CN113815880B - Power suspension rescue platform for distress pilot - Google Patents
Power suspension rescue platform for distress pilot Download PDFInfo
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- CN113815880B CN113815880B CN202111316444.2A CN202111316444A CN113815880B CN 113815880 B CN113815880 B CN 113815880B CN 202111316444 A CN202111316444 A CN 202111316444A CN 113815880 B CN113815880 B CN 113815880B
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- pilot
- cabin
- distress
- lifting mechanism
- rod
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C23/00—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
- B66C23/18—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes
- B66C23/20—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes with supporting couples provided by walls of buildings or like structures
- B66C23/202—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes with supporting couples provided by walls of buildings or like structures with supporting couples provided from below, e.g. by floors of buildings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C23/00—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
- B66C23/18—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes
- B66C23/26—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes for use on building sites; constructed, e.g. with separable parts, to facilitate rapid assembly or dismantling, for operation at successively higher levels, for transport by road or rail
- B66C23/28—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes for use on building sites; constructed, e.g. with separable parts, to facilitate rapid assembly or dismantling, for operation at successively higher levels, for transport by road or rail constructed to operate at successively higher levels
- B66C23/30—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes for use on building sites; constructed, e.g. with separable parts, to facilitate rapid assembly or dismantling, for operation at successively higher levels, for transport by road or rail constructed to operate at successively higher levels with frameworks composed of telescopic elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C23/00—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
- B66C23/18—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes
- B66C23/36—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes mounted on road or rail vehicles; Manually-movable jib-cranes for use in workshops; Floating cranes
Abstract
The invention discloses a distress pilot power suspension platform, and belongs to the technical field of pilot rescue equipment. The invention comprises a working cabin, a connecting arm component, a lifting mechanism, a front tilting door, a cabin door, an operating rod, a searchlight and a control console, wherein the lifting mechanism is arranged in the working cabin and is in sliding connection with the working cabin through a linear sliding rail, the contact surface of the front tilting door and an airplane adopts soft package materials to ensure the safety of the airplane, the battery capacity is not less than 15Ah, the battery capacity can be externally charged, the searchlight enables the lifting platform to operate under night conditions, and the operating rod can control the lifting and the inclination angle of the lifting mechanism, so that a pilot lifts off the cockpit of the airplane. The power rescue platform for the pilot in distress has an autonomous power rescue function, can complete the rescue process of the pilot by only 1 rescue person, and can be used for the pilot in distress to quickly separate from a cabin.
Description
Technical Field
The invention belongs to the technical field of pilot rescue equipment, and particularly relates to a power rescue platform for a pilot in distress.
Background
The pilot in danger breaks away from the cabin rapidly and carries out timely rescue, which is an important link and means for guaranteeing the life of the pilot and promoting the flight safety. The required operating personnel of the rescue devices such as the existing rescue ladder, crane are more, the cooperation between the devices is inconvenient, the secondary injury of pilots is easy to cause, the safety of rescue personnel is difficult to ensure, the emergency rescue requirement of the pilots in distress cannot be met, and the main problems are that:
1. 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 pilot is difficult to rescue quickly;
2. the height of the rescue ladder is limited, so that the rescue requirement of pilots of lower cabins can be met;
3. the universality is poor, the coordination between rescue devices such as a rescue ladder and a crane is inconvenient, and the rescue device is difficult to adapt to the operation requirements under complex environmental conditions.
In view of the above, there is a need to develop new power-type special rescue equipment to meet the need of rapid escape rescue of a pilot in distress.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a distress pilot power hanging and rescuing platform which solves the problems in the background art.
In order to achieve the above purpose, the present invention provides the following technical solutions: the utility model provides a pilot power hangs and rescue platform in distress, includes operation cabin, link arm component, lifting mechanism, anteverted door, hatch door, action bars, searchlight and control cabinet, the right side of operation cabin is equipped with the installation cavity, the one end of link arm component is installed in the installation cavity, lifting mechanism installs in the operation cabin, and has laid the linear slide rail between lifting mechanism bottom and the operation cabin in the bottom, and lifting mechanism and operation cabin pass through linear slide rail sliding connection, the punching plate has been laid to the interior bottom of operation cabin, install quick press tongs on the lifting mechanism, and in the punching plate is pressed in to the pressure head portion of quick press tongs, make lifting mechanism and operation cabin lock solid connect, the anteverted door passes through the door hinge to be installed in the left side of operation cabin, hatch door sliding mounting is in the front side of operation cabin, action bars and searchlight are installed respectively in the interior top of operation cabin, and action bars and lifting mechanism electric connection, the control cabinet is installed on the inside wall of operation cabin, link arm component and lifting mechanism electric connection with the control cabinet.
As an optimal technical scheme of the invention, the operation cabin is of a net frame structure, and the bottom of the operation cabin is fixedly provided with a universal wheel with a brake.
As a preferable technical scheme of the invention, the connecting arm component comprises a main arm support, an ear seat, a first electric push rod and a push rod support, wherein the main arm support is hinged with one end of the main arm support through a pin shaft, the ear seat is welded on the main arm support, one end of the first electric push rod is hinged with the ear seat through a pin shaft, and the output end of the first electric push rod is hinged with the push rod support through a pin shaft.
As a preferable technical scheme of the invention, the main arm frame is of a Y-shaped structure, the top end of the main arm frame is provided with a traction seat, and the first electric push rod is provided with an angle sensor.
As a preferable technical scheme of the invention, the lifting mechanism comprises a base plate, a pedestal, an electric telescopic rod, a second electric push rod and a suspension arm, wherein the pedestal is hinged on the base plate through a pin shaft, the electric telescopic rod is arranged on the pedestal, one end of the second electric push rod is hinged on the base plate, the output end of the second electric push rod is hinged with the electric telescopic rod, and the suspension arm is arranged on the output end of the electric telescopic rod.
As a preferable technical scheme of the invention, the electric telescopic rod is provided with the hoop, the second electric push rod is hinged with the electric telescopic rod through the hoop, one end of the suspension arm connected with the output end of the electric telescopic rod is of an open-loop structure, and the suspension arm is provided with a hand-screwed bolt which is tightly connected with the output end of the electric telescopic rod.
As a preferable technical scheme of the invention, the forward tilting door comprises a buffer cross rod, a gas spring and a deflector rod module, wherein one end of the gas spring is hinged on the buffer cross rod, and the output end of the gas spring is hinged with the deflector rod module.
As a preferable technical scheme of the invention, the cabin door comprises a framework, a guide rod and a lock catch, wherein the guide rod and the lock catch are sequentially arranged on the framework, and the cabin door is in buckling connection with the operation cabin through the lock catch.
As a preferable technical scheme of the invention, the operating rod is provided with a round key and a square key, and is used for controlling the lifting and tilting angles of the lifting mechanism.
As a preferable technical scheme of the invention, the control console mainly comprises a main power switch, a connecting arm adjusting key, a lifting standby control switch, an illuminating lamp switch and an emergency brake switch, and is used for realizing control of the connecting arm and lifting standby control.
Compared with the prior art, the invention provides a distress pilot power hanging and rescuing platform, which has the following beneficial effects:
(1) The power rescue platform for the pilot in distress is used for enabling the pilot in distress to quickly separate from a cabin, has an autonomous power rescue function, can complete the rescue process of the pilot by only 1 rescue personnel, and is simple in operation.
(2) The power rescue platform for the pilot in distress has a dynamic balance function, and is always in a horizontal state in the rescue process, so that the safety of rescue workers is ensured, and the contact surface of the power rescue platform for the pilot in distress and the aircraft is made of soft package materials, so that the safety of the aircraft is ensured.
(3) The power rescue platform for the pilot in distress has the maximum operation height of not less than 6m and is applicable to a wide range of models.
(4) The contact surface of the forward tilting door and the aircraft is made of soft package materials so as to ensure the safety of the aircraft; the power supply is built-in, the battery capacity is not less than 15Ah, the power supply can be externally connected for charging, the searchlight enables the rescue platform to work under the night condition, and the operating rod can control the lifting and tilting angle of the lifting mechanism, so that the pilot can lift off the cabin of the aircraft.
Drawings
FIG. 1 is a schematic diagram of a distress pilot powered rescue platform according to the present invention;
FIG. 2 is an exploded view of FIG. 1 of a distress pilot powered rescue platform in accordance with the present invention;
FIG. 3 is a reverse view of FIG. 1 of a distress pilot powered rescue platform of the present invention;
FIG. 4 is an exploded view of FIG. 3 of a distress pilot powered rescue platform in accordance with the present invention;
FIG. 5 is a schematic view of the structure of the arm members of the distress pilot powered rescue platform of the present invention;
FIG. 6 is a schematic view of a lifting mechanism of a distress pilot powered rescue platform according to the present invention;
FIG. 7 is a schematic view of the structure of a forward tilting door of a distress pilot powered rescue platform according to the present invention;
fig. 8 is a schematic diagram of a cabin door structure of a distress pilot power rescue platform according to the present invention.
In the figure: 1. an operation cabin; 2. a link arm member; 3. a lifting mechanism; 4. a forward tilting door; 5. a cabin door; 6. an operation lever; 7. a searchlight; 8. a console; 9. a mounting cavity; 10. a linear slide rail; 11. punching a plate; 12. quick pressing pliers; 13. a universal wheel; 14. a main arm support; 15. a main arm support; 16. an ear seat; 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 cross bar; 29. a gas spring; 30. a deflector rod module; 31. a skeleton; 32. a guide rod; 33. and (5) locking.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Referring to fig. 1-8, a distress pilot power rescue platform comprises a working cabin 1, a connecting arm component 2, a lifting mechanism 3, a front tilting door 4, a cabin door 5, an operating rod 6, a searchlight 7 and a control console 8, wherein an installation cavity 9 is arranged on the right side of the working cabin 1, one end of the connecting arm component 2 is installed in the installation cavity 9, the lifting mechanism 3 is installed in the working cabin 1, a linear slide rail 10 is paved between the bottom of the lifting mechanism 3 and the inner bottom of the working cabin 1, the lifting mechanism 3 and the working cabin 1 are in sliding connection through the linear slide rail 10, a punching plate 11 is paved at the inner bottom of the working cabin 1, a quick press clamp 12 is installed on the lifting mechanism 3, the pressing head of the quick press clamp 12 is pressed into the punching plate 11, the lifting mechanism 3 is connected with the working cabin 1, the front tilting door 4 is installed on the left side of the working cabin 1 through a door hinge, the cabin door 5 is in sliding installation on the front side of the working cabin 1, the operating rod 6 and the searchlight 7 are respectively installed in the working cabin 1, the inner side of the lifting mechanism 6 and the lifting mechanism 3 are electrically connected with the control console 8, and the inner side wall of the lifting mechanism 3 is electrically connected with the control console 8.
As a specific technical scheme of this embodiment, the working cabin 1 is a net frame structure, and a universal wheel 13 with a brake is fixedly installed at the bottom of the working cabin.
In this embodiment, as shown in fig. 1 to 4, the net frame structure is advantageous for lightening the working cabin 1, and the rescue platform can be moved in any direction by a rescuer by using the universal wheel 13 with the brake, and can be kept in a stopped state by using the brake of the universal wheel 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 mount 16, a first electric putter 17, and a putter support 18, where the main arm support 15 is hinged to one end of the main arm support 14 through a pin, the ear mount 16 is welded to the main arm support 14, one end of the first electric putter 17 is hinged to the ear mount 16 through a pin, and an output end of the first electric putter is hinged to the putter support 18 through a pin.
In this embodiment, as shown in fig. 5, the first electric push rod 17 and the angle sensor 20 are provided, and the electric push rod can work in two modes of manual adjustment and automatic adjustment, and in the manual mode, the angle of the connecting arm can be adjusted, so that the electric push rod can be in butt joint with the suspension arm of the emergency vehicle.
As a specific technical solution of this embodiment, the main arm frame 14 is in a Y-shaped structure, a traction seat 19 is disposed at the top end of the main arm frame 14, and an angle sensor 20 is mounted on the first electric push rod 17.
In this embodiment, as shown in fig. 5, in the automatic mode, the angle of the connection arm can be automatically adjusted by using the angle sensor 20, and automatic dynamic balance during the operation of the rescue platform is achieved.
As a specific technical solution of this embodiment, the lifting mechanism 3 includes a base 21, a pedestal 22, an electric telescopic rod 23, a second electric push rod 24, and a boom 25, where the pedestal 22 is hinged to the base 21 through a pin, the electric telescopic rod 23 is mounted on the pedestal 22, one end of the second electric push rod 24 is hinged to the base 21, and the output end of the second electric push rod is hinged to the electric telescopic rod 23, and the boom 25 is mounted on the output end of the electric telescopic rod 23.
In this embodiment, as shown in fig. 6, the rescue personnel can electrically control and adjust the pitch angle and the telescopic length of the lifting mechanism 3 through the operation rod 6, lift the pilot away from the cabin, and control the lifting mechanism 3 to move left and right in the operation cabin 1 through the linear slide rail 10, and realize automatic locking by pressing the quick clamp 12 into different through holes on the punching plate 11.
As a specific technical scheme of this embodiment, the electric telescopic rod 23 is provided with a hoop 26, the second electric push rod 24 is hinged to the electric telescopic rod 23 through the hoop 26, one end of the boom 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 mounted thereon, and is fastened and connected with the output end of the electric telescopic rod 23 through the hand-screwed bolt 27.
In this embodiment, as shown in fig. 6, the rescuer can manually control the rotation of the boom 25, and after rotating it into place, can be manually locked via manual tightening of the bolt 27.
As a specific technical solution of this embodiment, the front tilting door 4 includes a buffer cross bar 28, a gas spring 29, and a lever module 30, where one end of the gas spring 29 is hinged to the buffer cross bar 28, and an output end of the gas spring is hinged to the lever module 30.
In this embodiment, as shown in fig. 7, by manually controlling the lever module 30, under the action of the gas spring 29, the forward tilting door 4 can be opened or closed, and the opening angle of the forward tilting door 4 is adjusted, and the buffer cross bar 28 can protect the surface of the aircraft, so that the rescue platform is close to the cabin of the aircraft as much as possible, which is beneficial for rescue workers to complete quick escape rescue of pilots.
As a specific technical scheme of this embodiment, the cabin door 5 includes a skeleton 31, a guide rod 32 and a lock catch 33, the guide rod 32 and the lock catch 33 are sequentially installed on the skeleton 31, and the cabin door 5 is buckled and connected with the operation cabin 1 through the lock catch 33.
In this embodiment, as shown in fig. 8, the rescue worker wears the seat belt before entering the cabin, closes the cabin door 5 at the first time after entering the cabin, checks whether the lock catch 33 is fastened, and then hangs the seat belt at a designated position of the cabin.
As a specific technical solution of this embodiment, the operating lever 6 has a circular key and a square key, which are used to control the lifting and tilting angle of the lifting mechanism 3.
In this embodiment, as shown in fig. 1 to 4, the operation lever 6 can be pushed forward and pulled backward, the square key and the round key are pressed for a long time, the extension and shortening of the lifting mechanism 3 can be achieved, the forward pushing and pulling backward of the operation lever 6 can be achieved, the forward tilting and backward tilting of the lifting mechanism 3 can be achieved, and when adjusted to a proper position, pushing of the operation lever 6 is stopped.
As a specific technical scheme of this embodiment, the console 8 mainly includes a main power switch, a link arm adjusting key, a lifting standby control switch, an illumination lamp switch, and an emergency brake switch, which are used for implementing control of the link arm and lifting standby control.
In this embodiment, as shown in fig. 1 to 4, the console 8 further includes an automatic leveling switch, and in case of failure of the operation lever 6, standby control of the lifting mechanism 3 can be achieved, and when an emergency occurs, the emergency braking button can achieve complete machine emergency braking, lifting emergency braking and link arm emergency braking, thereby improving safety of operation of the lifting platform.
The working principle and the using flow of the invention are as follows: when the power rescue platform is used, rescue workers carry medical rescue equipment to quickly climb on the power rescue platform, the rescue platform is controlled to be close to an aircraft cabin through a hydraulic arm manipulator of the rescue vehicle, the injury condition of a pilot is checked, the rescue scheme of the pilot is determined, the hook on the lifting mechanism 3 is utilized to connect flying clothes worn by the pilot, the rescue workers adjust the pitching angle and the telescopic length of the lifting mechanism 3 through the operating rod 6, the pilot is adjusted away from the cabin, the hand-screwing bolt 27 on the suspension arm 25 is loosened, the pilot is brought away from the cabin by the adjusting angle, and the pilot can be stably and quickly lowered to the ground.
In conclusion, the distress pilot power rescue platform has an autonomous power rescue function, can complete the rescue process of pilots only by 1 rescue staff, and can be used for rapidly separating the pilots from the cockpit; the platform has a dynamic balance function, and the rescue platform is always in a horizontal state in the rescue process, so that the safety of rescue workers is ensured, and the contact surface of the platform and an airplane is made of soft package materials, so that the safety of the airplane is ensured; the maximum working height is not less than 6m, and the machine is wide in applicable machine type.
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 one … …" does not exclude the presence of other like 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 understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides a pilot power of distress hangs and rescue platform, includes operation cabin (1), link arm component (2), lifting mechanism (3), anteverted 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 lifting mechanism (3) is installed in the operation cabin (1), a linear slide rail (10) is paved between the bottom of the lifting mechanism (3) and the inner bottom of the operation cabin (1), the lifting mechanism (3) and the operation cabin (1) are in sliding connection through the linear slide rail (10), a punching plate (11) is paved at the inner bottom of the operation cabin (1), a quick pressing clamp (12) is installed on the lifting mechanism (3), the pressing head part of the quick pressing clamp (12) is pressed into the punching plate (11), the lifting mechanism (3) and the operation cabin (1) are connected, the front 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 connection with the front side of the operation cabin (1), the operation rod (6) and the searchlight (7) are respectively installed on the inner top of the operation cabin (1), and the operation rod (6) is electrically connected with the lifting mechanism (8) and the control arm (8) is electrically connected with the lifting mechanism (3);
the operation cabin (1) is of a net frame structure, and a universal wheel (13) with a brake is fixedly arranged at the bottom of the operation cabin;
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 with one end of the main arm support (14) through a pin shaft, the ear seat (16) is welded on the main arm support (14), one end of the first electric push rod (17) is hinged with the ear seat (16) through a pin shaft, and the output end of the first electric push rod is hinged with the push rod support (18) through a pin shaft.
2. A distress pilot powered rescue platform as defined in claim 1 wherein: the main arm frame (14) is of a Y-shaped structure, a traction seat (19) is arranged at the top end of the main arm frame (14), and an angle sensor (20) is arranged on the first electric push rod (17).
3. A distress pilot powered rescue platform as defined in claim 1 wherein: the lifting mechanism (3) comprises a base plate (21), a pedestal (22), an electric telescopic rod (23), a second electric push rod (24) and a suspension arm (25), wherein the pedestal (22) is hinged on the base plate (21) through a pin shaft, the electric telescopic rod (23) is installed on the pedestal (22), one end of the second electric push rod (24) is hinged on the base plate (21), the output end of the second electric push rod is hinged with the electric telescopic rod (23), and the suspension arm (25) is installed on the output end of the electric telescopic rod (23).
4. A distress pilot powered rescue platform as defined in claim 3 wherein: install hoop (26) on electric telescopic handle (23), second electric putter (24) are articulated with electric telescopic handle (23) through hoop (26), the one end that davit (25) are connected with the output of electric telescopic handle (23) is open loop structure, and installs on it and twist bolt (27), through twist bolt (27) and the output fastening connection of electric telescopic handle (23).
5. A distress pilot powered rescue platform as defined in claim 1 wherein: the forward tilting door (4) comprises a buffer cross rod (28), a gas spring (29) and a deflector rod module (30), wherein 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 deflector rod module (30).
6. A distress pilot powered rescue platform as defined in claim 1 wherein: the cabin door (5) comprises a framework (31), a guide rod (32) and a lock catch (33), wherein the guide rod (32) and the lock catch (33) are sequentially arranged 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).
7. A distress pilot powered rescue platform as defined in claim 1 wherein: the operating rod (6) is provided with a round key and a square key, and is used for controlling the lifting and tilting angles of the lifting mechanism (3).
8. A distress pilot powered rescue platform as defined in claim 1 wherein: the control console (8) mainly comprises a main power switch, a connecting arm adjusting key, a lifting standby control switch, an illuminating lamp switch and an emergency brake switch, and is used for realizing control of the connecting arm and lifting standby control.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110833412.3A CN113353277A (en) | 2021-07-22 | 2021-07-22 | Emergency pilot power lifting and rescuing platform |
| CN2021108334123 | 2021-07-22 |
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| Publication Number | Publication Date |
|---|---|
| CN113815880A CN113815880A (en) | 2021-12-21 |
| CN113815880B true CN113815880B (en) | 2023-06-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110833412.3A Pending CN113353277A (en) | 2021-07-22 | 2021-07-22 | Emergency pilot power lifting and rescuing platform |
| CN202111316444.2A Active CN113815880B (en) | 2021-07-22 | 2021-11-08 | Power suspension rescue platform for distress pilot |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202110833412.3A Pending CN113353277A (en) | 2021-07-22 | 2021-07-22 | Emergency pilot power lifting and rescuing platform |
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Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204340826U (en) * | 2014-12-23 | 2015-05-20 | 中国人民解放军空军南苑场站专用车辆技术保障队 | A kind of aircraft accident reserved vehicle |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7481290B2 (en) * | 2006-12-22 | 2009-01-27 | Pendzich Jerome S | Vertical lift vehicle |
| CN202322243U (en) * | 2011-10-19 | 2012-07-11 | 中国人民解放军空军航空医学研究所 | Rescue equipment for pilot in danger |
| CN111671562B (en) * | 2020-06-15 | 2022-05-10 | 中国人民解放军海军特色医学中心 | Quick pilot fixing and rescuing device |
| CN215043803U (en) * | 2021-07-22 | 2021-12-07 | 中国人民解放军空军军医大学 | Emergency pilot power lifting platform |
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2021
- 2021-07-22 CN CN202110833412.3A patent/CN113353277A/en active Pending
- 2021-11-08 CN CN202111316444.2A patent/CN113815880B/en active Active
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204340826U (en) * | 2014-12-23 | 2015-05-20 | 中国人民解放军空军南苑场站专用车辆技术保障队 | A kind of aircraft accident reserved vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113353277A (en) | 2021-09-07 |
| CN113815880A (en) | 2021-12-21 |
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