CN113815880A - Emergency pilot power lifting and rescuing platform - Google Patents
Emergency pilot power lifting and rescuing platform Download PDFInfo
- Publication number
- CN113815880A CN113815880A CN202111316444.2A CN202111316444A CN113815880A CN 113815880 A CN113815880 A CN 113815880A CN 202111316444 A CN202111316444 A CN 202111316444A CN 113815880 A CN113815880 A CN 113815880A
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- Prior art keywords
- pilot
- cabin
- distress
- operation cabin
- lifting
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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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Structural Engineering (AREA)
- Transportation (AREA)
- Civil Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention discloses a power rescue platform for a pilot in danger, and belongs to the technical field of pilot rescue equipment. The aircraft comprises an operation cabin, a connecting arm component, a hoisting mechanism, a forward tilting door, a cabin door, an operating rod, a searchlight and a control console, wherein the hoisting mechanism is arranged in the operation cabin and is in sliding connection with the operation cabin through a linear sliding rail, the contact surface of the forward tilting door and the aircraft is made of soft packing materials to ensure the safety of the aircraft, power is supplied in the forward tilting door, the battery capacity is not less than 15Ah, the forward tilting door and the aircraft can be externally charged, the rescue platform can be operated under the night condition through the searchlight, and the operating rod can control the lifting and the inclination angle of the hoisting mechanism to realize the lifting of a pilot from the aircraft cabin. 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 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 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. The required operating personnel of rescue devices such as current emergency escape ladder, crane are more, and the cooperation is inconvenient between the device, causes pilot secondary damage easily, and rescue personnel's safety also is difficult to guarantee, can't satisfy distress pilot's emergent rescue demand, and the main problem of existence has:
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 rapid rescue of pilots is difficult to carry out;
2. the height of the lifesaving ladder is limited, and the lifesaving ladder can only meet the rescue requirements of pilots in lower cockpits;
3. the universality is poor, the cooperation between rescue devices such as an escape ladder, a crane and the like is inconvenient, and the operation requirement under the complex environmental condition is difficult to adapt.
In order to solve the above problems, it is necessary to develop a novel power-type rescue device to meet the needs of emergency pilots to get off the aircraft quickly for rescue.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a power rescue platform for pilots in distress, which aims to solve the problems in the background art.
In order to achieve the purpose, the invention provides the 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 a preferred 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 preferred technical solution of the present invention, the linkage arm member includes a main arm support, an ear seat, a first electric push rod, and a push rod support, the main arm support is hinged to one end of the main arm support through a pin, the ear seat is welded to the main arm support, one end of the first electric push rod is hinged to the ear seat through a pin, and an output end of the first electric push rod is hinged to the push rod support through a pin.
As a preferred technical scheme of the invention, the main arm support is of a Y-shaped structure, a traction seat is arranged at the top end of the main arm support, and an angle sensor is mounted on the first electric push rod.
As a preferred technical solution of the present invention, the lifting mechanism includes a base plate, a pedestal, an electric telescopic rod, a second electric push rod, and a boom, the pedestal is hinged to the base plate through a pin, the electric telescopic rod is mounted on the pedestal, one end of the second electric push rod is hinged to the base plate, and an output end of the second electric push rod is hinged to the electric telescopic rod, and the boom is mounted on an output end of the electric telescopic rod.
As a preferred technical solution of the present invention, the electric telescopic rod is provided with a hoop, the second electric push rod is hinged to the electric telescopic rod through the hoop, one end of the boom connected to the output end of the electric telescopic rod is of an open-loop structure, and is provided with a hand-tightening bolt, and the hand-tightening bolt is fastened to the output end of the electric telescopic rod.
As a preferred 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 preferred 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 connected with the operation cabin through the lock catch in a buckling manner.
As a preferred technical solution of the present invention, the operating rod has a circular key and a square key, which are used for controlling the lifting and the inclination angle of the lifting mechanism.
As a preferred technical scheme of the invention, the control console 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, and is used for realizing the control of the connecting arm and the lifting standby control.
Compared with the prior art, the invention provides a distress pilot power lifting platform, which has the following beneficial effects:
(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.
(4) According to the distress pilot power lifting platform, the contact surface of the forward tilting door and the airplane is made of soft packing materials so as to ensure the safety of the airplane; the power supply is built in, the battery capacity is not less than 15Ah, the external charging can be realized, the searchlight enables the lifting and rescuing platform to work under night conditions, the operating rod can control the lifting and the inclination angle of the lifting mechanism, and the pilot can lift off an airplane cockpit.
Drawings
FIG. 1 is a schematic structural view of a rescue platform for a pilot in distress according to the present invention;
FIG. 2 is an exploded view of FIG. 1 of a distress pilot powered lift platform according to the present invention;
FIG. 3 is a reverse view of FIG. 1 of a distress pilot powered lift platform according to the present invention;
FIG. 4 is an exploded view of FIG. 3 of a distress pilot powered lift platform according to the present invention;
FIG. 5 is a schematic structural view of a linkage arm member of a rescue platform of a pilot power crane in distress according to the present invention;
FIG. 6 is a schematic structural view of a lifting mechanism of a rescue platform powered by pilots in distress according to the present invention;
FIG. 7 is a schematic structural view of a forward tilting door of a rescue platform for a pilot in distress according to the present invention;
fig. 8 is a schematic structural view of a cabin door of a distress pilot powered rescue platform according to the present invention.
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 clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within 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 fastening 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 working principle and the using process of the invention are as follows: 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 and is used for controlling the lifting and the inclination angle of the lifting mechanism (3).
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, and is used for realizing the control of the connecting arm and the lifting standby control.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2021108334123 | 2021-07-22 | ||
| CN202110833412.3A CN113353277A (en) | 2021-07-22 | 2021-07-22 | Emergency pilot power lifting and rescuing platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN113815880A true CN113815880A (en) | 2021-12-21 |
| CN113815880B CN113815880B (en) | 2023-06-27 |
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Family Applications (2)
| 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 |
Family Applications Before (1)
| 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 |
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| CN (2) | CN113353277A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080149780A1 (en) * | 2006-12-22 | 2008-06-26 | 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 |
| 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 |
| CN111671562A (en) * | 2020-06-15 | 2020-09-18 | 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 |
-
2021
- 2021-07-22 CN CN202110833412.3A patent/CN113353277A/en active Pending
- 2021-11-08 CN CN202111316444.2A patent/CN113815880B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080149780A1 (en) * | 2006-12-22 | 2008-06-26 | 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 |
| 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 |
| CN111671562A (en) * | 2020-06-15 | 2020-09-18 | 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 |
Non-Patent Citations (1)
| Title |
|---|
| 潘静涵;苏迅;: "遇险飞行员救护的研究与进展", 解放军护理杂志, no. 17, pages 38 - 41 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113353277A (en) | 2021-09-07 |
| CN113815880B (en) | 2023-06-27 |
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