CN202322243U - Rescue equipment for pilot in danger - Google Patents
Rescue equipment for pilot in danger Download PDFInfo
- Publication number
- CN202322243U CN202322243U CN2011204000159U CN201120400015U CN202322243U CN 202322243 U CN202322243 U CN 202322243U CN 2011204000159 U CN2011204000159 U CN 2011204000159U CN 201120400015 U CN201120400015 U CN 201120400015U CN 202322243 U CN202322243 U CN 202322243U
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- Prior art keywords
- danger
- aviator
- rescue
- rescue equipment
- lifting appliance
- 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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- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 claims description 54
- 229910000831 Steel Inorganic materials 0.000 claims description 10
- 239000010959 steel Substances 0.000 claims description 10
- 210000001217 buttock Anatomy 0.000 claims description 3
- 208000027418 Wounds and injury Diseases 0.000 abstract description 5
- 230000006378 damage Effects 0.000 abstract description 4
- 208000014674 injury Diseases 0.000 abstract description 4
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229920000742 Cotton Polymers 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000009429 distress Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- KQTVWCSONPJJPE-UHFFFAOYSA-N etridiazole Chemical compound CCOC1=NC(C(Cl)(Cl)Cl)=NS1 KQTVWCSONPJJPE-UHFFFAOYSA-N 0.000 description 1
- 210000002414 leg Anatomy 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Images
Landscapes
- Ladders (AREA)
- Emergency Lowering Means (AREA)
Abstract
The utility model provides rescue equipment for a pilot in danger, comprising a hoisting device, a lifting plate for fixing the pilot, a movable base and a lifting mechanism, wherein the hoisting device can be arranged on the base in a pivoted manner, and is connected with the lifting plate in an adjustable manner; the two ends of the lifting mechanism are respectively connected with the base and the hoisting device in a pivoted manner so as to drive the hoisting device to pivot in a vertical plane. Due to the movable base, the rescue equipment can be applicable to the environments of flat airports and war airports, can reach the accident site rapidly and rescue the pilot in danger quickly. The rescue equipment is applicable to fast deplaning when the pilots of various fighters and attackers are in danger on the airports, can meet the requirement for aerial sanitation guarantee of out-field flying, and has the characteristics of strong maneuverability and low cost. Due to adoption of the lifting plate, the secondary injury to the pilot with the injured vertebral column can be prevented.
Description
Technical field
The utility model relates to rescue equipment, more specifically, relates to a kind of aviator rescue equipment in danger.
Background technology
Aviator of the prior art rescue equipment in danger has following several kinds of forms: (1) single ladder, and it is used for the aviator and the technical attendant boards, and the rescue personnel boards with this ladder injured aviator is sued and laboured.(2) double ladder, it has telescopic band and has secondary ladder to rescue device with simply hanging, and the sanitation and first-aid personnel board with it the aviator are implemented first aid.(3) medical truck can be fixed on the medical truck casing hanging the equipment of rescuing, and is furnished with hanging basket, backbone protection boatswain chair etc. on the medical truck, and the rescue personnel stands in and hangs in the basket, hangs and rescues injured aviator.
Wherein, (1) and (2) dual mode goes out the situation that the passenger cabin mode does not consider that all aviator's backbone is hindered to injured aviator, thereby, possibly carry away in the passenger cabin process in that the aviator is taken, aviator's backbone is caused the injured problem of secondary.(3) kind mode can only be not easy to operation in a side of aircraft cockpit to suing and labouring of aviator, and the operation relative complex, needs the professional, and the equipment price is higher relatively, not through design typification, does not promote the use of so far.
The utility model content
The utility model aims to provide a kind of aviator rescue equipment in danger, gets into danger with the aviator who solves prior art and gives first aid to the problem that equipment mobility is not high, price is high, possibly cause secondary to injure the aviator of vertebrae injry.
For solving the problems of the technologies described above, according to an aspect of the utility model, a kind of aviator is provided the rescue equipment that gets into danger, comprising: lifting appliance, the boatswain chair that is used for fixing the aviator, moveable base and lifting mechanism; Lifting appliance is pivotably mounted on the base, and adjustable ground is connected between lifting appliance and the boatswain chair; The two ends of lifting mechanism are connected with lifting appliance to drive lifting appliance with base pivotly respectively and in perpendicular, pivot.
Further, base comprises the chassis and is arranged on the underframe on the chassis, is provided with a feet respectively pivotly on four angles of underframe.
Further, also be provided with tool box and horizontal rotation unit on the underframe, lifting appliance is installed on the horizontal rotation unit through the support portion.
Further, aviator's rescue equipment in danger also comprises the rescue ladder, and the support portion comprises support and is arranged on being used on the support and hangs the hook of rescue ladder.
Further, the rescue ladder comprises two ladders, and the middle part of two ladders removably connects through adjustable pipe link.
Further, two ladders be respectively arranged with sucker with the contacted end of passenger cabin aircraft.
Further, lifting appliance comprises a plurality of retracted support arms, is provided with the elastic locking element in the junction of adjacent two hold-down arms, and lifting appliance also comprises winch mechanism, and winch mechanism comprises steel rope, and boatswain chair is connected with steel rope.
Further, winch mechanism also comprises manual rocking handle.
Further, boatswain chair comprises the plate body of being processed by glass-felt plastic.
Further, boatswain chair also comprises head band, chest clamping band, fixing strap of waist, buttocks clamping band and the suspender belt that is arranged on the plate body.
The utility model base is movably; Applicable to flat, opportunity of combat field environment; Can arrive at the scene of the accident fast, rescue aviator in danger rapidly, be applicable to that various destroying (by force) hit machine aviator disembarking fast after getting into danger in the airport; And can satisfy the outfield flight hygiene of aviation and ensure requirement, have mobility strong, characteristics that cost is low.Owing to adopted boatswain chair, can prevent the aviator of vertebrae injry is caused the secondary injury.
Description of drawings
The accompanying drawing that constitutes the application's a part is used to provide the further understanding to the utility model, and illustrative examples of the utility model and explanation thereof are used to explain the utility model, do not constitute the improper qualification to the utility model.In the accompanying drawings:
Fig. 1 has schematically shown the front view of the utility model;
Fig. 2 has schematically shown the birds-eye view of Fig. 1;
Fig. 3 has schematically shown the running condition figure of the utility model;
Fig. 4 has schematically shown the structural representation of underframe;
Fig. 5 has schematically shown the birds-eye view of Fig. 4;
Fig. 6 has schematically shown the structural representation of support portion;
Fig. 7 has schematically shown the lateral plan of Fig. 6;
Fig. 8 has schematically shown the front view of lifting appliance;
Fig. 9 has schematically shown the birds-eye view of Fig. 8; And
Figure 10 has schematically shown the structural representation of boatswain chair.
The specific embodiment
Embodiment to the utility model is elaborated below in conjunction with accompanying drawing, but the multitude of different ways that the utility model can be defined by the claims and cover is implemented.
Shown in Fig. 1-3, the rescue equipment in danger of the aviator in the utility model comprises: lifting appliance 3, the boatswain chair 6 that is used for fixing the aviator, moveable base 1 and lifting mechanism 4; Wherein, lifting appliance 3 is pivotably mounted on the base 1, and adjustable ground is connected between lifting appliance 3 and the boatswain chair 6; The two ends of lifting mechanism 4 are connected with lifting appliance 3 to drive lifting appliance 3 with base 1 pivotly respectively and in perpendicular, pivot.Preferably, base 1 tows by tractor truck, thereby after can hanging over the airport service truck, is applicable to that outfield runway, pan soil ground, the meadow on airport exercised.As shown in Figure 3; In the time need rescuing to the aviator 8 in the passenger cabin 7 of aircraft; Can the rescue equipment in danger of the aviator in the utility model be moved near the passenger cabin through its moveable base; Utilize lifting mechanism that lifting appliance is rotated to the position of being convenient to lift by crane aviator 8 then, then aviator 8 is fixed on the boatswain chair, then can be with aviator's rescue to the destination through the operation lifting appliance.Owing to adopted moveable base, therefore, but the rescue equipment at high speed in danger of the aviator in the utility model arrives the scene of the accident, thereby has improved the speed of reaching the spot, and has mobility strong, characteristics that cost is low; Because the sling height of lifting appliance is adjustable, therefore, hits machine applicable to destroy (by force) of various types; Owing to adopted boatswain chair, can prevent the aviator of vertebrae injry is caused the secondary injury.Preferably, moveable base 1 adopts the military trailer chassis of military trailer chassis, particularly QG0.85.
Preferably; Lifting mechanism 4 comprises pitch wheel and tooth bar (not shown); Lifting mechanism 4 also comprises the friction ratchet gear unit (not shown) that is used to lock; The friction ratchet gear unit adopts the eccentric segment voussoir to replace ratchet, utilizes friction force and voussoir accentric geometric condition between voussoir and friction wheel to realize the unidirectional rotation at intermittence of friction wheel.Lifting mechanism 4 utilizes lever principle to operate lifting appliance 3, has when liter labour-saving characteristics.
Preferably, shown in Fig. 1-5, base 1 comprises chassis 11 and is arranged on the underframe 12 on the chassis 11, is provided with a feet 121 respectively pivotly on four angles of underframe 12, tumble at work preventing, and the stability when having strengthened work.Also be provided with tool box 123 and horizontal rotation unit 122 on the underframe 12, lifting appliance 3 is installed on the horizontal rotation unit 122 through support portion 2.Preferably, underframe 12 is welded by refined steel, and decorative pattern alloy aluminium sheet is adopted on its floor.Preferably, support portion 2 is formed by the seam of refined steel rectangular tube.The traction assembly on chassis 11 adopts the cotton fluted disc of both-end to clamp (not shown), can conveniently adjust the high and low position and the maintenance level of eye hitch, makes tractive force keep optimum regime.Preferably, chassis 11 is the single-axle trailer chassis, and it adopts the torsion bar (not shown) is damper element, adopts the inertia braking principle during driving, adopts hand brakingly during parking, thereby certain sloping ability of staying is arranged.Preferably, horizontal rotation unit 122 can adopt the rotation supporting structure of medium semitrailer, preferably; This rotation supporting structure comprises upper and lower revolution supporting disk composition; There is steel ball the centre of upper and lower revolution supporting disk, to reach spinfunction, adopts this rotation supporting structure to have compact conformation, good rigidly, running is steady, precision is high, safe and reliable characteristics; And simultaneously bearing radial force and tilting moment, be to bear heavy load, slow-revving ideal structure.
Preferably, like Fig. 1-3, shown in the 6-7, aviator's rescue equipment in danger also comprises rescue ladder 5, and rescue ladder 5 is mainly used in the rescue personnel and boards rapidly and launch the work of suing and labouring.Support portion 2 comprises support 21 and is arranged on being used on the support 21 and hangs the hook 22 of rescue ladder 5 that rescue ladder 5 is fixed on the hook 22, so that transportation obsolete the time; In use, can be easily will rescue ladder 5 on 22 and take off, and ride on the passenger cabin 7 from linking up with.Preferably, as shown in Figure 3, rescue ladder 5 comprises two ladders 51; The middle part of two ladders 51 removably connects through adjustable pipe link 52, and like this, an end of rescue ladder 5 rides on the passenger cabin 7; Its other end supports on the ground, thereby realizes to rescuing the fixing of ladder 5, therefore; Two ladders 51 can place the both sides of aircraft respectively, to guarantee two rescue personnels expansion rescue of can boarding simultaneously; In addition, the purpose that conversion launches height can also also be reached through the length of regulating pipe link 52, to be applicable to various type.Preferably; Passenger cabin 7 contacted ends two ladders 51 and aircraft are respectively arranged with the sucker (not shown); Above-mentioned end to prevent to rescue ladder 5 slides on the surface of passenger cabin 7, thereby guarantees the rescue group in the rescue process, and rescue terraced 5 remains stable.
Preferably, like Fig. 3, shown in the 8-9; Lifting appliance 3 comprises a plurality of retracted support arms 31, is provided with elastic locking element 33 in the junction of adjacent two hold-down arms 31, and lifting appliance 3 also comprises winch mechanism 32; Winch mechanism 32 comprises steel rope, and boatswain chair 6 is connected with steel rope.Elastic locking element 33 is used for keeping between two adjacent hold-down arms 31 state of locking, prevents the retraction of hold-down arm 31.In addition, between two hold-down arms 31 of cover that contract each other, also be provided with roller 34, so that hold-down arm 31 is flexible.Like this, when the steel rope of operation winch mechanism 32 folding and unfoldings on it, just can regulate the height of boatswain chair 6, so that rescue.Preferably, winch mechanism 32 also comprises manual rocking handle 321, therefore, does not need extra power, only need just can operate winch mechanism 32 through the mode of manual work, can under no any foreign aid's power situation, launch salvage work rapidly.Preferably, winch mechanism 32 also comprises the variable gear (not shown), can reach laborsaving, fast speed effect through variable gear.
Preferably, like Fig. 3, shown in 10, boatswain chair 6 comprises the plate body of being processed by glass-felt plastic 61, owing to adopted boatswain chair 6, therefore, can realize hanging the function of rescuing and can prevent that injured aviator's backbone secondary is injured.Boatswain chair 6 also comprises head band 62, chest clamping band 63, fixing strap of waist 65 and the buttocks clamping band 66 that is arranged on the plate body 61.Further, also be provided with suspender belt 64 on the boatswain chair 6, it has the characteristics of rescuing of hanging to non-vertebrae injry or the aviator of deliver from vault preparation voluntarily due to wound, can after canopy is opened or torn down, injured aviator be hung out passenger cabin, is put into ground.
During use, at first the rescue equipment in danger of the aviator in the utility model is connected with trailer, and being drawn to by the aircraft in distress; Then, the afterbody of trailer is adjusted to the position vertical with the passenger cabin of aircraft, the lifting appliance of the utility model is alignd with the passenger cabin middle part, preferably, the afterbody that makes trailer is apart from airframe 1.5～2m; Then; The utility model is separated with trailer, and the rescue worker will rescue ladder from the support portion of the utility model and take off, and respectively four supporting legs on the base launched; To rescue the terraced passenger cabin both sides of launching to place aircraft again; And connect fixingly with pipe link, at this moment, the rescue worker just can be from the rescue ladder of the both sides rescue the wounded of boarding; Simultaneously; Operating personal rotates to the direction parallel with aircraft with lifting appliance, and lifting appliance is launched, and through lifting mechanism lifting appliance is adjusted to suitable height; Rotate lifting appliance in the horizontal direction through the horizontal rotation unit then, make boatswain chair vertical with the middle part of passenger cabin; After the rescue worker inserts boatswain chair the aviator behind; Clamping band with on the boatswain chair is fixed the aviator; And boatswain chair and aviator be held together, through the operation winch mechanism hang out the aviator outside the passenger cabin and be placed directly on the stretcher after send in medical truck and treat.
The utility model base is movably; Applicable to flat, opportunity of combat field environment; Can arrive at the scene of the accident fast, rescue aviator in danger rapidly, be applicable to that various destroying (by force) hit machine aviator disembarking fast after getting into danger in the airport; And can satisfy the outfield flight hygiene of aviation and ensure requirement, have mobility strong, characteristics that cost is low.Owing to adopted boatswain chair, can prevent the aviator of vertebrae injry is caused the secondary injury.
The preferred embodiment that the above is merely the utility model is not limited to the utility model, and for a person skilled in the art, the utility model can have various changes and variation.All within the spirit and principle of the utility model, any modification of being done, be equal to replacement, improvement etc., all should be included within the protection domain of the utility model.
Claims (10)
1. aviator's rescue equipment in danger is characterized in that, comprising:
Lifting appliance (3), the boatswain chair (6) that is used for fixing aviator (8), moveable base (1) and lifting mechanism (4);
Said lifting appliance (3) is pivotably mounted on the said base (1), and adjustable ground is connected between said lifting appliance (3) and the said boatswain chair (6);
The two ends of said lifting mechanism (4) are connected with lifting appliance (3) to drive said lifting appliance (3) with said base (1) pivotly respectively and in perpendicular, pivot.
2. the aviator according to claim 1 rescue equipment that gets into danger; It is characterized in that; Said base (1) comprises chassis (11) and is arranged on the underframe (12) on the said chassis (11), is provided with a feet (121) respectively pivotly on four angles of said underframe (12).
3. the aviator according to claim 2 rescue equipment that gets into danger; It is characterized in that; Also be provided with tool box (123) and horizontal rotation unit (122) on the said underframe (12), said lifting appliance (3) is installed on the said horizontal rotation unit (122) through support portion (2).
4. the aviator according to claim 3 rescue equipment that gets into danger; It is characterized in that; Said aviator rescue equipment in danger also comprises rescue ladder (5), and said support portion (2) comprise support (21) and are arranged on being used on the said support (21) and hang the hook (22) of said rescue terraced (5).
5. the aviator according to claim 4 rescue equipment that gets into danger is characterized in that, said rescue ladder (5) comprises two ladders (51), and the middle part of said two ladders (51) removably connects through adjustable pipe link (52).
6. the aviator according to claim 5 rescue equipment that gets into danger is characterized in that said two ladders are (51) to be respectively arranged with sucker with the contacted end of passenger cabin aircraft (7).
7. the aviator according to claim 1 rescue equipment that gets into danger; It is characterized in that; Said lifting appliance (3) comprises a plurality of retracted support arms (31), is provided with elastic locking element (33) in the junction of adjacent two said hold-down arms (31), and said lifting appliance (3) also comprises winch mechanism (32); Said winch mechanism (32) comprises steel rope, and said boatswain chair (6) is connected with said steel rope.
8. the aviator according to claim 7 rescue equipment that gets into danger is characterized in that said winch mechanism (32) also comprises manual rocking handle (321).
9. the aviator according to claim 1 rescue equipment that gets into danger is characterized in that said boatswain chair (6) comprises the plate body of being processed by glass-felt plastic (61).
10. the aviator according to claim 9 rescue equipment that gets into danger; It is characterized in that said boatswain chair (6) also comprises head band (62), chest clamping band (63), fixing strap of waist (65), buttocks clamping band (66) and the suspender belt (64) that is arranged on the said plate body (61).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011204000159U CN202322243U (en) | 2011-10-19 | 2011-10-19 | Rescue equipment for pilot in danger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011204000159U CN202322243U (en) | 2011-10-19 | 2011-10-19 | Rescue equipment for pilot in danger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202322243U true CN202322243U (en) | 2012-07-11 |
Family
ID=46434233
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011204000159U Expired - Fee Related CN202322243U (en) | 2011-10-19 | 2011-10-19 | Rescue equipment for pilot in danger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202322243U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113815880A (en) * | 2021-07-22 | 2021-12-21 | 中国人民解放军空军军医大学 | Emergency pilot power lifting and rescuing platform |
-
2011
- 2011-10-19 CN CN2011204000159U patent/CN202322243U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113815880A (en) * | 2021-07-22 | 2021-12-21 | 中国人民解放军空军军医大学 | Emergency pilot power lifting and rescuing platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120711 Termination date: 20121019 |