 6, lower dovetail can be protruded into simultaneously when fixing the circular hole position that sliding block 3 and floating slider 4 are aligned on lower dovetail groove 1
Slot 1 and the cooperation of lower dovetail groove 1 and floating slider 4 pass through lifting can generate gap, fixed sliding block 3 and floating with lower dovetail groove 1
Circular hole position on sliding block 4 and lower dovetail groove 1 cannot deviate from when being staggered from lower dovetail groove 1, and the cooperation of bottom pin 6 is caught in lower dovetail groove 1
On circular hole position when, fixed sliding block 3 and floating slider 4 are staggered with the circular hole position on lower dovetail groove 1.It fixes sliding block 3 and floats
Movable slider 4 is located at the two sides of bottom pin 6, and anticreep effect is more preferable when locking, unilateral stress is avoided, since floating slider 4 is logical
Gap can be generated with lower dovetail groove 1 by crossing lifting, can will be on floating slider 4 therefore when adjustment seat 16 is slided along lower dovetail groove 1
Rise, such conveniently moving, avoid cooperation it is too close, be easy to block.
As shown in Figures 4 to 6, in the present embodiment, the cooperation of floating slider 4 is in 4 hole of floating slider and top and bottom end
It is all exposed, 4 top of floating slider is hinged with thrust handle 2, and the side of the hinge joint of thrust handle 2 is bent into arc-shaped, circular arc
The extrados (passing through nylon spacer 10) of shape is pressed in adjustment seat 16.By the leverage of 2 extrados of thrust handle, pressing or
Lift the lifting of the adjustable floating slider 4 of thrust handle 2.
As shown in Figures 4 to 6, in the present embodiment, 2 hinged place of thrust handle is a pair of of auricle, is set between a pair of of auricle
There is tabletting 5,4 top of floating slider is located between a pair of of auricle, and articulated shaft 15 passes through a pair of of auricle and is pressed in the top of floating slider 4
End, tabletting 5 and floating slider 4 are connected and fixed and 4 top of floating slider are cooperated to form the axis hole for accommodating articulated shaft 15.
As shown in Figures 4 to 6, in the present embodiment, tabletting 5 and floating slider 4 pass through the countersunk head spiral shell of 15 two sides of articulated shaft
Nail 12 is connected and fixed, sunk screw 12 expose after passing through floating slider 4 and tabletting 5 from 4 bottom of floating slider and exposed portion with
Cover type nut 13 connects.
As shown in Figures 4 to 6, in the present embodiment, bottom pin spring 11 is cased on bottom pin 6, under original state, spring is sold at bottom
11 compression bottom pins 6 are in extended position, and pin 6 top in bottom is connected with carrying handle 7, and carrying handle 7 is exposed at outside the top of adjusting seat
Face, when lifting carrying handle 7, bottom pin 6 is retracted and spring 11 is sold at compression bottom.
As shown in Figures 4 to 6, in the present embodiment, 16 bottom surface of adjustment seat is equipped with bottom pin hole, top surface is equipped with carrying handle slot
29, bottom pin hole is connected to carrying handle slot 29 by being narrower than the connecting hole 28 of bottom pin hole, 6 lower part of bottom pin be width portion and with bottom pin hole
Cooperation, top are narrow portion and are cased with bottom pin spring 11, and bottom pin spring 11 is stuck between bottom pin hole inner face and width portion, carrying handle
7 a part are connect with narrow portion, and another part is located in carrying handle slot 29 and cannot protrude into connecting hole 28.Structure fabrication installation
Simply, prevent bottom pin 6 from deviating from.
As shown in figure 3, in the present embodiment, support rod 23 includes horizontal support rod 23 and tilting support rod 23, branch
Strut 23 is realized flexible in such a way that multistage is socketed and realizes multiposition locking (support by multiple jacks and Quick-release pin cooperation
The arrangement of jack guarantees that two 16 spacing of adjustment seat in different upright bars are adjacent two circular hole portions on aircarrier aircraft sliding rail on bar 23
The integral multiple of column pitch, using rail structure made in Great Britain, adjacent two circular hole position spacing is the aircarrier aircraft sliding rail of the present embodiment
25.4mm), hingedly (23 both ends ears connector of support rod is by Quick-release pin and stands with two columns 18 respectively at the both ends of support rod 23
Monaural connector connection on column 18).
As shown in figure 3, in the present embodiment, 14 tail portion of stretcher is furnished with equipped with two-point belt restraint system 20, stem
Four point seat belt restraint system 21 and stem can be lifted up certain angle.
In the present embodiment, column 18 is equipped with several waist type grooves, and support arm 19 is mounted in waist type groove, support arm 19 with not
With position waist type groove cooperation realize height it is adjustable, so as to adjust stretcher 14 layer away from.
It should be understood that for those of ordinary skills, it can be modified or changed according to the above description,
And all these modifications and variations should all belong to the protection domain of appended claims of the present invention.
Claims (10)
1. a kind of stretcher station being mounted on aircarrier aircraft, it is characterised in that: including at least one layer of stretcher, each stretcher head and the tail
It is mounted on two support arms, ipsilateral support arm is height-adjustable to be mounted on the same column, by that can stretch between two columns
It is connected after contracting and flexible by the fixed support rod of lock, column is fixed on the base, and pedestal is set respectively by two adjustment seats
On adjacent two across aircarrier aircraft sliding rail, pedestal is equipped with locating slot, is equipped at the top of adjustment seat and to be slidably matched with base bottom
Upper dovetail groove and be able to cooperate the item pin for being caught in locating slot and being capable of resetting, bottom is equipped with and the lower dovetail groove of aircarrier aircraft sliding rail is sliding
The sliding block of dynamic cooperation and the bottom pin for being able to cooperate the circular hole position being caught on lower dovetail groove and being capable of resetting, the arrangement of locating slot guarantee
Two adjustment seats on pedestal adapt to the span of aircarrier aircraft sliding rail.
2. being mounted on the stretcher station on aircarrier aircraft as described in claim 1, it is characterised in that: locating slot is located at pedestal edge
Edge, base edge cooperate in upper dovetail groove, ejector pin be located at it is in upper dovetail groove and can with locating slot cooperate side be inside,
The other side that is outside upper dovetail groove and exposing adjustment seat outer surface of cupular part is outside, and ejector pin bottom is always by ejector pin spring top
Tightly, when cooperating on the inside of ejector pin with open slot, ejector pin inside top is against on dovetail groove, hereafter, when pressing on the outside of ejector pin can will
Dovetail groove or less is brought on the inside of ejector pin.
3. being mounted on the stretcher station on aircarrier aircraft as claimed in claim 2, it is characterised in that: adjustment seat bottom surface is equipped with ejector pin
Hole, top surface are equipped with ejector pin handle hole, and knock hole side is protruded into dovetail groove, the other side and ejector pin handle hole penetrate through, outside ejector pin
Lateral roof is located in ejector pin handle hole, rest part is located in knock hole, and knock hole bottom opening is capped closing, ejector pin spring
It is stuck between ejector pin and capping.
4. being mounted on the stretcher station on aircarrier aircraft as described in claim 1, it is characterised in that: an adjustment seat is fixed with two
A sliding block, a sliding block are fixed sliding block, another sliding block is the floating slider that can be gone up and down, fixed sliding block and floating slider difference
Positioned at the two sides of bottom pin, lower dovetail groove can be protruded into simultaneously when fixing the circular hole position that sliding block and floating slider are aligned on lower dovetail groove
With the cooperation of lower dovetail groove and floating slider is by lifting that gap can be generated with lower dovetail groove, and fixed sliding block and floating slider are under
Circular hole position on dovetail groove cannot deviate from when being staggered from lower dovetail groove, the circular hole position that bottom pin cooperation is caught on lower dovetail groove
When, fixed sliding block and floating slider are staggered with the circular hole position on lower dovetail groove.
5. being mounted on the stretcher station on aircarrier aircraft as claimed in claim 4, it is characterised in that: floating slider cooperation is being floated
In slider bore and top and bottom end are all exposed, and floating slider top is hinged with thrust handle, the side of the hinge joint of thrust handle
It is bent into arc-shaped, the extrados of arc-shaped is pressed in adjustment seat.
6. being mounted on the stretcher station on aircarrier aircraft as described in claim 1, it is characterised in that: be cased with bottom pin bullet on the pin of bottom
Spring, under original state, bottom sells spring compression bottom pin and is in extended position, and bottom pin top is connected with carrying handle, carrying handle dew
Outside the top of adjusting seat, when lifting carrying handle, bottom pin is retracted and spring is sold at compression bottom.
7. being mounted on the stretcher station on aircarrier aircraft as claimed in claim 6, it is characterised in that: sold the bottom of equipped with adjustment seat bottom surface
Hole, top surface are equipped with carrying handle slot, and bottom pin hole is connected to carrying handle slot by being narrower than the connecting hole of bottom pin hole, and bottom pin lower part is
Wide portion and be narrow portion with the cooperation of bottom pin hole, top and be cased with bottom and sell spring, bottom sell Spring Card bottom pin hole inner face and width portion it
Between, carrying handle a part is connect with narrow portion, and another part is located in carrying handle slot and cannot protrude into connecting hole.
8. being mounted on the stretcher station on aircarrier aircraft as described in claim 1, it is characterised in that: support rod includes horizontal branch
Strut and tilting support rod, support rod are realized flexible in such a way that multistage is socketed and are cooperated by multiple jacks and Quick-release pin
Realize multiposition locking, the both ends of support rod are hinged with two columns respectively.
9. being mounted on the stretcher station on aircarrier aircraft as described in claim 1, it is characterised in that: be furnished with two point form in stretcher tail portion
Safety belt restraining system, stem are equipped with four point seat belt restraint system and stem can be lifted up certain angle.
10. being mounted on the stretcher station on aircarrier aircraft as described in claim 1, it is characterised in that: column is equipped with several
Waist type groove, support arm are mounted in waist type groove, and the waist type groove cooperation of support arm and different location realizes that height is adjustable, so as to adjust stretcher
Layer away from.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811349382.3A CN109436333A (en) | 2018-11-13 | 2018-11-13 | It is mounted on the stretcher station on aircarrier aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811349382.3A CN109436333A (en) | 2018-11-13 | 2018-11-13 | It is mounted on the stretcher station on aircarrier aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109436333A true CN109436333A (en) | 2019-03-08 |
Family
ID=65552225
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811349382.3A Pending CN109436333A (en) | 2018-11-13 | 2018-11-13 | It is mounted on the stretcher station on aircarrier aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109436333A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111150562A (en) * | 2019-11-15 | 2020-05-15 | 陕西飞机工业（集团）有限公司 | Stretcher rescue equipment used on airplane |
| CN111671578A (en) * | 2020-07-23 | 2020-09-18 | 沈刚 | Batch wounded post-delivery transportation system |
| CN112402124A (en) * | 2020-11-17 | 2021-02-26 | 中航通飞华南飞机工业有限公司 | Quick assembly disassembly and locking device of aircraft airborne stretcher |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2743684A (en) * | 1952-07-12 | 1956-05-01 | Gordon D Brown | Tie-down track fitting |
| US4213593A (en) * | 1979-05-25 | 1980-07-22 | Koehler-Dayton, Inc. | Aircraft seat with concealed locking and releasing mechanism |
| US4913489A (en) * | 1979-06-06 | 1990-04-03 | Tissmetal Lionel-Dupont | Device for varying the distance between the seats in commercial aircraft |
| US20030143052A1 (en) * | 2002-01-30 | 2003-07-31 | Arinc Incorporated | Medical evacuation patient support pallet |
| WO2008113610A2 (en) * | 2007-03-22 | 2008-09-25 | Allsafe Jungfalk Gmbh & Co.Kg | Device for the fixation of objects |
| CN201743842U (en) * | 2010-08-30 | 2011-02-16 | 山东太古飞机工程有限公司 | Civil aviation airline aviation stretcher |
| CN106580567A (en) * | 2017-01-22 | 2017-04-26 | 湖北航宇嘉泰飞机设备有限公司 | Aviation stretcher capable of being rapidly detached |
| CN106726178A (en) * | 2017-01-22 | 2017-05-31 | 湖北航宇嘉泰飞机设备有限公司 | The double-deck aviation stretcher torn open can quickly be pacified |
-
2018
- 2018-11-13 CN CN201811349382.3A patent/CN109436333A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2743684A (en) * | 1952-07-12 | 1956-05-01 | Gordon D Brown | Tie-down track fitting |
| US4213593A (en) * | 1979-05-25 | 1980-07-22 | Koehler-Dayton, Inc. | Aircraft seat with concealed locking and releasing mechanism |
| US4913489A (en) * | 1979-06-06 | 1990-04-03 | Tissmetal Lionel-Dupont | Device for varying the distance between the seats in commercial aircraft |
| US20030143052A1 (en) * | 2002-01-30 | 2003-07-31 | Arinc Incorporated | Medical evacuation patient support pallet |
| WO2008113610A2 (en) * | 2007-03-22 | 2008-09-25 | Allsafe Jungfalk Gmbh & Co.Kg | Device for the fixation of objects |
| CN201743842U (en) * | 2010-08-30 | 2011-02-16 | 山东太古飞机工程有限公司 | Civil aviation airline aviation stretcher |
| CN106580567A (en) * | 2017-01-22 | 2017-04-26 | 湖北航宇嘉泰飞机设备有限公司 | Aviation stretcher capable of being rapidly detached |
| CN106726178A (en) * | 2017-01-22 | 2017-05-31 | 湖北航宇嘉泰飞机设备有限公司 | The double-deck aviation stretcher torn open can quickly be pacified |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111150562A (en) * | 2019-11-15 | 2020-05-15 | 陕西飞机工业（集团）有限公司 | Stretcher rescue equipment used on airplane |
| CN111671578A (en) * | 2020-07-23 | 2020-09-18 | 沈刚 | Batch wounded post-delivery transportation system |
| CN112402124A (en) * | 2020-11-17 | 2021-02-26 | 中航通飞华南飞机工业有限公司 | Quick assembly disassembly and locking device of aircraft airborne stretcher |
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Application publication date: 20190308 |