Transport machine and aircraft

Patent metadata

Field	Value
Publication number	US-2016207635-A1
Application number	US-201514965494-A
Country	US
Kind code	A1
Filing date	Dec 10, 2015
Priority date	Jan 19, 2015
Publication date	Jul 21, 2016
Grant date	—

Abstract

The present invention provides a transport machine such as an aircraft ( 1 ), into the transport machine, an electronic device ( 30 ) that generates an electromagnetic wave is carried, the transport machine including: a cable ( 27 ) to which the electronic device ( 30 ) is connected; a clamp ( 31 ) having a clamp body ( 32 ), the clamp body ( 32 ) holding the cable ( 27 ); and a medium ( 31 A) that is provided inside the clamp body ( 32 ) to absorb the electromagnetic wave conducted through the cable ( 27 ).

First claim

What is claimed is:

1 . A transport machine into which an electronic device that generates an electromagnetic wave is carried, the transport machine comprising:
a cable to which the electronic device is connected; a clamp having a clamp body, the clamp body holding the cable; and a medium that is provided inside the clamp body to absorb the electromagnetic wave conducted through the cable.

2 . The transport machine according to claim 1 ,
wherein the transport machine is an aircraft comprising an airframe, the electronic device being carried into the airframe, the airframe comprises the cable, the clamp, and the medium.

3 . The transport machine according to claim 1 ,
wherein the medium is a ferrite core containing ferrite.

4 . The transport machine according to claim 1 ,
wherein the clamp includes the clamp body that internally receives the cable, and the medium that is interposed between the clamp body and the cable.

5 . The transport machine according to claim 4 ,
wherein the clamp further includes a cover that is fitted to at least the clamp body out of the clamp body and the medium.

6 . The transport machine according to claim 3 ,
wherein the ferrite core includes a plurality of segments, and has an annular shape as a whole.

7 . The transport machine according to claim 1 ,
wherein the medium absorbs the electromagnetic wave in a band of 100 MHz or more.

8 . The transport machine according to claim 1 ,
wherein the medium is configured to function as a high-pass filter.

9 . The transport machine according to claim 1 ,
wherein the transport machine comprises a floor panel, and the clamp body is fastened to the floor panel.

10 . The transport machine according to claim 1 ,
wherein the clamp body has a P shape, the medium is an annular ferrite core, and the annular ferrite core is disposed inside the clamp body.

11 . The transport machine according to claim 10 ,
wherein the clamp further comprises a resin cover, and the cover is fitted to the clamp body and the ferrite core.

12 . The transport machine according to claim 1 ,
wherein the cable is a power supply line for supplying electric power to devices mounted on the transport machine or a signal line for transmitting and receiving signals between the devices.

13 . An aircraft comprising an airframe into which an electronic device that generates an electromagnetic wave is carried,
wherein the airframe includes: a cable to which the electronic device is connected; a clamp having a clamp body, the clamp body holding the cable; and a medium that is provided inside the clamp body to absorb the electromagnetic wave conducted through the cable.

14 . The aircraft according to claim 13 ,
wherein the medium is a ferrite core containing ferrite.

15 . The aircraft according to claim 13 ,
wherein the clamp includes the clamp body that internally receives the cable, and the medium that is interposed between the clamp body and the cable.

16 . The aircraft according to claim 15 ,
wherein the clamp further includes a cover that is fitted to at least the clamp body out of the clamp body and the medium.

17 . The aircraft according to claim 14 ,
wherein the ferrite core includes a plurality of segments, and has an annular shape as a whole.

18 . The aircraft according to claim 13 ,
wherein the medium absorbs the electromagnetic wave in a band of 100 MHz or more.

19 . The aircraft according to claim 13 ,
wherein the airframe comprises a floor panel, and the clamp body is fastened to the floor panel.

20 . The aircraft according to claim 13 ,
wherein the clamp body has a P shape, the medium is an annular ferrite core, and the annular ferrite core is disposed inside the clamp body.

Assignees

• Mitsubishi Aircraft Corp

Inventors

• Yokoi Takashi

Classifications

• B64D45/00 Primary

  Aircraft indicators or protectors not otherwise provided for · CPC title

• H02G3/32

  using mounting clamps · CPC title

• B64D45/0063

  by avoiding the use of electronic equipment during flight, e.g. of mobile phones or laptops · CPC title