Novel anti-shake device for aircraft environment control radiator
By designing the heat dissipation structure and fastening structure in the aircraft's environmentally controlled radiator, the problem of radiator jitter is solved, stable clamping and efficient heat dissipation are achieved, and the heat dissipation performance of the aircraft's environmentally controlled radiator is improved.
Patent Information
- Application Number
- CN202322905011.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2023-10-27
- Publication Date
- 2024-12-27
- Estimated Expiration
- 2033-10-27
AI Technical Summary
During operation, the aircraft's environmentally controlled radiator is prone to jitter due to the lack of effective external force tightening, which affects its heat dissipation performance.
A new anti-shake device including a heat dissipation structure and a fastening structure is designed. The rotating frame is driven by the motor to rotate and drive the rotating frame. The heat dissipation plate absorbs and discharges heat, and the elastic structure uses the hand handle and locking structure to achieve the heat dissipation device. Stable clamping to prevent jitter.
It effectively prevents shaking of the radiator, improves heat dissipation efficiency, and achieves stable clamping of the heat dissipation device through the design of the elastic structure, ensuring the normal operation of the aircraft's environmentally controlled heat dissipation.
Smart Images
Figure CN222247651U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of radiators, in particular to a novel anti-shake device for an aircraft environmental control radiator. Background Art
[0002] Radiators are frequently used equipment in industrial production, and their quality has an important impact on aircraft environmental control.
[0003] The radiator plays an important role in environmental control. In the process of assisting the operation of other components, it is prone to shaking due to the lack of good external force to tighten it, which affects the use of the radiator. Utility Model Content
[0004] 1. Technical issues to be solved
[0005] In order to solve the above technical problems, the utility model provides a novel anti-shake device for an aircraft environmental control radiator.
[0006] (II) Technical solution
[0007] Based on this, the utility model provides the following technical solutions: a novel anti-shake device for an aircraft environmental control radiator, comprising a top cover, a carrying handle, a heat dissipation port, a heat dissipation structure and a fastening structure, wherein the top cover is snap-fitted and installed on the upper end of the fastening structure, the carrying handle is embedded and connected to the upper end surface of the top cover, the heat dissipation port and the top cover are an integrated structure and are arranged through, and the fastening structure is nested in the outer periphery of the heat dissipation structure;
[0008] The heat dissipation structure includes a ring plate frame, a motor, a rotating shaft, a rotating frame, a heat sink and a chassis. The ring plate frame is installed above the heat sink, the motor is installed at the top of the rotating shaft, the rotating frame and the rotating shaft are an integrated structure and the rotating frame is located at the outer periphery of the rotating shaft, the upper end of the heat sink is connected to the rotating shaft, and the chassis is embedded and connected to the bottom end of the heat sink.
[0009] Preferably, the fastening structure comprises a fixed ring frame, a placement area, a displacement area and an elastic structure, the placement area is located on the inner side of the fixed ring frame, the displacement area and the fixed ring frame are an integrated structure and are arranged through, and the elastic structure moves in the placement area.
[0010] Preferably, the tensioning structure includes a hand handle, a solid frame, a locking structure, a limiting path and an anti-deviating rod, the hand handle is embedded and connected to the outer side of the solid frame, the locking structure is rotatably engaged with the solid frame, the limiting path and the solid frame are an integrated structure, and the anti-deviating rod moves in the limiting path.
[0011] Preferably, the locking structure includes an arc plate, a rotating block, a tightening block and a fulcrum shaft, the rotating block is embedded in the lower end of the arc plate, the upper end of the arc plate is hinged to the tightening block, and the fulcrum shaft passes through the front position of the tightening block.
[0012] Preferably, the heat dissipation opening is located above the ring plate frame, and the fastening structure is sleeved on the outer circumference of the ring plate frame.
[0013] Preferably, the elastic structure is movably fitted to the outer periphery of the ring plate frame, and the displacement zone is an empty opening of a certain length, which provides limit control for the movement of the elastic structure.
[0014] Preferably, the hand handle passes through the displacement area, and the solid frame is gap-fitted on the inner side of the fixed ring frame. The solid frame is annular in shape and is provided with six limiting paths. It makes annular displacement changes under the drive of the hand handle, and can make directional annular displacement by the cooperation of the anti-drift rod and the limiting path, so that the space on the inner side of the locking structure can be flexibly changed when the locking structure is rotated.
[0015] Preferably, the rotating block is movably engaged with the inner side of the solid frame, and the arc plate, rotating block and tightening block cooperate as a group, and there are six groups, which are evenly distributed in a ring shape. When driven, they can flip at a certain angle, making it convenient for the tightening block to lean against the outside of the ring plate frame to exert a stable clamping force on it.
[0016] (III) Beneficial effects
[0017] Compared with the prior art, the utility model provides a novel anti-shake device for an aircraft environmental control radiator, which has the following beneficial effects:
[0018] 1. This novel anti-shake device for an aircraft environmental control radiator is provided with a heat dissipation structure, and a motor is started to drive the rotating shaft to rotate, thereby driving the rotating frame to rotate. The heat absorbed by the heat dissipation plate is driven to the rows under the action of the rotating frame, and is discharged out of the device through the heat dissipation port, thereby playing a heat dissipation role for the aircraft environmental control. By providing a fastening structure, the heat dissipation structure is placed at the position of the placement area, and the personnel can control the tightness of the heat dissipation device by turning the hand handle according to the area occupied by the heat dissipation structure in the placement area.
[0019] 2. This novel anti-shake device for an aircraft environmentally controlled radiator is provided with an elastic structure. The anti-deviance rod moves along the limit path as the solid frame rotates, and the reverse direction provides an annular positioning effect for the displacement of the solid frame. The position of the rotating block changes as the solid frame rotates, driving the position of the arc plate to change, thereby exerting a driving force on the tight hoop block. The tight hoop block rotates a certain angle with the fulcrum axis as the fulcrum, so that the six sets of locking structures all make synchronous position changes, so that the fulcrum axis can be attached to the outer wall of the ring plate frame, which has a confinement effect on it, and the entire device has an anti-shake effect. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Figure 1 It is a schematic diagram of the overall structure of the novel anti-shake device of the aircraft environmental control radiator of the utility model;
[0021] Figure 2 It is a structural schematic diagram of the heat dissipation structure of the utility model;
[0022] Figure 3 It is a structural schematic diagram of the fastening structure of the utility model;
[0023] Figure 4 It is a structural schematic diagram of the elastic structure of the utility model;
[0024] Figure 5 It is a structural schematic diagram of the locking structure of the utility model.
[0025] In the figure: top cover-1, carrying handle-2, heat dissipation port-3, heat dissipation structure-4, fastening structure-5, ring plate frame-41, motor-42, rotating shaft-43, rotating frame-44, heat dissipation plate-45, chassis-46, fixed ring frame-51, placement area-52, displacement area-53, elastic structure-54, hand handle-q1, solid frame-q2, locking structure-q3, limit track-q4, anti-deviation rod-q5, arc plate-q31, rotating block-q32, tight hoop block-q33, fulcrum shaft-q34. DETAILED DESCRIPTION
[0026] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0027] See also Figure 1-2 , a new type of anti-shake device for an aircraft environmental control radiator, comprising a top cover 1, a carrying handle 2, a heat dissipation port 3, a heat dissipation structure 4 and a fastening structure 5, the top cover 1 is snap-fitted and installed on the upper end of the fastening structure 5, the carrying handle 2 is embedded and connected to the upper end surface of the top cover 1, the heat dissipation port 3 and the top cover 1 are an integrated structure and are arranged through, the fastening structure 5 is nested in the outer periphery of the heat dissipation structure 4, the heat dissipation structure 4 comprises a ring plate frame 41, a motor 42, a rotating shaft 43, a rotating frame 44, a heat dissipation plate 45 and a chassis 46, the ring plate frame 41 is installed above the heat dissipation plate 45, the motor 42 is installed at the top of the rotating shaft 43, the rotating frame 44 and the rotating shaft 43 are an integrated structure and the rotating frame 44 is located at the outer periphery of the rotating shaft 43, the upper end of the heat dissipation plate 45 is connected to the rotating shaft 43, the chassis 46 is embedded and connected to the bottom end of the heat dissipation plate 45, the heat dissipation port 3 is through-located above the ring plate frame 41, and the fastening structure 5 is sleeved on the outer periphery of the ring plate frame 41.
[0028] See also Figure 3-4 A novel anti-shake device for an aircraft environmental control radiator, wherein a fastening structure 5 comprises a fixed ring frame 51, a placement area 52, a displacement area 53 and an elastic structure 54, wherein the placement area 52 is located on the inner side of the fixed ring frame 51, the displacement area 53 and the fixed ring frame 51 are an integrated structure and are arranged through, and the elastic structure 54 moves in the placement area 52, and the elastic structure 54 comprises a hand handle q1, a solid frame q2, a locking structure q3, a limit path q4 and an anti-deviating rod q5, wherein the hand handle q1 is embedded and connected to the outer side of the solid frame q2, the locking structure q3 is rotatably engaged with the solid frame q2, and the limit path q4 is integrated with the solid frame q2 The anti-deviation rod q5 moves in the limit track q4, the tension structure 54 moves and cooperates with the outer periphery of the ring plate frame 41, the displacement area 53 is an empty opening of a certain length, which provides limit control for the movement of the tension structure 54, the hand handle q1 passes through the displacement area 53, and the solid frame q2 is gap-fitted on the inner side of the fixed ring frame 51. The solid frame q2 is annular and has six limit tracks q4. It makes annular displacement changes under the drive of the hand handle q1. The anti-deviation rod q5 and the limit track q4 can make directional annular displacement, which is convenient for the locking structure q3 to flexibly change its inner space when rotating.
[0029] See also Figure 5 A novel anti-shake device for an aircraft environmentally controlled radiator, wherein a locking structure q3 comprises an arc plate q31, a rotating block q32, a clamping block q33 and a fulcrum shaft q34, wherein the rotating block q32 is embedded and connected to the lower end of the arc plate q31, and the upper end of the arc plate q31 is hinged to the clamping block q33, and the fulcrum shaft q34 passes through the front position of the clamping block q33, and the rotating block q32 is movably engaged with the inner side of the solid frame q2, and the arc plate q31, the rotating block q32 and the clamping block q33 are a group for coordinated movement, and six groups are provided, which are evenly distributed in a ring shape, and can be flipped at a certain angle when driven, so that the clamping block q33 can be attached to the outside of the ring plate frame 41 to generate a stable clamping force thereon.
[0030] In summary, by setting up the heat dissipation structure 4, the motor 42 is started, and the driving shaft 43 is rotated to drive the rotating frame 44 to rotate. The heat absorbed by the heat dissipation plate 45 is driven to the row under the action of the rotating frame 44, and is discharged out of the device through the heat dissipation port 3, thereby playing a heat dissipation role for the aircraft environmental control. By setting up the fastening structure 5, the heat dissipation structure 4 is placed at the position of the placement area 52, and the personnel then toggle the hand handle q1 according to the size of the area occupied by the heat dissipation structure 4 in the placement area 52. By setting up the elastic structure 54, the hand handle q1 can be manually moved along the arc of the displacement area 53 by the personnel. The anti-deviance rod q5 is displaced along the limit path q4 as the solid frame q2 rotates, and the reverse direction provides an annular positioning effect for the displacement of the solid frame q2. The position of the fulcrum shaft q34 is fixed, and the position of the rotating block q32 will change as the solid frame q2 rotates, driving the position of the arc plate q31 to change, thereby exerting a driving force on the tightening block q33. The tightening block q33 rotates a certain angle with the fulcrum shaft q34 as the fulcrum, so that the six groups of locking structures q3 all make synchronous position changes, so that the fulcrum shaft q34 can be attached to the outer wall of the ring plate frame 41, which has a confinement effect on it, and the whole device has an anti-shake effect.
[0031] The control method of the present invention is to control by manually starting and closing the switch. The wiring diagram of the power element and the provision of power supply are common knowledge in the field, and the present invention is mainly used to protect mechanical devices, so the present invention will not explain the control method and wiring arrangement in detail.
[0032] The control method of the present invention is automatic control through a controller. The control circuit of the controller can be realized by simple programming by technicians in this field. The provision of power is also common knowledge in this field. The present invention is mainly used to protect mechanical devices, so the present invention will no longer explain the control method and circuit connection in detail.
[0033] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.
Claims
1. A novel anti-shake device for an aircraft environmental control radiator, characterized in that: The invention comprises a top cover (1), a carrying handle (2), a heat dissipation port (3), a heat dissipation structure (4) and a fastening structure (5), wherein the top cover (1) is snap-fitted and mounted on the upper end of the fastening structure (5), the carrying handle (2) is embedded and connected to the upper end surface of the top cover (1), the heat dissipation port (3) and the top cover (1) are an integrated structure and are arranged through, and the fastening structure (5) is nested in the outer periphery of the heat dissipation structure (4); The heat dissipation structure (4) comprises a ring plate frame (41), a motor (42), a rotating shaft (43), a rotating frame (44), a heat dissipation plate (45) and a chassis (46); the ring plate frame (41) is installed above the heat dissipation plate (45); the motor (42) is installed at the top of the rotating shaft (43); the rotating frame (44) and the rotating shaft (43) are an integrated structure and the rotating frame (44) is located on the outer periphery of the rotating shaft (43); the upper end of the heat dissipation plate (45) is connected to the rotating shaft (43); and the chassis (46) is embedded and connected to the bottom end of the heat dissipation plate (45).
2. The novel anti-shake device for an aircraft environment-controlled radiator according to claim 1, characterized in that: The fastening structure (5) comprises a fixed ring frame (51), a placement area (52), a displacement area (53) and an elastic structure (54); the placement area (52) is located on the inner side of the fixed ring frame (51); the displacement area (53) and the fixed ring frame (51) are an integrated structure and are arranged through; and the elastic structure (54) moves in the placement area (52).
3. The novel anti-shake device for an aircraft environment-controlled radiator according to claim 2, characterized in that: The tensioning structure (54) comprises a hand handle (q1), a solid frame (q2), a locking structure (q3), a limiting path (q4) and an anti-deviating rod (q5); the hand handle (q1) is embedded and connected to the outer side of the solid frame (q2); the locking structure (q3) is rotatably engaged with the solid frame (q2); the limiting path (q4) and the solid frame (q2) are an integrated structure; and the anti-deviating rod (q5) moves in the limiting path (q4).
4. The novel anti-shake device for an aircraft environment-controlled radiator according to claim 3 is characterized in that: The locking structure (q3) comprises an arc plate (q31), a rotating block (q32), a tightening block (q33) and a fulcrum shaft (q34); the rotating block (q32) is embedded and connected to the lower end of the arc plate (q31); the upper end of the arc plate (q31) is hinged to the tightening block (q33); and the fulcrum shaft (q34) passes through a front position of the tightening block (q33).
5. The novel anti-shake device for an aircraft environment-controlled radiator according to claim 1, characterized in that: The heat dissipation opening (3) is located above the ring plate frame (41), and the fastening structure (5) is sleeved on the outer circumference of the ring plate frame (41).
6. The novel anti-shake device for an aircraft environment-controlled radiator according to claim 2, characterized in that: The elastic structure (54) is movably matched with the outer periphery of the ring plate frame (41).
7. The novel anti-shake device for an aircraft environment-controlled radiator according to claim 3 is characterized by: The hand lever (q1) passes through the displacement area (53), and the solid frame (q2) is loosely fitted inside the fixed ring frame (51).
8. The novel anti-shake device for an aircraft environment-controlled radiator according to claim 4, characterized in that: The rotating block (q32) is movably engaged with the inner side of the solid frame (q2).