A helicopter all-visibility hatch

Abstract

The application provides a helicopter full-view cabin door, and belongs to the technical field of helicopter cabin doors. Specifically, the helicopter full-view cabin door comprises a door plate and a viewing window. The viewing window bulges towards the outside of the helicopter cabin. The viewing window is composed of two transparent units, and the two transparent units are rotationally connected to the door plate. A limiting and fixing assembly is slidably mounted in the door plate. An adjusting block is fixed on the limiting and fixing assembly. A driving assembly is connected to the output end of the limiting and fixing assembly through a connecting rod. The driving assembly is used to drive the limiting and fixing assembly to approach the edge of the transparent unit to limit the rotation of the transparent unit, or drive the limiting and fixing assembly to move away from the transparent unit to release the limitation on the transparent unit. A breaking assembly is used to break the connecting rod. The adjusting block is manually operated to drive the limiting and fixing assembly to move away from the transparent unit to release the limitation on the transparent unit after the connecting rod is broken. The processing scheme improves the escape probability of the helicopter after a safety accident.

Description

Technical Field

[0001] The present application relates to the field of helicopter doors, and in particular to a helicopter full-view door. Background Art

[0002] Helicopter doors are typically traditional metal structures with limited window area, significantly restricting the occupants' ability to observe the external environment. During missions such as rescue, reconnaissance, and sightseeing, the narrow window makes it difficult for operators to fully understand the surrounding situation, hindering efficient mission execution.

[0003] The full-view cabin door in the prior art is obtained by enlarging the window area on the helicopter cabin door. The material used for the window is a transparent composite material, which has the advantage of high strength.

[0004] When an accident occurs during a helicopter mission and the helicopter needs to break out of the door, breaking through the high-strength transparent composite material becomes a practical problem. Due to the limited range of movement of the personnel in the cabin, they are unable to forcefully break through the windows made of transparent composite materials, thus delaying their survival time. Summary of the Invention

[0005] In view of this, the present application provides a helicopter full-view cabin door, which aims to overcome the problems of existing helicopter cabin doors with a small visual range and the difficulty of breaking and opening the visible part in an emergency, so as to improve the probability of escape after a safety accident occurs in the helicopter.

[0006] The present application provides a helicopter full-view door that adopts the following technical solutions:

[0007] A helicopter full-view cabin door, the cabin door body comprising a door panel and a visual window, the visual window being provided on the door panel and bulging outward from the helicopter cabin, the visual window being composed of two transparent units, which, when joined together, form a complete visual window, and the two transparent units being rotatably connected to the door panel;

[0008] A limit fixing assembly is slidably mounted in the door panel, an adjustment block is fixed to the limit fixing assembly, the adjustment block extends from the limit fixing assembly toward the interior of the helicopter cockpit, and a sliding groove is provided on the inner side of the door panel for the adjustment block to extend and slide;

[0009] A driving assembly, wherein the output end of the driving assembly is connected to the limiting and fixing assembly via a connecting rod, and is used to drive the limiting and fixing assembly to approach the edge of the transparent unit to limit the rotation of the transparent unit, or to drive the limiting and fixing assembly away from the transparent unit to release the restriction on the transparent unit;

[0010] The breaking assembly is used to destroy the connecting rod, and the adjusting block is used to be manually operated after the connecting rod is destroyed to drive the limiting and fixing assembly away from the transparent unit to release the restriction on the transparent unit.

[0011] Optionally, the helicopter full-view door further comprises a connecting splint, wherein the connecting splint is wrapped around the edge of the transparent unit, and a cavity is formed between the connecting splint and the edge of the transparent unit;

[0012] Each of the two transparent units is correspondingly provided with a limit fixing assembly, and the limit fixing assembly includes a mounting frame and a limit column. The mounting frame is slidably connected to the door panel, and the mounting frame is located at the outer periphery of the transparent unit. There are multiple limit columns, and multiple limit columns are symmetrically installed on the mounting frame. Limit holes are opened at positions corresponding to the connecting splints and the limit columns, and the limit columns are used to extend into the limit holes.

[0013] Optionally, a sliding groove perpendicular to the mating surfaces of the two transparent units is opened on the door panel at a side of the mounting frame away from the transparent unit, and the adjustment block is fixedly connected to the mounting frame.

[0014] Optionally, the driving component includes:

[0015] A rotating handle, the rotating handle being rotatably connected to the door panel;

[0016] A connecting rod driving member, the connecting rod driving member is used to drive the movement of the limiting fixing assembly on one side;

[0017] A gear driving member, the gear driving member is used to drive the movement of the limiting fixing assembly on the other side;

[0018] The connecting rod driving member and the gear driving member are both driven by the rotating handle.

[0019] Optionally, the connecting rod driving member includes:

[0020] a fixing rod, the fixing rod being fixedly connected to the rotating handle and being located inside the door panel;

[0021] A rotating rod, one end of which is rotatably connected to the end of the fixed rod, a point between the two ends of the rotating rod is rotatably connected to the door panel, and the other end of the rotating rod is fixedly connected to the mounting bracket through the connecting rod.

[0022] Optionally, the gear driving member comprises a plurality of gears and a rack, the number of gears is even, the rotating handle is provided with a gear tooth, the plurality of gears are arranged adjacently, and the two adjacent gears are engaged with each other, the gears at both ends of the plurality of gears arranged adjacently are engaged with the rotating handle and the rack respectively, and one end of the rack is fixedly connected with the other mounting frame through the connecting rod.

[0023] Optionally, the breaking assembly comprises:

[0024] A breaking knife is arranged in the door plate and located on the side of the connecting rod away from the rotating handle, and the blade of the breaking knife is opposite to the connecting rod;

[0025] A driving block is fixedly connected with the breaking knife, a driving groove is arranged on the door plate at the position corresponding to the breaking knife, the driving groove is perpendicular to the connecting rod, and the driving block slides in the driving groove.

[0026] Optionally, the door plate is provided with a door handle and a door lock.

[0027] Optionally, the opposite sides of the connecting clamping plate and the mounting frame are both provided with sealing rubber strips.

[0028] In summary, the present application has the following beneficial technical effects:

[0029] The cabin personnel can observe the environment outside the cabin through the visual window when performing the flight task, the visual window can further widen the visual field range by bulging outwards of the door plate, the limiting column and the limiting hole are used in cooperation to enable the visual window to be firmly limited on the door plate during the flight, the temperature in the cabin is not easy to lose under the action of the sealing rubber strip, and the wind noise can be reduced, the mounting frame can be simply and quickly lifted and landed by driving the connecting rod driving member and the gear driving member, the cooperation of the limiting column and the limiting hole is further controlled, the breaking knife can be manually driven to cut the connecting rod when the cabin door cannot be normally opened due to the accident of the aircraft, then the limiting column is moved out of the limiting hole through the adjusting block, and then the transparent unit can be opened to escape, and the escape probability of the cabin personnel is effectively improved. BRIEF DESCRIPTION OF DRAWINGS

[0030] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings needed to be used in the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative labor.

[0031] Figure 1 A three-dimensional structure schematic diagram of a helicopter full-view cabin door disclosed by the embodiments of the present application is shown in the figure.

[0032] Figure 2 This is a partial structural cross-sectional view of a full-view door for a helicopter disclosed in an embodiment of the present application;

[0033] Figure 3 for Figure 2 A magnified schematic diagram of part A;

[0034] Figure 4 This is a three-dimensional schematic diagram of the internal structure of a helicopter full-view door disclosed in an embodiment of the present application;

[0035] Figure 5 A three-dimensional cross-sectional view of a helicopter full-view door disclosed in an embodiment of the present application from another perspective;

[0036] Figure 6 for Figure 5 Schematic diagram of the enlarged portion B.

[0037] Explanation of the accompanying reference numerals: 1. Door body; 11. Door panel; 111. Door handle; 112. Door lock; 113. Drive slot; 114. Slide slot; 12. Visual window; 121. Transparent unit; 2. Connecting splint; 21. Limiting hole; 3. Limiting fixing assembly; 31. Mounting frame; 32. Limiting column; 33. Adjusting block; 4. Driving assembly; 41. Turning handle; 42. Connecting rod driving member; 421. Fixed rod; 422. Turning rod; 423. Connecting rod; 43. Gear driving member; 431. Gear; 432. Rack; 5. Demolition assembly; 51. Demolition knife; 52. Driving block; 6. Sealing strip. DETAILED DESCRIPTION

[0038] The embodiments of the present application are described in detail below with reference to the accompanying drawings.

[0039] The following describes the embodiments of the present application through specific examples, and those skilled in the art can easily understand other advantages and effects of the present application from the contents disclosed in this specification. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. The present application can also be implemented or applied through other different specific embodiments, and the details in this specification can also be modified or changed in various ways based on different viewpoints and applications without departing from the spirit of the present application. It should be noted that, in the absence of conflict, the features in the following embodiments and embodiments can be combined with each other. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without making creative work are within the scope of protection of this application.

[0040] It should be noted that various aspects of the embodiments within the scope of the appended claims are described below. It should be apparent that the aspects described herein can be embodied in a wide variety of forms, and any specific structure and / or function described herein is merely illustrative. Based on this application, it should be understood by those skilled in the art that an aspect described herein can be implemented independently of any other aspect, and two or more of these aspects can be combined in various ways. For example, any number of aspects described herein can be used to implement an apparatus and / or practice a method. In addition, other structures and / or functionalities other than one or more of the aspects described herein can be used to implement this apparatus and / or practice this method.

[0041] It should also be noted that the illustrations provided in the following embodiments are only schematic illustrations of the basic concept of the present application. The illustrations only show components related to the present application and are not drawn according to the number, shape and size of components in actual implementation. In actual implementation, the type, quantity and proportion of each component can be changed at will, and the component layout type may also be more complicated.

[0042] Additionally, in the following description, specific details are provided to provide a thorough understanding of the examples. However, one skilled in the art will appreciate that the aspects described can be practiced without these specific details.

[0043] like Figures 1 to 6 As shown, an embodiment of the present application provides a helicopter full-view door, comprising:

[0044] like Figure 1 As shown, the cabin door body 1 includes a door panel 11 and a visual window 12. The visual window 12 is provided on the door panel 11. The visual window 12 is curved and bulges toward the outside of the helicopter cabin. The visual window 12 is composed of two transparent units 121. The two transparent units 121 are connected to form a complete visual window 12. The two transparent units 121 are rotatably connected to the door panel 11. The door panel 11 is provided with a door handle 111 and a door lock 112. The door lock 112 can firmly lock the cabin door body 1 to the aircraft cabin to improve safety. The door handle 111 can facilitate the opening and closing of the cabin door body 1.

[0045] In an embodiment of the present application, the transparent unit 121 is rotatably connected to the door panel 11 through a rotating shaft. The rotating shaft is embedded in the door panel 11, and a damping is provided at the rotating shaft. The rotation connection position is located on the opposite side of the two symmetrically arranged transparent units 121. The close ends of the two transparent units 121 abut against each other on the symmetry axis. On the door panel 11, an avoidance embedding groove is opened at the position of the rotating shaft, thereby ensuring that the transparent unit 121 can be opened to the outside of the cabin without obstacles.

[0046] like Figure 1、 Figure 2 、 Figure 3 and Figure 4 As shown, the limiting and fixing component 3 is slidably installed in the door panel 11, and an adjustment block 33 is fixed on the limiting and fixing component 3. The adjustment block 33 extends from the limiting and fixing component 3 toward the inside of the helicopter cockpit, and a sliding groove 114 is provided on the inner side of the door panel 11 for the adjustment block 33 to extend and slide.

[0047] like Figure 4 As shown, the driving component 4, the output end of the driving component 4 and the limiting and fixing component 3 are connected by a connecting rod 423, which is used to drive the limiting and fixing component 3 to approach the edge of the transparent unit 121 to limit the rotation of the transparent unit 121, or drive the limiting and fixing component 3 away from the transparent unit 121 to release the restriction on the transparent unit 121.

[0048] like Figure 5 and Figure 6 As shown, the demolition component 5 is used to destroy the connecting rod 423, and the adjustment block 33 is used to be manually operated to drive the limiting and fixing component 3 away from the transparent unit 121 to release the restriction on the transparent unit 121 after the connecting rod 423 is destroyed.

[0049] The visual window 12, which is composed of two transparent units 121, bulges to one side, allowing the personnel in the cabin to observe the external environment in full view when performing flight missions. The connecting splint 2 rotates the transparent unit 121 to the door panel 11, and the visual window 12 composed of the transparent units 121 can be opened outward by rotating it, which not only further increases the field of view, but also can be used for escape in the event of an accident. The limit fixing component 3 is used to fix the visual window 12 to the door panel 11. When the visual window 12 is not needed to be opened, it can ensure the safety of the personnel in the cabin during the flight and further reduce wind noise and temperature loss. The setting of the adjustment block 33 can manually directly release the fixed limit, so that after an accident occurs in the aircraft, the personnel in the cabin can open the visual window 12 more quickly and open the escape passage for emergency escape, effectively improving the emergency escape probability of the personnel in the cabin.

[0050] like Figure 2 and Figure 3 As shown, the helicopter full-view door also includes a connecting splint 2. The connecting splint 2 is made of metal material, and the connecting splint 2 is wrapped around the edge of the transparent unit 121, and a cavity is formed between the connecting splint 2 and the edge of the transparent unit 121; in the embodiment of the present application, the connecting splint 2 is made of stainless steel alloy, and the connecting splint 2 has the same edge contour shape as the transparent unit 121, and the connecting splint 2 is wrapped around the edge of the transparent unit 121 by bonding.

[0051] like Figures 2 to 4As shown, each of the two transparent units 121 is correspondingly provided with a limiting fixing component 3, and each of the two limiting fixing components 3 is correspondingly provided with an adjustment block 33 and a connecting rod 423. The limiting fixing component 3 includes a mounting bracket 31 and a limiting column 32. The mounting bracket 31 is slidably connected to the door panel 11, and the output end of the driving component 4 is connected to the mounting bracket 31 through a connecting rod 423. The edge shape of the mounting bracket 31 is the same as that of the transparent unit 121. The mounting bracket 31 is located at the outer periphery of the transparent unit 121. There are multiple limiting columns 32, and multiple limiting columns 32 are symmetrically fixed on the mounting bracket 31. The limiting columns 32 are installed on the side of the mounting bracket 31 facing the transparent unit 121. A limiting hole 21 is opened at the position corresponding to the connecting splint 2 and the limiting column 32. The limiting column 32 is used to extend into the limiting hole 21. A cavity is formed between the connecting splint 2 and the edge of the transparent unit 121 to provide space for accommodating the limiting column 32.

[0052] By moving the mounting bracket 31 through the driving component 4 or manually controlling the adjustment block 33, the limiting column 32 can be inserted into the limiting hole 21, so that the limiting column 32 is located in the cavity formed between the connecting splint 2 and the visual window 12 to limit and fix the visual window 12, thereby firmly limiting the visual window 12 on the door panel 11. When the mounting bracket 31 drives the limiting column 32 to move out of the limiting hole 21, the transparent unit 121 can be rotated by the rotating shaft embedded in the door panel 11.

[0053] Regarding the setting of the sliding groove 114 and the adjustment block 33: the sliding groove 114 perpendicular to the mating surfaces of the two transparent units 121 is opened on the side of the mounting frame 31 on the door panel 11 away from the transparent unit 121, and the adjustment block 33 is fixedly connected to the mounting frame 31.

[0054] In this embodiment, a sealing strip 6 is provided on the opposite side of the connecting plate 2 and the mounting bracket 31. The sealing strip 6 is bonded to one side of the mounting bracket 31. The sealing strip 6 prevents rapid temperature loss within the chamber, reduces wind noise, and reduces hard contact damage to the transparent unit caused by bumps.

[0055] like Figure 4 As shown, the driving assembly 4 includes:

[0056] A rotating handle 41 is rotatably connected to the door panel 11 . The rotating handle 41 is located on a side of the door panel 11 facing the interior of the cockpit.

[0057] The connecting rod driving member 42 is used to drive the movement of the limiting and fixing assembly 3 on one side.

[0058] The gear driving member 43 is used to drive the movement of the limiting and fixing component 3 on the other side.

[0059] The connecting rod driving member 42 and the gear driving member 43 are both driven by the rotating handle 41 .

[0060] After the handle 41 is rotated, the fixing rod 421 is driven to rotate, and the fixing rod 421 and the connecting rod 423 are rotatably connected, so that one end of the connecting rod 423 can be driven to rotate along the rotation connection point between the connecting rod 423 and the door panel 11 as the center of the circle, and then the other end of the rotating rod 422 is driven to rotate in the opposite direction, thereby driving the connecting rod 423 to move along the length direction parallel to the slide groove 114, and finally removing the limiting column 32 from the limiting hole 21, which has the advantages of easy operation and simple structure.

[0061] The connecting rod driving member 42 includes:

[0062] A fixing rod 421 is fixedly connected to the rotating handle 41 and is located inside the door panel 11 .

[0063] The rotating rod 422 has one end that is rotatably connected to the end of the fixed rod 421 , a point between the two ends of the rotating rod 422 is rotatably connected to the door panel 11 , and the other end of the rotating rod 422 is fixedly connected to the mounting bracket 31 through the connecting rod 423 .

[0064] Regarding the specific setting of the connecting rod: the cross-sectional area of ​​the connecting rod 423 is smaller than the cross-sectional areas of the fixed rod 421 and the rotating rod 422, one end of the connecting rod 423 is rotatably connected to the end of the rotating rod 422, and the other end is fixedly connected to the adjustment block 33.

[0065] The gear drive member 43 includes a plurality of gears 431 and a rack 432. The number of the gears 431 is an even number. In this embodiment, there are four gears 431 and one rack 432. The rotating handle 41 is provided with gear teeth. The plurality of gears 431 are arranged adjacent to each other, and two adjacent gears 431 are meshed with each other. The gears 431 at both ends of the plurality of adjacently arranged gears 431 are respectively meshed with the rotating handle 41 and the rack 432. One end of the rack 432 is fixedly connected to the other mounting bracket 31 via the connecting rod 423.

[0066] The personnel in the cabin can simultaneously control the movement of the connecting rod driving member 42 and the gear driving member 43 by turning the handle 41. When the handle 41 is turned 90° clockwise, the fixed rod 421 rotates from the vertical direction to the horizontal direction. The fixed rod 421 can drive one end of the rotating rod 422 to make an arc motion with the rotating connection between the rotating rod 422 and the door panel 11 as the center, and then drive the other end of the rotating rod 422 to lift upward, thereby driving the connecting rod 423 to lift vertically upward, and then by lifting the mounting frame 31, the limiting column 32 located in the upper part is removed from the limiting hole 21; at the same time, the gear teeth on the rotating handle 41 will drive the gear 431 meshing with it to rotate, and through the sequential driving of the adjacent gears 431, the rack 432 can eventually be moved downward in the vertical direction, and the rack 432 will drive the connecting rod 423 connected to it to move downward, and finally the limiting column 32 located in the lower part is removed from the limiting hole 21, thereby releasing the limiting fixation of the viewing window 12.

[0067] As for the gear drive, in other embodiments, the gear drive may also include two driving gears and a belt, the driving gear including a large wheel and a small wheel, the large wheel and the small wheel are concentrically connected and integrally formed, the large wheel of one driving gear is engaged with the gear teeth of the rotating handle, and the large wheel of the other driving gear is engaged with the rack, the belt is sleeved on the small wheels of the two driving gears, and by turning the rotating handle, the rotating handle drives the large wheel engaged with it to rotate, thereby driving the small wheel to rotate, and the small wheel drives the belt to drive the small wheel of the other driving gear to rotate, and finally controls the large wheel to drive the rack to rotate.

[0068] like Figure 5 and Figure 6 As shown, the demolition assembly 5 includes:

[0069] A demolition knife 51 is provided in the door panel 11 and is located on a side of the connecting rod 423 away from the rotating handle 41 , with the blade of the demolition knife 51 facing the connecting rod 423 ;

[0070] The driving block 52 is fixedly connected to the demolition knife 51 , and a driving groove 113 is provided on the door panel 11 at a position corresponding to the demolition knife 51 . The driving groove 113 is perpendicular to the connecting rod 423 , and the driving block 52 slides in the driving groove 113 .

[0071] The sliding drive block 52 can manipulate the demolition knife 51 to cut off the connecting rod 423 at the corresponding position. Since the cross-sectional area of ​​the connecting rod 423 is smaller than that of the fixed rod 421 and the rotating rod 422, it is easiest to cut the connecting rod 423 by using the demolition knife 51. After cutting the connecting rod 423, the adjustment block 33 can be manually slid to move the limiting column 32 out of the limiting hole 21, thereby opening the viewing window 12.

[0072] The design principle of the present invention is: by rotating the handle 41, the connecting rod driving part 42 and the gear driving part 43 can be driven to quickly and effectively drive the limit column 32 to move in the limit hole 21, so that the visual window 12 can be locked and opened at any time. If after an accident in the aircraft, the connecting rod driving part 42 and the gear driving part 43 are damaged, the visual window 12 cannot be opened by rotating the handle 41 and the cabin door body 1 cannot be opened by the door lock 112 for escape, at this time, the driving block 52 can be manually slid to drive the demolition knife 51 to cut off the connecting rod 423, and then the adjustment block 33 can be manually slid to move the limit column 32 out of the limit hole 21, so that the visual window 12 can be opened for escape.

[0073] The above description is merely a specific embodiment of the present application, but the scope of protection of the present application is not limited thereto. Any changes or substitutions that can be easily conceived by a person skilled in the art within the technical scope disclosed in the present application should be included in the scope of protection of the present application. Therefore, the scope of protection of the present application should be based on the scope of protection of the claims.

Claims

1. A helicopter full-view door, characterized in that: include: A cabin door body (1) comprises a door panel (11) and a visual window (12). The visual window (12) is provided on the door panel (11). The visual window (12) bulges outward from the helicopter cabin. The visual window (12) is composed of two transparent units (121). The two transparent units (121) are connected to form a complete visual window (12). The two transparent units (121) are rotatably connected to the door panel (11). A position limiting and fixing assembly (3) is slidably mounted in the door panel (11); an adjustment block (33) is fixed on the position limiting and fixing assembly (3); the adjustment block (33) extends from the position limiting and fixing assembly (3) toward the interior of the helicopter cockpit; and a sliding groove (114) is provided on the inner side of the door panel (11) for the adjustment block (33) to extend and slide. A driving component (4), wherein an output end of the driving component (4) and the position-limiting and fixing component (3) are connected via a connecting rod (423), and is used to drive the position-limiting and fixing component (3) to approach an edge of the transparent unit (121) to limit the rotation of the transparent unit (121), or to drive the position-limiting and fixing component (3) to move away from the transparent unit (121) to release the restriction on the transparent unit (121); A breaking assembly (5) is used to destroy the connecting rod (423); the adjusting block (33) is used to be manually operated after the connecting rod (423) is destroyed to drive the limiting fixing assembly (3) away from the transparent unit (121) to release the restriction on the transparent unit (121); The helicopter full-view door further comprises a connecting splint (2), wherein the connecting splint (2) is wrapped around the edge of the transparent unit (121), and a cavity is formed between the connecting splint (2) and the edge of the transparent unit (121); Each of the two transparent units (121) is provided with a corresponding limiting fixing assembly (3), and the limiting fixing assembly (3) includes a mounting frame (31) and a limiting column (32), the mounting frame (31) is slidably connected to the door panel (11), the mounting frame (31) is located on the outer periphery of the transparent unit (121), there are multiple limiting columns (32), and the multiple limiting columns (32) are symmetrically installed on the mounting frame (31), and the connecting splint (2) is provided with a limiting hole (21) at a position corresponding to the limiting column (32), and the limiting column (32) is used to extend into the limiting hole (21); The door panel (11) is provided with a sliding groove (114) on a side of the mounting frame (31) facing away from the transparent unit (121), which is perpendicular to the butt joint surfaces of the two transparent units (121); the adjustment block (33) is fixedly connected to the mounting frame (31); The driving assembly (4) comprises: A rotating handle (41), wherein the rotating handle (41) is rotatably connected to the door panel (11); A connecting rod driving member (42), the connecting rod driving member (42) is used to drive the movement of the limiting fixing assembly (3) on one side; a gear driving member (43), the gear driving member (43) being used to drive the movement of the position limiting and fixing assembly (3) on the other side; The connecting rod driving member (42) and the gear driving member (43) are both driven by the rotating handle (41); The connecting rod driving member (42) comprises: a fixing rod (421), the fixing rod (421) being fixedly connected to the rotating handle (41) and located inside the door panel (11); A rotating rod (422), one end of the rotating rod (422) is rotatably connected to the end of the fixed rod (421), a point between the two ends of the rotating rod (422) is rotatably connected to the door panel (11), and the other end of the rotating rod (422) is fixedly connected to the mounting frame (31) via the connecting rod (423); The gear drive member (43) includes a plurality of gears (431) and racks (432). The number of the gears (431) is an even number. The rotating handle (41) is provided with gear teeth. The plurality of gears (431) are arranged adjacent to each other, and two adjacent gears (431) are meshed with each other. The gears (431) at both ends of the plurality of adjacently arranged gears (431) are respectively meshed with the rotating handle (41) and the racks (432). One end of the rack (432) is fixedly connected to another mounting frame (31) via the connecting rod (423).

2. The helicopter full-view door according to claim 1, characterized in that: The demolition assembly (5) comprises: a demolition knife (51), the demolition knife (51) being arranged in the door panel (11) and being located on a side of the connecting rod (423) away from the rotating handle (41), and the blade of the demolition knife (51) facing the connecting rod (423); A driving block (52) is fixedly connected to the demolition knife (51), and a driving groove (113) is provided on the door panel (11) at a position corresponding to the demolition knife (51), wherein the driving groove (113) is perpendicular to the connecting rod (423), and the driving block (52) slides in the driving groove (113).

3. A helicopter full-view door according to claim 1, characterized in that: The door panel (11) is provided with a door handle (111) and a door lock (112).

4. The helicopter full-view door according to claim 1, characterized in that: Sealing strips (6) are provided on opposite sides of the connecting splint (2) and the mounting frame (31).

Images