Copilot rudder pedal assembly

Abstract

The utility model relates to the technical field of aircraft pedal assemblies, in particular to a co-pilot rudder pedal assembly which comprises a pedal body and a transmission part hinged support arranged on the pedal body, a long shaft is arranged on the pedal body, a shaft hole is formed in the pedal body, a left bearing and a right bearing are arranged in the shaft hole, and the long shaft penetrates through inner rings of the bearings. Inner lantern rings are fixedly installed on the left side face and the right side face of the pedal body respectively, a left outer lantern ring and a right outer lantern ring which are symmetrical are installed on the long shaft, the corresponding inner lantern rings are sleeved with the outer lantern rings, the outer lantern rings are rotationally connected with the inner lantern rings, an end threaded pipe is fixedly installed at the end, communicated with the outside, of the long shaft, and the air outlets are communicated with the end threaded pipe. A hose is installed at the air outlet end of the air source, a hard pipe is fixedly installed at the end of the hose and matched with the end threaded pipe in an inserted mode, an abutting ring is fixedly installed on the hard pipe, and the rotary knob is in threaded connection with the end threaded pipe. According to the utility model, impurities can be prevented from entering to cause blockage, and the rotation is smoother.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft pedal assemblies, in particular to a co-pilot rudder pedal assembly. Background Art

[0002] In the aviation field, the aircraft's control system is a key part of ensuring flight safety. With the continuous development of flight technology, the control methods of aircraft are also constantly evolving. Traditional flight control mainly relies on the pilot to manually operate various mechanical components, such as rudders and elevators, to achieve control of the aircraft. However, with the increasing complexity of modern aircraft, the requirements for the accuracy and response speed of the control system are also getting higher and higher.

[0003] To meet these requirements, modern aircraft generally use fly-by-wire flight control systems, which transmit the pilot's instructions through electrical signals to achieve precise control of the aircraft. In this system, the pilot inputs instructions into the flight computer by operating pedals, side sticks and other control components, and the flight computer then controls the various actuators of the aircraft through electrical signals.

[0004] As an important component of the fly-by-wire flight control system, the design and performance of the aircraft co-pilot pedal assembly are directly related to the accuracy and comfort of flight control. Traditional co-pilot pedal assemblies usually use mechanical or hydraulic connections, which have problems such as slow response speed, low accuracy, and complex maintenance. Currently, common pedals often use electrical connections or force feedback mechanisms for operation.

[0005] However, since the pedals are supported on corresponding shafts, one end of the pedals is rotatably connected to the shafts, and the other end is connected to the corresponding external drive components. At this time, ensuring stable rotation between the pedals and the shafts is essential. However, in actual use, since the soles of shoes directly contact the pedals, impurities on the soles of the shoes can easily enter the rotating part between the pedals and the shafts, affecting the stable transmission of the pedals. This type of pedal and shaft rotating part lacks a component that can block impurities, which is not conducive to the effective impurity blocking effect. In view of this, we propose a co-pilot rudder pedal assembly. Utility Model Content

[0006] The purpose of the present invention is to provide a co-pilot rudder pedal assembly to solve the defects mentioned in the above background technology.

[0007] To achieve the above objectives, the present invention provides the following technical solutions:

[0008] A co-pilot rudder pedal assembly includes a pedal body and a transmission member hinge seat arranged on the pedal body, the pedal body is provided with a long axis, the pedal body is provided with an axial hole with both ends connected to the outside world, two symmetrical bearings are provided in the axial hole, the long axis passes through the inner ring of the bearing, and inner rings concentrically arranged with the axial hole are fixedly installed on the left and right side surfaces of the pedal body, the inner ring is sleeved on the long axis and rotatably connected to the long axis, and two symmetrical outer rings are fixedly installed on the long axis, the outer rings are sleeved on the corresponding inner rings and rotatably connected to the inner rings.

[0009] Preferably, two groups of symmetrical air outlet holes are provided on the long axis, and the air outlet holes are located at the inner side of the outer ring. The end of the long axis is provided with an air source for ventilating toward the air outlet holes.

[0010] Preferably, one end of the long shaft is sealed, and the other end of the long shaft is connected to the outside world. The end of the long shaft connected to the outside world is fixedly installed with an end threaded tube, the air outlet is connected to the end threaded tube, the air outlet end of the air source is fixedly installed with a hose, and the end of the hose is fixedly installed with a hard tube, and the hard tube and the end threaded tube are plugged in and matched.

[0011] Preferably, a tightening ring is fixedly mounted on the hard tube, a knob is slidably connected to the hard tube, and the knob is threadedly connected to the end threaded tube.

[0012] Preferably, the rear arm of the knob abuts against the side surface of the abutting ring, and the outer diameter of the abutting ring is smaller than the inner diameter of the knob.

[0013] Preferably, a sealing ring is sleeved on the hard tube, and the tightening ring presses the sealing ring onto the front side surface of the end threaded tube.

[0014] Preferably, the number of the air outlet holes in each group is between 10 and 20, and the vertical distance between two adjacent air outlet holes is less than 5 mm.

[0015] Compared with the prior art, the beneficial effects of the present invention are:

[0016] 1. The utility model provides a long shaft and a bearing so that the pedal body can rotate normally. The inner ring and the outer ring are provided. The inner ring is sleeved on the long shaft to prevent impurities from entering. The outer ring is sleeved on the inner ring to further block impurities, thereby achieving the effect of preventing impurities from entering.

[0017] 2. The utility model provides components such as an air source and an air outlet, so that when needed, the air source can be used to supply air, so that the gas is blown out from the air outlet from the inside to the outside, thereby blowing out impurities between the inner ring and the outer ring to avoid clogging by impurities. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0019] Figure 2 This is a schematic diagram of the explosion structure of the utility model;

[0020] Figure 3 For this utility model Figure 2 Enlarged view of point B in the middle;

[0021] Figure 4 For this utility model Figure 2 Enlarged view of point A in the middle;

[0022] The meaning of each number in the figure is:

[0023] 1. Pedal body; 10. Axis hole; 11. Inner ring; 12. Bearing; 13. Transmission hinge seat;

[0024] 2. Long axis; 20. Air outlet; 21. Outer ring; 22. End threaded tube;

[0025] 3. Air source; 31. Hose; 32. Hard pipe; 33. Tightening ring; 34. Sealing ring; 35. Knob. DETAILED DESCRIPTION

[0026] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0027] See also Figure 1-Figure 4 The present invention provides a technical solution: a co-pilot rudder pedal assembly, comprising a pedal body 1 and a transmission member hinge seat 13 provided on the pedal body 1, the transmission member hinge seat 13 being connected to a transmission member on an aircraft, a long shaft 2 being provided on the pedal body 1, a shaft hole 10 being provided in the pedal body 1, both ends of which are connected to the outside world, two left and right symmetrical bearings 12 being provided in the shaft hole 10, the long shaft 2 passing through the inner ring of the bearing 12, the inner and outer rings of the bearing 12 being fixedly mounted on the long shaft 2 and the shaft hole 10 respectively, so that the bearing 12 is not likely to slide left and right;

[0028] Specifically, inner rings 11 concentrically arranged with the shaft hole 10 are fixedly installed on the left and right side surfaces of the pedal body 1. The inner ring 11 is sleeved on the long shaft 2 and rotatably connected to the long shaft 2. Two symmetrical outer rings 21 are fixedly installed on the long shaft 2. The outer rings 21 are sleeved on the corresponding inner rings 11 and rotatably connected to the inner rings 11. The inner rings 11 and the outer rings 21 are arranged to prevent impurities from entering the bearing 12 and the shaft hole 10. The distance between the inner ring 11 and the long shaft 2, and the distance between the outer ring 21 and the inner ring 11 are less than 0.1 mm, which are used to prevent impurities from entering.

[0029] In this embodiment, two groups of symmetrical air outlet holes 20 are provided on the long axis 2. The air outlet holes 20 are located on the inner side of the outer ring 21. The end of the long axis 2 is provided with an air source 3 for ventilating toward the air outlet holes 20, so that the air outlet holes 20 are blown from the inside to the outside, so that even if impurities enter between the inner ring 11 and the outer ring 21, they can be blown out smoothly.

[0030] Specifically, one end of the long axis 2 is sealed, and the other end of the long axis 2 is connected to the outside world. The end of the long axis 2 connected to the outside world is fixedly installed with an end threaded tube 22, and the air outlet 20 is connected to the end threaded tube 22. The air outlet end of the air source 3 is fixedly installed with a hose 31, and the end of the hose 31 is fixedly installed with a hard tube 32. The hard tube 32 and the end threaded tube 22 are plugged together. A tightening ring 33 is fixedly installed on the hard tube 32, and a knob 35 is slidably connected to the hard tube 32. The knob 35 is threadedly connected to the end threaded tube 22 to facilitate stable connection operation.

[0031] Furthermore, the rear arm of the knob 35 rests on the side of the tightening ring 33, the outer diameter of the tightening ring 33 is smaller than the inner diameter of the knob 35, and a sealing ring 34 is sleeved on the hard tube 32. The tightening ring 33 presses the sealing ring 34 against the front side of the end threaded tube 22 to achieve a sealing and tightening operation.

[0032] It is worth noting that the number of each group of air outlet holes 20 is between 10 and 20, and the vertical distance between two adjacent air outlet holes 20 is less than 5 mm, which is conducive to normal air outlet and blowing operation.

[0033] When the co-pilot rudder pedal assembly of the present invention is in use, since the inner ring 11 is sleeved on the long axis 2, and the outer ring 21 is sleeved on the inner ring 11, the distance between the inner ring 11 and the long axis 2, and the distance between the outer ring 21 and the inner ring 11 are small, which can block the entry of impurities. In addition, after the gas source 3 supplies gas, the gas enters the long axis 2 along the hose 31, the hard tube 32 and the end threaded tube 22, and the gas is blown out from the air outlet 20, which can blow out the impurities entering between the outer ring 21 and the inner ring 11, and avoid the outer ring 21 and the inner ring 11 being blocked by impurities.

[0034] The above shows and describes the basic principles, main features, and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely preferred examples of the present invention and are not intended to limit the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention, and such changes and improvements fall within the scope of the present invention. The scope of protection claimed in the present invention is defined by the appended claims and their equivalents.

Claims

1. A co-pilot rudder pedal assembly, comprising a pedal body (1) and a transmission member hinge seat (13) arranged on the pedal body (1), characterized in that: The pedal body (1) is provided with a long axis (2), and the pedal body (1) is provided with an axial hole (10) whose two ends are connected to the outside world. Two mutually symmetrical bearings (12) are provided in the axial hole (10). The long axis (2) passes through the inner ring of the bearing (12). The left and right side surfaces of the pedal body (1) are fixedly mounted with inner rings (11) concentrically arranged with the axial hole (10). The inner ring (11) is sleeved on the long axis (2) and is rotatably connected to the long axis (2). The long axis (2) is fixedly mounted with two mutually symmetrical outer rings (21) on the left and right sides. The outer rings (21) are sleeved on the corresponding inner rings (11) and are rotatably connected to the inner rings (11).

2. The passenger steering pedal assembly according to claim 1, characterized in that: Two groups of mutually symmetrical air outlet holes (20) are provided on the long shaft (2), the air outlet holes (20) are located at the inner side of the outer ring (21), and an air source (3) for ventilating toward the air outlet holes (20) is provided at the end of the long shaft (2).

3. The passenger steering pedal assembly according to claim 2, characterized in that: One end of the long shaft (2) is blocked, and the other end of the long shaft (2) is connected to the outside. The end of the long shaft (2) connected to the outside is fixedly installed with an end threaded tube (22), and the air outlet (20) is connected to the end threaded tube (22). The air outlet end of the air source (3) is fixedly installed with a hose (31), and the end of the hose (31) is fixedly installed with a hard tube (32), and the hard tube (32) is plugged into and fitted with the end threaded tube (22).

4. The passenger steering pedal assembly according to claim 3, characterized in that: A tightening ring (33) is fixedly mounted on the hard tube (32), a knob (35) is slidably connected to the hard tube (32), and the knob (35) is threadedly connected to the end threaded tube (22).

5. The passenger steering pedal assembly according to claim 4, characterized in that: The rear arm of the knob (35) abuts against the side surface of the abutting ring (33), and the outer diameter of the abutting ring (33) is smaller than the inner diameter of the knob (35).

6. The passenger steering pedal assembly according to claim 5, characterized in that: A sealing ring (34) is sleeved on the hard tube (32), and the tightening ring (33) presses the sealing ring (34) against the front side of the end threaded tube (22).

7. The passenger steering pedal assembly according to claim 2, characterized in that: The number of the air outlet holes (20) in each group is between 10 and 20, and the vertical distance between two adjacent air outlet holes (20) is less than 5 mm.

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