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KR840000402Y1 - Tire of aircraft - Google Patents

Tire of aircraft Download PDF

Info

Publication number
KR840000402Y1
KR840000402Y1 KR2019820000046U KR820000046U KR840000402Y1 KR 840000402 Y1 KR840000402 Y1 KR 840000402Y1 KR 2019820000046 U KR2019820000046 U KR 2019820000046U KR 820000046 U KR820000046 U KR 820000046U KR 840000402 Y1 KR840000402 Y1 KR 840000402Y1
Authority
KR
South Korea
Prior art keywords
tire
aircraft
landing
wheel
present
Prior art date
Application number
KR2019820000046U
Other languages
Korean (ko)
Other versions
KR830002828U (en
Inventor
김상호
Original Assignee
김상호
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 김상호 filed Critical 김상호
Priority to KR2019820000046U priority Critical patent/KR840000402Y1/en
Publication of KR830002828U publication Critical patent/KR830002828U/en
Application granted granted Critical
Publication of KR840000402Y1 publication Critical patent/KR840000402Y1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/54Floats
    • B64C25/56Floats inflatable

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)

Abstract

내용 없음.No content.

Description

항공기용 타이어Aircraft tires

제1도는 본 고안의 전체 사시도.1 is an overall perspective view of the present invention.

제2도는 본 고안의 A-A선 단면도.2 is a cross-sectional view taken along line A-A of the present invention.

제3도는 본 고안의 B-B선 확대 단면도.3 is an enlarged cross-sectional view taken along line B-B of the present invention.

제4도는 본 고안의 사용상태 측면도.Figure 4 is a side view of the state of use of the present invention.

* 도면의 주요부분에 대한 부호의 설명* Explanation of symbols for main parts of the drawings

1 : 타이어 동체 2, 2a : 바람잡이 호형 바켓1: tire fuselage 2, 2a: wind-shaped arc bucket

본 고안은 착륙시 착륙장치에 의하여 바퀴가 노출되면 진행방향으로 바퀴가 회전되게 하기 위하여 타이어의 양측면에 바람잡이 호형 바켓을 일체로 형성한 항공기용 타이어에 관한 것으로 종래에도 바퀴를 진행방향으로 회전시켜 주기 위하여 바퀴 고정 휘일에 날개를 형성한 것이 있으나 이는 경이 적은 휘일의 주연에 날개를 형성하였기 때문에 공기저항이 필요한 양에 미치지 못하여 착륙시 생기는 마찰손실을 줄이기에 효과가 적고 한쪽에만 설치되었으므로 안전운행을 보장할 수 없었다.The present invention relates to an aircraft tire in which wind wheel arc brackets are integrally formed on both sides of a tire so that the wheel rotates in the traveling direction when the wheel is exposed by the landing device during landing. In order to ensure the safe operation, the wing is formed on the wheel fixing wheel. However, since the wing is formed on the peripheral edge of the wheel, the air resistance is less than the required amount, so it is less effective to reduce the frictional loss caused by the landing. I could not.

본 고안은 이와 같은 점을 감안하여 항공기의 대형화 및 고속화됨에 따라 착륙시 타이어의 마모가 많아지고 착륙장치에 심한 충격을 받게 되는 것을 최대한으로 줄이기 위하여 기존 항공기용 타이어 좌우 양측에 대칭으로 여러개의 바람잡이 호형 바켓을 형성하여 착륙장치를 기체 밖으로 내렸을때 활공기류의 힘으로 바퀴가 활주시와 같은 방향으로 회전케 하므로서 활주로에 착지시에 타이어에 심한 마모가 생기지 않고 착륙장치에도 심한 충격을 주지 않게 한 것으로 첨부도면에 의하여 상세히 설명하면 다음과 같다.In consideration of the above, the present invention has a large number of wind-shaped arcs symmetrically on both sides of the existing aircraft tires in order to maximize the wear and tear of the tire and the severe impact on the landing gear. When the landing gear is lowered out of the aircraft by forming a bucket, the wheels are rotated in the same direction as the slide by the force of the gliding air, so that the tire does not cause severe wear when landing on the runway and does not give a heavy impact to the landing gear. Referring to the drawings in detail as follows.

타이어 동체(1)의 양측 주연에 대칭으로 바람잡이 호형 바켓(2)(2a)을 일방향으로 위치하게 일정간격으로 다수 돌설하여서 된 것이다.It is made by protruding a large number of wind trapping arc-shaped baskets (2) (2a) at a predetermined interval symmetrically on both sides of the tire body (1) in one direction.

미설명부호 3은 타이어 고정휘일이다.Reference numeral 3 is a tire fixed wheel.

이상과 같이 된 본 고안은 작용 효과를 설명하면 다음과 같다.The present invention made as described above will be described as follows.

타이어 동체(1)의 양측 주연에 바람잡이 호형 바켓(2)(2a)을 일방향으로 위치되게 일정 간격으로 다수 형성하여 타이어의 최상부에는 기류의 저항을 최소로 받게 하고 타이어의 최하부에서 기류의 저항을 최대로 받게 하여 활주시의 회전방향과 같은 방향으로 바퀴가 회전되게 하므로써 착지시에 타이어 동체(1)의 마모를 최대한으로 줄이는 동시에 착륙장치에 발생하는 충격을 적게 받게 한 것인데 본 고안품의 타이어를 사용할 경우에는 타이어의 회전확인장치를 설치하면 더욱 효과적으로 타이어의 마모와 착륙장치의 충격을 효과적으로 완화시켜 줄 수 있는 이점이 있는 것이다.A large number of wind-shaped arc baskets (2) (2a) are formed at regular intervals on both sides of the tire fuselage (1) so as to be located in one direction, so that the resistance of the airflow is minimized at the top of the tire and the resistance of the airflow is at the bottom of the tire The wheels are rotated in the same direction as the rotational direction of the slide, thereby minimizing the wear of the tire body (1) at the time of landing and at the same time reducing the impact of the landing gear. There is an advantage that can effectively alleviate the wear of the tire and the impact of the landing gear by installing the tire rotation check device.

Claims (1)

타이어 동체(1)의 양측 주연에 공지의 대칭으로 바람잡이 호형 바켓(2)(2a)을 일방향으로 위치하게 일정간격으로 다수 돌설하여서 된 항공기용 타이어.A tire for an aircraft in which a plurality of wind-shaped arc baskets (2) (2a) are located in one direction at regular intervals on both sides of a tire body (1) in a known symmetry.
KR2019820000046U 1982-01-06 1982-01-06 Tire of aircraft KR840000402Y1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR2019820000046U KR840000402Y1 (en) 1982-01-06 1982-01-06 Tire of aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR2019820000046U KR840000402Y1 (en) 1982-01-06 1982-01-06 Tire of aircraft

Publications (2)

Publication Number Publication Date
KR830002828U KR830002828U (en) 1983-11-25
KR840000402Y1 true KR840000402Y1 (en) 1984-03-12

Family

ID=19223709

Family Applications (1)

Application Number Title Priority Date Filing Date
KR2019820000046U KR840000402Y1 (en) 1982-01-06 1982-01-06 Tire of aircraft

Country Status (1)

Country Link
KR (1) KR840000402Y1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020072327A (en) * 2001-03-08 2002-09-14 공종철 Prefabricated yachts, boats, ships, building equipment, machinery, toys, etc.
KR100423935B1 (en) * 2001-02-22 2004-03-30 공종철 Prefabricated yachts, boats, ships, building equipment, machinery, toys, etc.
KR100423936B1 (en) * 2001-02-22 2004-05-03 공종철 Prefab boat. yacht. Ship. Building equipment. Hardware. Parts such as toys and how to assemble.
WO2007086635A1 (en) * 2006-01-24 2007-08-02 Kim, Sung Bae Airplane tire with air pocket
KR100844451B1 (en) * 2006-09-29 2008-07-07 김성배 The air frame of adhersive airplane tire

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100423935B1 (en) * 2001-02-22 2004-03-30 공종철 Prefabricated yachts, boats, ships, building equipment, machinery, toys, etc.
KR100423936B1 (en) * 2001-02-22 2004-05-03 공종철 Prefab boat. yacht. Ship. Building equipment. Hardware. Parts such as toys and how to assemble.
KR20020072327A (en) * 2001-03-08 2002-09-14 공종철 Prefabricated yachts, boats, ships, building equipment, machinery, toys, etc.
WO2007086635A1 (en) * 2006-01-24 2007-08-02 Kim, Sung Bae Airplane tire with air pocket
KR100844451B1 (en) * 2006-09-29 2008-07-07 김성배 The air frame of adhersive airplane tire

Also Published As

Publication number Publication date
KR830002828U (en) 1983-11-25

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