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CN-122007965-A - Drilling device for manufacturing aircraft ultra-high strength material parts

CN122007965ACN 122007965 ACN122007965 ACN 122007965ACN-122007965-A

Abstract

The present invention discloses a drilling device for manufacturing aircraft ultra-high strength material parts, which relates to the field of aircraft parts production technology. The present invention comprises a main body, a jet mechanism is provided on the side of the main body, a placement mechanism is provided inside the main body, and the placement mechanism is located in the middle position of the main body. The main body is provided with a pushing mechanism and a collecting mechanism, and the pushing mechanism is located above the collecting mechanism. In the present invention, the gas sprayed by the jet mechanism cleans the waste on the upper surface of the raw material to avoid the accumulation of waste on the upper surface of the raw material, which may cause blurry images captured by the camera and affect the efficiency and accuracy of drilling positioning. The waste is collected by the collecting mechanism to facilitate centralized processing of the waste. In the present invention, the waste at the bottom of the shell is pushed by the movement of the scraper. The debris moves, Move the debris inside the storage box to avoid manual cleaning, save labor, and improve cleaning efficiency.

Inventors

  • YANG XUE
  • LIU QIAO
  • DONG XIAOGANG
  • YANG BOBO
  • ZHANG ZHIHUI

Assignees

  • 汉中万利航空装备制造有限公司

Dates

Publication Date
20260512
Application Date
20260410

Claims (10)

  1. 1. The drilling device for manufacturing the ultra-high strength material parts of the aircraft comprises a main body (1) and is characterized in that an air injection mechanism (2) is arranged on the side face of the main body (1), a placement mechanism (3) is arranged in the main body (1), the placement mechanism (3) is located in the middle of the main body (1), a pushing mechanism (4) and a collecting mechanism (5) are arranged in the main body (1), and the pushing mechanism (4) is located above the collecting mechanism (5).
  2. 2. The drilling device for manufacturing the parts made of the ultra-high strength materials of the airplane according to claim 1, wherein the main body (1) comprises a shell (101), an adjusting frame (102) is slidably installed in the shell (101), sliding blocks (103) are fixedly installed on two sides of the adjusting frame (102), the sliding blocks (103) are slidably arranged inside the shell (101), a first screw (110) is rotatably installed on two sides of the shell (101), the first screw (110) is in threaded connection with the sliding blocks (103), a second bevel gear (109) is fixedly installed at the center of the top end of the first screw (110), an installation seat (106) is fixedly installed on the side face of the shell (101), a motor (107) is fixedly installed in the installation seat (106), one end of an output shaft of the motor (107) is rotatably arranged inside the shell (101), two first bevel gears (108) are fixedly installed on the outer surface of the output shaft of the motor (107), the first bevel gears (108) are meshed with the second bevel gears (109), and a drilling device (104) is fixedly installed on the lower surface of the adjusting frame (102).
  3. 3. The drilling device for manufacturing the ultra-high strength material parts of the airplane according to claim 2, wherein the air injection mechanism (2) comprises a mounting frame (201), the mounting frame (201) is fixedly arranged on the side surface of the outer shell (101) far away from the two first screw rods (110), a sealing barrel (206) is fixedly arranged in the mounting frame (201), a pull rod (208) is slidably arranged in the sealing barrel (206), a piston (207) is fixedly arranged at the center of the bottom end of the pull rod (208), the piston (207) is slidably arranged in the sealing barrel (206), a pull handle (209) is fixedly arranged at the center of the top end of the pull rod (208), limiting blocks (213) are fixedly arranged on two sides of the pull handle (209) and are slidably arranged in the mounting frame (201), two connecting pipes (210) are fixedly arranged on the outer surface of the sealing barrel (206), one ends of the two connecting pipes (210) far away from the sealing barrel (206) are fixedly connected with a transmission pipe (211), one ends of the transmission pipe (211) are far away from the outer shell (208), one ends of the connecting pipes (101) are far away from the inner ends of the connecting pipes (105) are fixedly arranged in the inner sides of the connecting pipes (201) and are far away from the inner sides of the connecting pipes (105), the ball valve (212) is rotationally installed in the connecting pipe (210), the air inlet pipe (220) is fixedly installed on the upper side and the lower side of the sealing barrel (206), the sealing plug (221) is slidably installed in the air inlet pipe (220), two connecting strips (222) are fixedly installed on the upper surface of the sealing plug (221), the connecting strips (222) are slidably arranged inside the air inlet pipe (220), a spring (223) is fixedly installed on the upper surface of the connecting strips (222), and one end of the spring (233) away from the connecting strips (22) is fixedly connected inside the air inlet pipe (220).
  4. 4. A drilling device for manufacturing ultra-high strength material parts of an aircraft according to claim 3, wherein a mounting frame (115) is fixedly mounted in a side plate of the housing (101) close to the mounting frame (201), a first mounting rod (116) is rotatably mounted in two side plates of the mounting frame (115), a third bevel gear (118) is fixedly mounted at the center of one end of the two first mounting rods (116) close to each other, a first fixing rod (119) is rotatably mounted in two transverse plates of the mounting frame (115), three fourth bevel gears (120) are fixedly mounted on the outer surface of the first fixing rod (119), the third bevel gear (118) is meshed with the fourth bevel gears (120) positioned in the middle of the first fixing rod (119), two second transmission rods (218) are fixedly mounted on the outer surface of the ball valve (212), a fifth bevel gear (219) is fixedly mounted at one end of the two second transmission rods (218) far away from each other, and the fifth bevel gears (219) are meshed with the fourth bevel gears (120) positioned at the two ends of the first fixing rod (119).
  5. 5. The drilling device for manufacturing the ultra-high strength material parts of the airplane according to claim 4, wherein a first toothed plate (214) is fixedly arranged on the side surface of the two limiting blocks (213) close to the mounting frame (115), the first toothed plate (214) is slidably arranged inside the mounting frame (201), a first gear (215) is rotatably arranged in the two side plates of the mounting frame (201) close to the first toothed plate (214), the first gear (215) is movably meshed with the first toothed plate (214), a one-way bearing (216) is fixedly arranged on the side surface of the first gear (215) away from each other, a second belt pulley (217) is fixedly arranged at the center of one end of the one-way bearing (216) away from the first gear (215), a second belt pulley (117) is fixedly arranged at the center of one end of the first mounting rod (116) away from each other, and a connecting belt is arranged between the second belt pulley (217) and the second belt pulley (117).
  6. 6. The drilling device for manufacturing the ultra-high strength material parts of the airplane according to claim 3, wherein the mounting frame (201) is far away from a side plate of the shell (101) and is rotationally provided with a second mounting rod (203), a rotating plate (204) is fixedly arranged at the center of one end of the second mounting rod (203) close to the shell (101), a limit rod (205) is fixedly arranged at the side surface of the rotating plate (204) far away from the second mounting rod (203), one end of the limit rod (205) far away from the rotating plate (204) is slidingly inserted into the pull handle (209), a first toothed plate (111) is fixedly arranged at the side surface of the slider (103) positioned on the right side, a first gear (112) is rotationally arranged at the toothed plate of the shell (101) close to the first toothed plate (111), the first gear (112) is meshed with the first toothed plate (111), a first connecting rod (113) is rotationally arranged in the inner side of the shell (101) close to the first toothed plate (111), one end of the first connecting rod (113) far away from the first toothed plate (112) is fixedly arranged at the center of the first end (202) far away from the first pulley (114), and a fixed belt is arranged between the first belt pulley (202) and the first belt pulley (114) in a transmission way.
  7. 7. The drilling device for manufacturing the ultra-high strength material parts of the airplane according to claim 1, wherein the placement mechanism (3) comprises a placement plate (301), the placement plate (301) is slidably arranged inside the shell (101), sliding strips (305) are fixedly arranged on two sides of the placement plate (301), the sliding strips (305) are slidably arranged inside the shell (101), a first electric cylinder (121) is fixedly arranged in a side plate of the shell (101) close to the mounting frame (201), the first electric cylinder (121) is fixedly connected to the placement plate (301) far from the center of one end of the mounting frame (201), two movable plates (302) are slidably arranged on the upper surface of the placement plate (301), the side surfaces of the movable plates (302) close to each other are in movable contact with two sides of raw materials, movable blocks (303) are fixedly arranged on two sides of the movable plates (302) close to the placement plate (301), the movable blocks (303) are slidably arranged inside the placement plate (301), two electric cylinders (304) are fixedly arranged on the upper surface of the placement plate (301), and the two electric cylinders (304) are fixedly connected to the center of one end of the other movable plates (304).
  8. 8. The drilling device for manufacturing the ultra-high strength material parts of the airplane according to claim 7, wherein the pushing mechanism (4) comprises a scraper blade (401), the scraper blade (401) is arranged inside the shell (101) in a sliding manner, both sides of the scraper blade (401) are fixedly provided with a limiting bar (402), the limiting bar (402) is arranged inside the shell (101) in a sliding manner, a third screw (128) is rotatably arranged in both side plates of the shell (101) close to the limiting bar (402), the third screw (128) is connected with the limiting bar (402) in a threaded manner, the side surface of the sliding bar (305) positioned on the left side is fixedly provided with a third toothed plate (307), the third toothed plate (307) is arranged inside the shell (101), the side plates of the shell (101) close to the third toothed plate (307) are rotatably provided with a third gear (132), the side plates of the shell (101) close to the third toothed plate (307) are rotatably meshed, the side plates of the shell (101) close to the third toothed plate (307) are rotatably provided with a third gear (135), the side plates of the third toothed plate (307) are fixedly arranged at the top end of the connecting rod (133) close to the third toothed plate (307), three No. four bevel gears (136) are fixedly mounted on the rotating rod (135), the No. three bevel gears (134) are meshed with the No. four bevel gears (136) located in the middle of the rotating rod (135), a No. five bevel gear (137) is fixedly mounted at the center of one end of the third screw rod (128) close to the rotating rod (135), and the No. five bevel gears (137) are meshed with the No. four bevel gears (136) located in the middle of the rotating rod (135).
  9. 9. Drilling device for manufacturing parts of ultra-high strength materials for aircraft according to claim 1, characterized in that the collection mechanism (5) comprises storage boxes (501), two storage boxes (501) are slidably arranged inside the housing (101), the two storage boxes (501) are respectively positioned at two sides of the bottom of the housing (101), moving bars (502) are fixedly arranged at two sides of the storage boxes (501), and the moving bars (502) are slidably arranged inside the housing (101).
  10. 10. The drilling device for manufacturing the parts made of the ultra-high strength material of the airplane according to claim 2, wherein the shell (101) is far away from the side plate of the mounting frame (201) and is slidably provided with the baffle (122), the baffle (122) is slidably arranged inside the shell (101), the shell (101) is far away from the side plate of the mounting frame (201) and is rotatably provided with two second screw rods (123), the second screw rods (123) are connected with the baffle (122) through threads, a second bevel gear (126) is fixedly arranged at the center of the top end of the second screw rods (123), a first transmission rod (124) is rotatably arranged inside the side plate of the shell (101) close to the baffle (122), two first bevel gears (125) are rotatably arranged on the first transmission rod (124), the first bevel gears (125) are meshed with the second bevel gears (126), the shell (101) is far away from the side plate of the third toothed plate (307), a second toothed plate (306) is slidably arranged inside the side plate, the second toothed plate (306) is fixedly arranged on the side plate (305), a second toothed plate (306) is fixedly arranged on the lower surface of the sliding plate (305), the shell (101) is rotatably provided with a first toothed plate (129) which is rotatably arranged near the second toothed plate (306), the second toothed plate (129) and is rotatably arranged near the second toothed plate (129), and second dead lever (130) are close to the one end center department fixed connection of placing board (301) on second gear (129), one end center department fixed mounting that second dead lever (130) kept away from second gear (129) has fourth belt pulley (131), one end center department fixed mounting that first transfer line (124) are close to fourth belt pulley (131) has third belt pulley (127), and installs the drive belt between third belt pulley (127) and fourth belt pulley (131).

Description

Drilling device for manufacturing aircraft ultra-high strength material parts Technical Field The invention relates to the technical field of aircraft part production, in particular to a drilling device for manufacturing an aircraft ultra-high strength material part. Background An aircraft refers to an aircraft which is heavier than air and flies in the atmosphere by generating forward thrust or pulling force by a power device with one or more engines and generating lifting force by fixed wings of a fuselage, and most of the aircraft consists of five main parts, namely wings, a fuselage, a tail wing, a landing gear and a power device. In the process of aircraft manufacturing, the assembly is convenient between each part of aircraft, thereby need to bore holes to the spare part, thereby assemble conveniently, thereby consequently lead to aircraft spare part quantity more owing to the volume of aircraft is great, but when processing the spare part of common rectangle, usually adopt automatic drilling machine to process, thereby improve efficiency, but most automatic drilling machines at present are when using, all shoot the raw materials by the camera, fix a position the drilling position through the picture of shooing, and can produce the sweeps in the in-process of boring, when piling up too much sweeps on the raw materials surface, a plurality of targets can appear in the camera picture, thereby the picture that leads to the camera to shoot appears fuzzy phenomenon, the efficiency and the degree of accuracy of location lead to the fact the influence, and most rotation drilling machines at present are when using, can not clear up the sweeps that drops voluntarily, need manual clearance, inconvenient daily use, the inventor proposes a drilling equipment for aircraft ultra-high strength material part manufacturing is used for solving above-mentioned problem. Disclosure of Invention The invention aims to solve the problems that scraps are easy to accumulate on the surfaces of raw materials and the scraps need to be cleaned manually, and provides a drilling device for manufacturing parts made of ultra-high strength materials of an airplane. In order to solve the technical problems, the drilling device for manufacturing the parts of the ultra-high strength materials of the airplane comprises a main body, wherein an air injection mechanism is arranged on the side surface of the main body, a placement mechanism is arranged in the main body and is positioned in the middle of the main body, a pushing mechanism and a collecting mechanism are arranged in the main body, and the pushing mechanism is positioned above the collecting mechanism. Preferably, the main part includes the shell, sliding mounting has the alignment jig in the shell, the equal fixed mounting in both sides of alignment jig has the slider, and the slider slides and sets up inside the shell, the both sides of shell all rotate and install first screw rod, and threaded connection has the slider on the first screw rod, top center department fixed mounting of first screw rod has the second bevel gear, the side fixed mounting of shell has the mount pad, fixed mounting has the motor in the mount pad, and the one end rotation setting of motor output shaft is inside the shell, the surface fixed mounting of motor output shaft has two first bevel gears, and first bevel gear meshes with the second bevel gear, the lower fixed surface of alignment jig installs the perforator. Preferably, the air injection mechanism comprises a mounting frame, and the mounting frame fixed mounting is kept away from on the side of two first screw rods at the shell, sealing barrel is fixed mounting in the mounting frame, sliding mounting has the pull rod in the sealing barrel, bottom center department fixed mounting of pull rod has the piston, and the piston slides and sets up inside the sealing barrel, top center department fixed mounting of pull rod has the pull handle, both sides of pull handle all fixed mounting has the stopper, and stopper sliding arrangement is inside the mounting frame, sealing barrel's surface fixed mounting has two connecting pipes, two connecting pipes are kept away from sealing barrel's one end fixedly connected with transmission pipe, and the one end that the transmission pipe kept away from the connecting pipe runs through the shell, the side fixed mounting that the perforator is close to the mounting frame has the elasticity clamp, and the one end movable clamp that the connecting pipe was kept away from to the connecting pipe is inside the elasticity clamp, connecting pipe internal rotation mounting has the ball valve, both sides equal fixed mounting has the intake pipe about the sealing barrel, sliding mounting has the sealing plug, the upper surface fixed mounting of sealing plug has two connecting strips, and the connecting strip slides and sets up inside the intake pipe, the upper surface fixed mounting of connecting strip has the spring, and the o