CN215043803U - Emergency pilot power lifting platform - Google Patents
Emergency pilot power lifting platform Download PDFInfo
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- CN215043803U CN215043803U CN202121684454.7U CN202121684454U CN215043803U CN 215043803 U CN215043803 U CN 215043803U CN 202121684454 U CN202121684454 U CN 202121684454U CN 215043803 U CN215043803 U CN 215043803U
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- operation cabin
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- cabin
- hoisting mechanism
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Abstract
The utility model discloses an emergency pilot power hangs platform of rescuing belongs to emergency pilot rescue equipment technical field. The platform comprises an operation cabin, a connecting arm member, a hoisting mechanism, a forward tilting door, a cabin door, an operating rod, a searchlight and a control console, wherein an installation cavity is arranged on the right side of the operation cabin, one end of the connecting arm member is installed in the installation cavity, the hoisting mechanism is installed in the operation cabin, a linear slide rail is laid between the bottom of the hoisting mechanism and the bottom of the operation cabin, the hoisting mechanism and the operation cabin are in sliding connection through the linear slide rail, a punching plate is laid at the inner bottom of the operation cabin, a quick pressing clamp is installed on the hoisting mechanism, and a pressing head of the quick pressing clamp is pressed into the punching plate. The power lifting and rescuing platform for the distress pilots has an autonomous power lifting and rescuing function, can finish the lifting and rescuing process of the pilots by only 1 rescue worker, and can be used for the distress pilots to quickly separate from a cockpit.
Description
Technical Field
The utility model belongs to the technical field of pilot rescue equipment in distress, particularly, relate to a pilot power that distress hangs platform.
Background
The emergency pilot can quickly break away from the cockpit and timely rescue the emergency pilot, which is an important link and means for guaranteeing the life of the pilot and promoting the flight safety. Rescue devices such as current combination formula emergency escape ladder, rescue stretcher, unpowered crane operate complicatedly, need 3 people's collective operations, and sling device fault rate is high, and the capstan winch device easily leads to operating personnel to be injured, can't satisfy the emergent rescue demand of the pilot in danger, and the main problem of existence has:
1. the rescue ability is poor, the emergency pilot is rescued by using the combined escape ladder and the pilot emergency rescue equipment, the emergency rescue requirements of the pilot of the old model can only be met, and the emergency rescue requirements of the new model are difficult to meet;
2. the rescue efficiency is low, the existing emergency rescue equipment is used, the labor intensity is high, the operation time is long, the efficiency is low, and the rapid rescue of pilots is difficult to carry out;
3. the mode is single, adaptability is poor, the mode of the emergency rescue plan that the existing distress pilot breaks away from the cockpit after forced landing is single, and the requirements of all models and all dangerous situations are difficult to adapt.
In order to solve the above problems, it is necessary to develop a novel power-type special rescue device, which is combined with a multi-mode rescue plan design to meet the needs of the pilots in danger for fast getting off the aircraft for rescue.
SUMMERY OF THE UTILITY MODEL
The utility model provides a pilot power that meets danger hangs and rescues platform to the not enough of prior art to solve the problem of proposing in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a pilot power hoisting and rescuing platform in danger comprises an operation cabin, a connecting arm member, a hoisting mechanism, a forward tilting door, a cabin door, an operating rod, a searchlight and a control console, wherein the right side of the operation cabin is provided with an installation cavity, one end of the connecting arm member is installed in the installation cavity, the hoisting mechanism is installed in the operation cabin, a linear slide rail is paved between the bottom of the hoisting mechanism and the inner bottom of the operation cabin, the hoisting mechanism and the operation cabin are in sliding connection through the linear slide rail, a punching plate is paved at the inner bottom of the operation cabin, a quick pressing clamp is installed on the hoisting mechanism, the pressing head part of the quick pressing clamp is pressed into the punching plate, the hoisting mechanism and the operation cabin are in locking connection, the forward tilting door is installed at the left side of the operation cabin through a door hinge, the cabin door is in sliding installation at the front side of the operation cabin, the operating rod and the searchlight are respectively installed at the inner top end of the operation cabin, and the operating rod is electrically connected with the hoisting mechanism, the control console is arranged on the inner side wall of the operation cabin, and the connecting arm member and the hoisting mechanism are electrically connected with the control console.
As an optimal technical scheme of the utility model, the operation cabin is the screen frame structure, and its bottom fixed mounting has the area to brake the universal wheel.
As a preferred technical scheme of the utility model, the hookup arm component includes main cantilever crane, main arm support, ear seat, first electric putter and push rod support, the main arm support is articulated mutually through the round pin axle with the one end of main cantilever crane, the welding has the ear seat on the main cantilever crane, first electric putter's one end is articulated mutually through round pin axle and ear seat, and its output is articulated mutually through round pin axle and push rod support.
As an optimized technical scheme of the utility model, the main cantilever crane is Y type structure, and the top of main cantilever crane is equipped with the traction seat, install angle sensor on the first electric putter.
As a preferred technical scheme of the utility model, it includes base plate, pedestal, electrodynamic type telescopic link, second electric putter and davit to hang lift mechanism, the pedestal articulates on the base plate through the round pin axle, the electrodynamic type telescopic link is installed on the pedestal, second electric putter's one end articulates on the base plate, and its output is articulated mutually with the electrodynamic type telescopic link, the davit is installed on the output of electrodynamic type telescopic link.
As a preferred technical scheme of the utility model, install the hoop on the electrodynamic type telescopic link, second electric putter passes through the hoop and is articulated with the electrodynamic type telescopic link, the one end that the davit is connected with the output of electrodynamic type telescopic link is the open loop configuration, and installs the hand on it and twists the bolt, twists the output fastening connection of bolt and electrodynamic type telescopic link through the hand.
As a preferred technical scheme of the utility model, the door that leans forward is including buffering horizontal pole, air spring and driving lever module, the one end of air spring articulates on buffering horizontal pole, and its output is articulated mutually with the driving lever module.
As an optimal technical scheme of the utility model, the hatch door includes skeleton, guide arm and hasp are installed in proper order on the skeleton, the hatch door passes through the hasp and is connected with the operation cabin lock.
As an optimized technical scheme of the utility model, the action bars has circular button and square button, and it is used for realizing the lift and the inclination of control hoisting mechanism.
As an optimal technical scheme of the utility model, the control cabinet mainly comprises total switch, hookup arm adjustment key, the reserve control switch that lifts, light switch and emergency braking switch, and it is used for realizing the control and the reserve control that lifts of hookup arm.
Compared with the prior art, the utility model provides a pilot power in danger hangs platform of rescuing possesses following beneficial effect:
(1) the power lifting and rescuing platform for the pilots in distress is used for enabling the pilots in distress to quickly separate from a cockpit, has an autonomous power lifting and rescuing function, can finish the lifting and rescuing process of the pilots by only 1 rescue worker, and is simple to operate.
(2) The power lifting and rescuing platform for the pilots in distress has a dynamic balance function, the lifting and rescuing platform is always in a horizontal state in the rescuing process, the safety of rescuers is ensured, and the contact surface of the lifting and rescuing platform and an airplane is made of soft packing materials, so that the safety of the airplane is ensured.
(3) The power lifting and rescuing platform for the pilots in distress has the maximum operation height of not less than 6m and wide applicable machine types.
Drawings
FIG. 1 is a schematic structural view of a distress power rescue platform for pilots in distress;
FIG. 2 is an exploded view of FIG. 1 of the distress pilot powered lift platform;
FIG. 3 is a reverse view of FIG. 1 of the distress pilot powered lift platform;
FIG. 4 is an exploded view of FIG. 3 of the distress pilot powered lift platform;
FIG. 5 is a schematic structural view of a linkage arm member of the distress pilot powered rescue platform;
FIG. 6 is a schematic structural view of a lifting mechanism of a rescue platform powered by a pilot in distress;
FIG. 7 is a schematic structural view of a forward tilting door of the power rescue platform for pilots in distress;
fig. 8 is a schematic structural view of a cabin door of a distress pilot powered rescue platform.
In the figure: 1. an operation cabin; 2. a coupling arm member; 3. a hoisting mechanism; 4. a forward tilt door; 5. a cabin door; 6. An operating lever; 7. a searchlight; 8. a console; 9. a mounting cavity; 10. a linear slide rail; 11. punching a plate; 12. pressing pliers quickly; 13. a universal wheel; 14. a main arm support; 15. a main arm support; 16. an ear mount; 17. A first electric push rod; 18. a push rod support; 19. a traction seat; 20. an angle sensor; 21. a substrate; 22. a pedestal; 23. an electric telescopic rod; 24. a second electric push rod; 25. a suspension arm; 26. a hoop; 27. screwing the bolt by hand; 28. a buffer rail; 29. a gas spring; 30. a deflector rod module; 31. a framework; 32. A guide bar; 33. and (5) locking.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-8, a pilot power lifting platform in distress comprises an operation cabin 1, a connecting arm member 2, a lifting mechanism 3, a forward-tilting door 4, a cabin door 5, an operating rod 6, a searchlight 7 and a control console 8, wherein the right side of the operation cabin 1 is provided with an installation cavity 9, one end of the connecting arm member 2 is installed in the installation cavity 9, the lifting mechanism 3 is installed in the operation cabin 1, a linear slide rail 10 is laid between the bottom of the lifting mechanism 3 and the bottom in the operation cabin 1, the lifting mechanism 3 and the operation cabin 1 are connected in a sliding manner through the linear slide rail 10, a punching plate 11 is laid at the bottom in the operation cabin 1, a rapid press clamp 12 is installed on the lifting mechanism 3, the pressing head of the rapid press clamp 12 is pressed into the punching plate 11, the lifting mechanism 3 is connected with the operation cabin 1 in a locking manner, the forward-tilting door 4 is installed at the left side of the operation cabin 1 through a door hinge, the cabin door 5 is slidably mounted on the front side of the operation cabin 1, the operating rod 6 and the searchlight 7 are respectively mounted at the inner top end of the operation cabin 1, the operating rod 6 is electrically connected with the hoisting mechanism 3, the console 8 is mounted on the inner side wall of the operation cabin 1, and the connecting arm component 2 and the hoisting mechanism 3 are both electrically connected with the console 8.
As a specific technical scheme of this embodiment, the operation cabin 1 is of a net frame structure, and a universal wheel 13 with a brake is fixedly mounted at the bottom thereof.
In the present embodiment, as shown in fig. 1 to 4, the net frame structure is beneficial to making the operation cabin 1 light, the rescue workers can move the rescue platform in any direction by using the universal wheels 13 with the brake, and the rescue platform can be kept in a stop state by using the brake of the universal wheels 13.
As a specific technical solution of this embodiment, the coupling arm member 2 includes a main arm support 14, a main arm support 15, an ear seat 16, a first electric push rod 17 and a push rod support 18, the main arm support 15 is hinged to one end of the main arm support 14 through a pin, the ear seat 16 is welded to the main arm support 14, one end of the first electric push rod 17 is hinged to the ear seat 16 through a pin, and an output end of the first electric push rod is hinged to the push rod support 18 through a pin.
In the present embodiment, as shown in fig. 5, the first electric push rod 17 and the angle sensor 20 are provided, and can work in two modes, namely a manual mode and an automatic mode, and in the manual mode, the angle of the connecting arm can be adjusted to realize the butt joint with the boom of the emergency car.
As a specific technical solution of this embodiment, the main arm support 14 is a Y-shaped structure, a traction seat 19 is disposed at the top end of the main arm support 14, and an angle sensor 20 is mounted on the first electric push rod 17.
In the present embodiment, as shown in fig. 5, in the automatic mode, the angle sensor 20 is used to automatically adjust the angle of the connecting arm, so as to realize automatic dynamic balance during the operation of the rescue platform.
As a specific technical solution of the present embodiment, the lifting mechanism 3 includes a base plate 21, a pedestal 22, an electric telescopic rod 23, a second electric push rod 24 and a suspension arm 25, the pedestal 22 is hinged to the base plate 21 through a pin, the electric telescopic rod 23 is installed on the pedestal 22, one end of the second electric push rod 24 is hinged to the base plate 21, an output end of the second electric push rod is hinged to the electric telescopic rod 23, and the suspension arm 25 is installed at an output end of the electric telescopic rod 23.
In the embodiment, as shown in fig. 6, the rescue personnel can adjust the pitch angle and the telescopic length of the lifting mechanism 3 through the electric control of the operating rod 6, lift the pilot from the cockpit, control the lifting mechanism 3 to move left and right in the operation cabin 1 by using the linear slide rail 10, and realize automatic locking by pressing the quick pressing pliers 12 into different through holes on the punching plate 11.
As a specific technical solution of this embodiment, a hoop 26 is installed on the electric telescopic rod 23, the second electric push rod 24 is hinged to the electric telescopic rod 23 through the hoop 26, one end of the suspension arm 25 connected to the output end of the electric telescopic rod 23 is in an open-loop structure, and a hand-screwed bolt 27 is installed thereon and is tightly connected to the output end of the electric telescopic rod 23 through the hand-screwed bolt 27.
In this embodiment, as shown in fig. 6, the rescue personnel can manually control the boom 25 to rotate, and after rotating to a proper position, the boom can be manually locked by screwing the bolt 27 by hand.
As a specific technical solution of this embodiment, the forward tilting door 4 includes a buffer cross bar 28, a gas spring 29 and a lever module 30, one end of the gas spring 29 is hinged to the buffer cross bar 28, and the output end of the gas spring is hinged to the lever module 30.
In the embodiment, as shown in fig. 7, the forward tilting door 4 can be opened or closed under the action of the gas spring 29 by manually controlling the deflector rod module 30, and the opening angle of the forward tilting door 4 is adjusted, so that the buffering cross rod 28 can protect the surface of the airplane, the lifting and rescue platform is close to the cockpit of the airplane as much as possible, and the rescue personnel can complete the quick escape rescue of the pilot.
As a specific technical solution of this embodiment, the cabin door 5 includes a framework 31, a guide rod 32 and a lock catch 33, the guide rod 32 and the lock catch 33 are sequentially installed on the framework 31, and the cabin door 5 is connected to the operation cabin 1 through the lock catch 33 in a buckling manner.
In the present embodiment, as shown in fig. 8, the rescue worker wears the safety belt before entering the cabin, and after entering the cabin, the cabin door 5 is closed first, and the lock catch 33 is checked to determine whether the safety belt is fastened, and then the safety belt is hung at the designated position of the cabin.
As a specific technical solution of this embodiment, the operating rod 6 has a round key and a square key, and is used for controlling the lifting and the inclination angle of the lifting mechanism 3.
In this embodiment, as shown in fig. 1 to 4, the operation rod 6 can be pushed forward and pulled backward, the square key and the round key can be pressed long and short, the lifting mechanism 3 can be extended and shortened, the operation rod 6 can be pushed forward and pulled backward, the lifting mechanism 3 can be tilted forward and backward, and when the operation rod 6 is adjusted to a proper position, the operation rod 6 is stopped being pushed.
As a specific technical solution of this embodiment, the console 8 mainly includes a main power switch, a connecting arm adjusting key, a lifting standby control switch, a lighting lamp switch, and an emergency brake switch, and is configured to implement control of the connecting arm and lifting standby control.
In the present embodiment, as shown in fig. 1 to 4, the console 8 further includes an automatic leveling switch, in case of failure of the operating lever 6, the standby control of the hoisting mechanism 3 can be realized, and when an emergency occurs, the emergency brake button can realize the emergency braking of the whole machine, the hoisting emergency braking and the emergency braking of the coupling arm, thereby improving the safety of the operation of the hoisting rescue platform.
The utility model discloses a theory of operation and use flow: when the power lifting rescue platform is used, a rescuer carries medical rescue equipment to quickly board the power lifting rescue platform, the rescue platform is controlled to be close to an airplane cockpit through a hydraulic arm operator of the rescue vehicle, the injury condition of a pilot is checked, the rescue scheme of the pilot is determined, a flight suit worn by the pilot is connected by utilizing a hook on the lifting mechanism 3, the rescuer adjusts the pitching angle and the telescopic length of the lifting mechanism 3 through the operating rod 6, the pilot is transferred away from the cockpit, the hand-screwed bolt 27 on the lifting arm 25 is loosened, the pilot is taken away from the cockpit by the adjusting angle, and the pilot can stably and quickly descend to the ground.
In conclusion, the power lifting and rescuing platform for the distress pilots has an autonomous power lifting and rescuing function, can finish the lifting and rescuing process of the pilots by only 1 rescue worker, and can be used for the distress pilots to quickly separate from the cockpit; the platform has a dynamic balance function, the lifting rescue platform is always in a horizontal state in the rescue process, so that the safety of rescuers is ensured, and the safety of an airplane is ensured by adopting a soft packing material on the contact surface of the lifting rescue platform and the airplane; the maximum working height is not less than 6m, and the applicable machine type is wide.
It should be noted that, in this document, terms such as "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. The utility model provides a pilot power of distress lifts by crane platform, includes operation cabin (1), hookup arm component (2), lifts mechanism (3), leans forward door (4), hatch door (5), action bars (6), searchlight (7) and control cabinet (8), its characterized in that: the right side of the operation cabin (1) is provided with an installation cavity (9), one end of the connecting arm component (2) is installed in the installation cavity (9), the hoisting mechanism (3) is installed in the operation cabin (1), a linear slide rail (10) is laid between the bottom of the hoisting mechanism (3) and the inner bottom of the operation cabin (1), the hoisting mechanism (3) and the operation cabin (1) are in sliding connection through the linear slide rail (10), a punching plate (11) is laid at the inner bottom of the operation cabin (1), a rapid pressing pliers (12) is installed on the hoisting mechanism (3), the pressing head of the rapid pressing pliers (12) is pressed into the punching plate (11), the hoisting mechanism (3) and the operation cabin (1) are in locking connection, the forward tilting door (4) is installed on the left side of the operation cabin (1) through a door hinge, the cabin door (5) is in sliding installation at the front side of the operation cabin (1), the operation rod (6) and the searchlight (7) are respectively installed at the inner top end of the operation cabin (1), the operation rod (6) is electrically connected with the hoisting mechanism (3), the control console (8) is installed on the inner side wall of the operation cabin (1), and the connecting arm component (2) and the hoisting mechanism (3) are both electrically connected with the control console (8).
2. The distress pilot powered lift-rescue platform of claim 1, wherein: the operation cabin (1) is of a net frame structure, and the bottom of the operation cabin is fixedly provided with a universal wheel (13) with a brake.
3. The distress pilot powered lift-rescue platform of claim 1, wherein: the connecting arm component (2) comprises a main arm support (14), a main arm support (15), an ear seat (16), a first electric push rod (17) and a push rod support (18), wherein the main arm support (15) is hinged to one end of the main arm support (14) through a pin shaft, the ear seat (16) is welded to the main arm support (14), one end of the first electric push rod (17) is hinged to the ear seat (16) through the pin shaft, and the output end of the first electric push rod is hinged to the push rod support (18) through the pin shaft.
4. A distress pilot powered lift-rescue platform according to claim 3, wherein: the main arm support (14) is of a Y-shaped structure, a traction seat (19) is arranged at the top end of the main arm support (14), and an angle sensor (20) is mounted on the first electric push rod (17).
5. The distress pilot powered lift-rescue platform of claim 1, wherein: hang and rise mechanism (3) and include base plate (21), pedestal (22), electrodynamic type telescopic link (23), second electric putter (24) and davit (25), pedestal (22) articulate on base plate (21) through the round pin axle, electrodynamic type telescopic link (23) are installed on pedestal (22), the one end of second electric putter (24) articulates on base plate (21), and its output is articulated mutually with electrodynamic type telescopic link (23), davit (25) are installed on the output of electrodynamic type telescopic link (23).
6. The distress pilot powered lift-rescue platform of claim 5, wherein: install hoop (26) on electrodynamic type telescopic link (23), second electric putter (24) are articulated through hoop (26) and electrodynamic type telescopic link (23), the one end that davit (25) are connected with the output of electrodynamic type telescopic link (23) is the open loop structure, and installs hand on it and twist bolt (27), twists bolt (27) through the hand and is connected with the output fastening of electrodynamic type telescopic link (23).
7. The distress pilot powered lift-rescue platform of claim 1, wherein: the forward tilting door (4) comprises a buffer cross rod (28), a gas spring (29) and a shifting rod module (30), one end of the gas spring (29) is hinged to the buffer cross rod (28), and the output end of the gas spring is hinged to the shifting rod module (30).
8. The distress pilot powered lift-rescue platform of claim 1, wherein: the cabin door (5) comprises a framework (31), a guide rod (32) and a lock catch (33), the guide rod (32) and the lock catch (33) are sequentially installed on the framework (31), and the cabin door (5) is connected with the operation cabin (1) in a buckled mode through the lock catch (33).
9. The distress pilot powered lift-rescue platform of claim 1, wherein: the operating rod (6) is provided with a round key and a square key.
10. The distress pilot powered lift-rescue platform of claim 1, wherein: the control console (8) mainly comprises a main power switch, a connecting arm adjusting key, a lifting standby control switch, a lighting lamp switch and an emergency brake switch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121684454.7U CN215043803U (en) | 2021-07-22 | 2021-07-22 | Emergency pilot power lifting platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121684454.7U CN215043803U (en) | 2021-07-22 | 2021-07-22 | Emergency pilot power lifting platform |
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| Publication Number | Publication Date |
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| CN215043803U true CN215043803U (en) | 2021-12-07 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121684454.7U Active CN215043803U (en) | 2021-07-22 | 2021-07-22 | Emergency pilot power lifting platform |
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| CN (1) | CN215043803U (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 |
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2021
- 2021-07-22 CN CN202121684454.7U patent/CN215043803U/en active Active
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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