KR950003315Y1 - Structure for height preception - Google Patents
Structure for height preception Download PDFInfo
- Publication number
- KR950003315Y1 KR950003315Y1 KR2019930011574U KR930011574U KR950003315Y1 KR 950003315 Y1 KR950003315 Y1 KR 950003315Y1 KR 2019930011574 U KR2019930011574 U KR 2019930011574U KR 930011574 U KR930011574 U KR 930011574U KR 950003315 Y1 KR950003315 Y1 KR 950003315Y1
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- KR
- South Korea
- Prior art keywords
- height
- column
- encoder
- boarding bridge
- rack
- Prior art date
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Classifications
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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
- B64F1/30—Ground or aircraft-carrier-deck installations for embarking or disembarking passengers
- B64F1/305—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
- G01B5/02—Measuring arrangements characterised by the use of mechanical techniques for measuring length, width or thickness
- G01B5/06—Measuring arrangements characterised by the use of mechanical techniques for measuring length, width or thickness for measuring thickness
- G01B5/061—Measuring arrangements characterised by the use of mechanical techniques for measuring length, width or thickness for measuring thickness height gauges
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D5/00—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable
- G01D5/12—Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable using electric or magnetic means
Abstract
내용 없음.No content.
Description
제1도는 일반적인 항공기 탑승교를 나타내는 측면도.1 is a side view showing a typical aircraft boarding bridge.
제2도는 종래 탑승교의 승강장치인 드라이브컬럼을 나타내는 단면도.2 is a cross-sectional view showing a drive column that is a lifting device of a conventional boarding bridge.
제3a도는 본 고안의 높이 감지장치 취부구조를 나타내는 부분 절개 분해사시도, b도는 본 고안의 높이 감지장치 취부구조를 나타내는 횡단면도.Figure 3a is a partially exploded perspective view showing a height sensing device mounting structure of the present invention, b is a cross-sectional view showing a height sensing device mounting structure of the present invention.
제4도는 본 고안 높이 감지장치의 회로도.4 is a circuit diagram of a height sensing device of the present invention.
* 도면의 주요부분에 대한 부호의 설명* Explanation of symbols for main parts of the drawings
42 : 외측컬럼 43 : 내측컬럼42: outer column 43: inner column
47 : 래크 48 : 피니언기어47: rack 48: pinion gear
49 : 엔코더 49a : 카운터49: encoder 49a: counter
49b : 리미트스위치49b: limit switch
본 고안은 외측컬럼과 내측컬럼의 가이드에 의해 탑승교의 높이를 조정하는 승강장치에 관한 것으로서, 높이 감지가 정밀하고 고장이 적도록 하는 항공기 탑승교의 높이 감지장치 취부구조에 관한 것이다.The present invention relates to a lifting device for adjusting the height of the boarding bridge by the guide of the outer column and the inner column, and relates to the height sensing device mounting structure of the aircraft boarding bridge so that the height detection is accurate and less trouble.
최근 사용되는 항공기의 탑승교는 제1도에서 도시되는 바와 같이, 콘테이너로 형성되는 턴넬(10)들이 내부로 수납 가능하게 서로 연결되고, 턴넬(10) 일단부에 좌우로 회전되는 로턴다(rotunda)(20)가 연결되며, 턴넬(10) 타단부에 모터에 의한 회전장치(31)가 부가되는 캡(cap)(30)이 연결되어, 공항청사의 게이트에 로턴다(20)가 연통되게 연결되고, 항공기의 도어에 캡(30)이 연통되게 연결되도록 되어 있다.As shown in FIG. 1, a boarding bridge of an aircraft used in recent years is a rotunda which is connected to each other so that the turnnels 10 formed of containers are receivable therein, and rotates left and right at one end of the turnnel 10. 20 is connected, and the other end of the turnnel 10 is connected to the cap 30 to which the rotating device 31 is added by a motor, so that the roton 20 is connected to the gate of the airport building. The cap 30 is connected to the door of the aircraft in communication.
여기에서, 턴넬(10)은 제1턴넬(11), 제2턴넬(12), 제3턴넬(13)이 각기 폭과 높이가 다르게 형성되고, 서로 내측으로 수납이 가능하게 구성되어, 항공기의 기종에 따라 턴넬의 전체길이를 조정할 수 있도록 되어 있다. 또한, 제1턴넬(11)은 외곽에 탑승교의 승강장치인 드라이브컬럼(drive column)(40)이 장치되어, 항공기 기종에 따라 탑승교 접혀분의 높이와 항공기 도어의 높이를 일치시키도록 되어 있다. 또한, 드라이브컬럼(40) 하단부에는 휠캐리어(wheel carrier)(50)가 장치되고, 휠캐리어(50)에 구동모터(51)가 장치되어, 구동모터(51)가 바퀴(52)를 구동하므로, 턴넬(10)의 전후 및 좌우 이동이 가능하게 되어 있다.In this case, the turnnel 10 is formed of a width and a height of the first turnnel 11, the second turnnel 12, and the third turnnel 13 are different from each other, and can be accommodated inside each other. The overall length of the tunnel can be adjusted according to the model. In addition, the first tunnel 11 is provided with a drive column 40, which is a lifting device of a boarding bridge, on the outside, so that the height of the boarding bridge folded portion and the height of the aircraft door are matched according to the aircraft model. In addition, a wheel carrier 50 is installed at the lower end of the drive column 40, and a drive motor 51 is installed at the wheel carrier 50, so that the drive motor 51 drives the wheel 52. The front and rear and left and right movements of the turnnel 10 are made possible.
한편, 드라이브컬럼(40)은 제2도에서 도시되는 바와 같이, 휠캐리어(50) 상단에 하이드로유닛(41)이 설치되고, 하이드로유닛(41) 상부 양측에 각기 외측컬럼(42)과 내측컬럼(43)이 슬라이딩 가능하게 체결되며, 내측컬럼(43) 내부에 실린더(44)와 실린더로드(45)가 장치되고, 외측컬럼(42) 상단과 하단에 각기 마운팅브라켓(46)이 형성되어 마운팅브라켓(46)에 의해 턴넬(10)이 지지되어 있다.On the other hand, the drive column 40, as shown in Figure 2, the hydro unit 41 is installed on the top of the wheel carrier 50, the outer column 42 and the inner column respectively on both sides of the upper hydro unit 41 (43) is slidably fastened, the cylinder 44 and the cylinder rod 45 is installed inside the inner column 43, and mounting brackets 46 are formed at the top and bottom of the outer column 42, respectively, for mounting. The turnnel 10 is supported by the bracket 46.
이러한 드라이브컬럼(40)은 자중에 의해 하강되고, 하이드로유니트(41)의 작동에 의해 실린더(44)가 턴넬(10)을 상승시키게 되는데, 턴넬(10)의 높이를 감지하기 위해 컬럼 외측에 일정 간격으로 센서(미도시)가 부착되고, 체인(미도시)에 의해 구동되는 탑승교의 높이 감지장치(미도시)가 컬럼 외측에 취부되어 있다.The drive column 40 is lowered by its own weight, and the cylinder 44 raises the turnnel 10 by the operation of the hydro unit 41, which is fixed outside the column to sense the height of the turnnel 10. Sensors (not shown) are attached at intervals, and a height sensing device (not shown) of a boarding bridge driven by a chain (not shown) is mounted outside the column.
그런데, 이러한 종래 탑승교의 높이 감지장치는 체인(미도시)에 의해 드라이브 컬럼에 취부되어, 체인이 이탈되는 등의 고장이 잦은 단점이 있었다.However, such a height sensing device of a conventional boarding bridge is attached to the drive column by a chain (not shown), which has a disadvantage in that the chain is frequently broken.
본 고안의 목적은 상기와 같은 종래의 단점을 해결하기 위해, 외측컬럼과 내측컬럼에 래크와 피니언기어가 연동 가능하게 장치되고, 피니언기어에 의해 엔코더가 작동 가능하게 연결되어, 피니언기어가 엔코더를 구동하도록 하는 항공기 탑승교의 높이 감지장치 취부구조를 제공하는데 있다.An object of the present invention is to solve the above disadvantages, the rack and the pinion gear is interlocked to the outer column and the inner column, the encoder is operably connected by the pinion gear, the pinion gear to the encoder To provide a height sensor mounting structure of the aircraft boarding bridge to drive.
이하 첨부된 도면에 따라 본 고안의 기술적 구성을 상세히 설명하면 다음과 같다.Hereinafter, the technical configuration of the present invention according to the accompanying drawings in detail.
제3a도는 본 고안의 높이 감지장치 취부구조를 나타내는 부분 절개 분해 사시도이고, b도는 본 고안의 높이 감지장치 취부구조를 나타내는 횡단면도이며, 제4도는 본 고안 높이 감지장치의 회로도이다.Figure 3a is a partially cutaway exploded perspective view showing a height sensing device mounting structure of the present invention, b is a cross-sectional view showing a height sensing device mounting structure of the present invention, Figure 4 is a circuit diagram of the height sensing device of the present invention.
본 고안의 탑승교 승강장치도 제2도에서 도시된 바와같이, 휠캐리지(50) 상단에 하이드로유닛(41)이 고정되고, 하이드로유닛(41) 상부 양측에 각기 외측컬럼(42)과 내측컬럼(43)이 슬라이딩 가능하게 체결되며, 내측컬럼(43) 내부에 실린더(44)와 실린더로드(45)가 장치되고, 외측컬럼(42) 상단과 하단에 각기 마운팅브라켓(46)이 형성되어 마운팅브라켓(46)에 의해 턴넬(10)이 지지되는 것은 종래와 같다. 단, 본 고안은 제3도와 제4도에서 도시되는 바와같이, 내측컬럼(43) 외주면에 내부가 확대되는 요홈이 축방향으로 형성되어 요홈에 래크(47)가 견고하게 삽입되고, 래크(47)의 기어 전면쪽이 통공되게 외측컬럼(42)에 체결구멍(42a)이 형성되며, 외측컬럼(42)의 외주면에 탑승교의 높이 감지용 엔코더(49)가 취부되고, 체결구멍(42a)을 통해 래크(47)와 맞물리는 피니언기어(48)가 엔코더(49)에 커플링됨을 그 기술적 구성상의 기본 특징으로 한다.As shown in FIG. 2, the boarding bridge elevating device of the present invention has a hydro unit 41 fixed to the top of the wheel carriage 50, and an outer column 42 and an inner column respectively on both sides of the upper hydro unit 41. 43 is slidably fastened, the cylinder 44 and the cylinder rod 45 is installed inside the inner column 43, and mounting brackets 46 are formed at the upper and lower ends of the outer column 42, respectively, for mounting brackets. The turnnel 10 is supported by 46 is conventional. However, in the present invention, as shown in FIG. 3 and FIG. 4, the inner groove is formed on the outer circumferential surface of the inner column 43 in the axial direction so that the rack 47 is firmly inserted into the groove, and the rack 47 The fastening hole 42a is formed in the outer column 42 so that the front side of the gear is through, and the height detecting encoder 49 of the boarding bridge is attached to the outer circumferential surface of the outer column 42, and the fastening hole 42a is provided. The pinion gear 48 meshing with the rack 47 is coupled to the encoder 49 as a basic feature of the technical configuration.
이와 같이 구성되는 본 고안은 자중에 의해 턴넬(10)이 하강되고, 하이드로유니트(41)의 작동에 의해 실린더(44)가 외측컬럼(42)과 함께 턴넬(10)을 상승시키게 되며, 외측컬럼(42)의 상승 및 하강시 피니언기어(48)가 내측컬럼(43)에 고정된 래크(47)에 의해 회전된다. 또한, 회전되는 피니언기어(48)가 엔코더(49)에 기계적인 신호를 입력시키고, 엔코더(49)가 기계적인 신호를 전기적인 펄스신호로 변환시켜 출력하게 된다.The present invention constituted as described above, the turnnel 10 is lowered by its own weight, the cylinder 44 by the operation of the hydro unit 41 to raise the turnnel 10 together with the outer column 42, the outer column When the 42 is raised and lowered, the pinion gear 48 is rotated by the rack 47 fixed to the inner column 43. In addition, the pinion gear 48 to be rotated inputs a mechanical signal to the encoder 49, and the encoder 49 converts the mechanical signal into an electrical pulse signal and outputs the mechanical signal.
연기에서, 엔코더(49)는 1회전당 1000펄스의 로터리식이 적용되며, 피니언기어(48)에 연동되게 연결되고, 엔코더(49)의 출력측에 카운터(49a)가 연결되며, 카운터(49a)에 리세트용 리미트스위치(49b)가 장치된다.In the acting, the encoder 49 is applied with a rotary pulse of 1000 pulses per revolution, connected to the pinion gear 48 interlocked, the counter 49a is connected to the output side of the encoder 49, and connected to the counter 49a. A reset limit switch 49b is provided.
이러한 엔코더(49)는 피니언기어(48)의 회전에 따른 이동거리가 로터리를 통해 회전에 따른 펄스(pulse) 시그널이 전기적인 신호로 변환되어 출력되며, 전기적인 펄스시그널이 카운터(49a)에 입력되면, 펄스신호가 프리스케일(free scale) 기능을 가진 카운터(49a)가 이를 감지하여 모니터에 나타나게 된다. 또한, 높이를 감지하는 엔코더(49)의 위치가 일정높이에 이르면, 리미트스위치(49b)가 작동되어 입력된 일정높이의 치수가 카운터(49a)에 리세트된다.In the encoder 49, the movement distance according to the rotation of the pinion gear 48 is converted into an electrical signal by a pulse signal according to the rotation through a rotary, and the electrical pulse signal is input to the counter 49a. When the pulse signal is detected, the counter 49a having a free scale function detects it and appears on the monitor. In addition, when the position of the encoder 49 for detecting the height reaches a certain height, the limit switch 49b is operated to reset the input dimension of the predetermined height to the counter 49a.
한편, 카운터(49a)의 모니터에 디스플레이 되는 높이는, 피니언기어(48)의 지름에 따른 1회전당 이동거리와 로터리 1회전당의 펄스수에 의해, 1펄스단위로 카운터(49a)에 입력되어 나타난다.On the other hand, the height displayed on the monitor of the counter 49a is inputted to the counter 49a in units of one pulse by the movement distance per revolution according to the diameter of the pinion gear 48 and the number of pulses per rotary revolution. .
따라서, 이러한 본 고안은 높이 감지장치가 래크(47)와 피니언기어(48)에 의해 엔코더(49)가 구동되도록 하므로, 그 취부상태가 견고하여 고장요인이 없으며, 엔코더(49)의 펄스신호를 출력하여 카운터(49a)에 프리스케일 기능으로 나타내므로, 탑승교의 운전자가 보다 신속하고 정확하게 비행기와 접현할 수 있으며, 비행기 동체와 탑승교의 위치를 정확하게 맞춤으로써 기체손상을 방지할 수 있다. 또한, 일정높이를 통과할 때 리세트되는 기능이 부가되어, 원주에서 발생되는 누적오차를 제거해 준다.Therefore, the present invention allows the encoder 49 to be driven by the rack 47 and the pinion gear 48, so that the mounting state is firm, there is no failure factor, and the pulse signal of the encoder 49 is transmitted. Since the output is displayed on the counter 49a as a freescale function, the driver of the boarding bridge can make contact with the plane more quickly and accurately, and the aircraft body can be prevented by precisely aligning the position of the plane and the boarding bridge. It also adds the ability to reset when passing a certain height, eliminating cumulative errors that occur on the circumference.
이상에서 살펴본 바와 같이, 본 고안은 래크와 피니언 기어를 컬럼에 조합시키고, 피니언기어에 의해 로터리 엔코더가 구동되어, 엔코더에서 출력된 펄스신호가 모니터에 프리스케일로 나타내므로, 고장이 없이 신속하고 정밀한 감지를 얻을 수 있는 매우 유용한 것이다.As described above, the present invention combines the rack and pinion gear in a column, and the rotary encoder is driven by the pinion gear, so that the pulse signal output from the encoder is displayed on the monitor as freescale, so that it is quick and precise without trouble. It is very useful to get the detection.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019930011574U KR950003315Y1 (en) | 1993-06-29 | 1993-06-29 | Structure for height preception |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019930011574U KR950003315Y1 (en) | 1993-06-29 | 1993-06-29 | Structure for height preception |
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| Publication Number | Publication Date |
|---|---|
| KR950001123U KR950001123U (en) | 1995-01-03 |
| KR950003315Y1 true KR950003315Y1 (en) | 1995-04-25 |
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| KR2019930011574U KR950003315Y1 (en) | 1993-06-29 | 1993-06-29 | Structure for height preception |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101524235B1 (en) * | 2014-09-04 | 2015-05-29 | 한국공항공사 | Boarding bridge of Rotunda height adjustment device |
-
1993
- 1993-06-29 KR KR2019930011574U patent/KR950003315Y1/en not_active IP Right Cessation
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101524235B1 (en) * | 2014-09-04 | 2015-05-29 | 한국공항공사 | Boarding bridge of Rotunda height adjustment device |
| WO2016035963A1 (en) * | 2014-09-04 | 2016-03-10 | 한국공항공사 | Height adjustment device for rotunda of boarding bridge |
| US9834322B2 (en) | 2014-09-04 | 2017-12-05 | Ag Co., Ltd. | Height adjustment device for rotunda of boarding bridge |
Also Published As
| Publication number | Publication date |
|---|---|
| KR950001123U (en) | 1995-01-03 |
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