JPS6311209U

JPS6311209U -

Info

Publication number: JPS6311209U
Application number: JP10457886U
Authority: JP
Priority date: 1986-07-08
Filing date: 1986-07-08
Publication date: 1988-01-25

Description

[Brief explanation of the drawing]

第１図は本考案航空機用タイヤの第１実施例を
示す側面図、第２図ａはタイヤ本体の周側面に固
着した風圧抵抗部としてのブレードの側面図、第
２図ｂは同平面図、第３図ａは本考案航空機用タ
イヤの第２の実施例を示す側面図、第３図ｂはブ
レード部分の平面図である。１…タイヤ本体、２…トレツド、３…ビード、
４…ブレード、５…サイドウオール、６…先端部
、７…受圧部、８…凹部、１０…タイヤ。 Fig. 1 is a side view showing the first embodiment of the aircraft tire of the present invention, Fig. 2a is a side view of a blade as a wind pressure resistance part fixed to the circumferential side of the tire body, and Fig. 2b is a plan view of the same. FIG. 3a is a side view showing a second embodiment of the aircraft tire of the present invention, and FIG. 3b is a plan view of the blade portion. 1... Tire body, 2... Tread, 3... Bead,
4...Blade, 5...Sidewall, 6...Tip, 7...Pressure receiving part, 8...Recess, 10...Tire.

Claims

[Claims for Utility Model Registration] (1) An aircraft tire characterized by being constructed by disposing a plurality of wind pressure resistance parts on the circumferential side of the tire body. (2) The aircraft tire according to claim 1, wherein the wind pressure resistance portion has a shape that increases resistance in a direction opposite to wind pressure and decreases resistance in the rotation direction of the tire. (3) The wind pressure resistance part is integrally protruded from the circumferential side of the tire body using the same material or different materials, or is formed separately and then fixed to the circumferential side of the tire body.Registered as a utility model. An aircraft tire according to claim 1. (4) The wind pressure resistance section is formed of a tip end and a pressure receiving section, and is made up of a plurality of blades that are gradually thinner and narrower from the pressure receiving section to the tip. Scope of Utility Model Registration Claim 1 Aircraft tires listed. (5) The wind pressure resistance section is formed of a tip end and a pressure receiving section, and is formed of a plurality of blades that are gradually thinner and narrower from the pressure receiving section to the tip end, and is located in front of the pressure receiving section of each blade. 2. The aircraft tire according to claim 1, wherein the aircraft tire comprises a recess provided in the sidewall surface of the tire body.