Telescoping electrical cable

Patent metadata

Field	Value
Publication number	US-10422301-B2
Application number	US-201514797930-A
Country	US
Kind code	B2
Filing date	Jul 13, 2015
Priority date	Jul 13, 2015
Publication date	Sep 24, 2019
Grant date	Sep 24, 2019

Abstract

An aircraft includes a jet engine and a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of the jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine. A jet engine includes a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of a jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine.

First claim

What is claimed:

1. An aircraft, comprising:
a jet engine assembly; and
a telescopic tube assembly positioned on the jet engine assembly, the telescopic tube assembly comprising:
one end portion of the telescopic tube assembly is secured to a thrust reverser translating sleeve of the jet engine assembly; and
an opposing end portion of the telescopic tube assembly is secured to a fixed portion of the of the jet engine assembly, wherein:
an electrical cable positioned within and extends along the telescopic tube assembly; and
the telescopic tube assembly extends from opposing end portion such that with thrust reverser translating sleeve in a deployed position an opening is positioned between the thrust reverser translating sleeve and the fixed portion of the jet engine assembly with the telescopic tube assembly extending across the opening; and

at least two tube segments, wherein:
a first tube segment has a greater interior dimension than an exterior dimension of a second tube segment permitting the second tube segment to slide within the first tube segment;
the first tube segment comprises one of a projection and groove extending along a length of the first tube segment; and
the second tube segment comprises the other of the projection and the groove of the first tube segment, wherein:
the one of the projection and the groove of the first tube segment comprises a size complimentary to engage the other of the one of the projection and the groove of the second tube segment; and
rotation of one of the first and second tube segments, in turn, imparts rotation to the other of the first and second tube segments wherein the one end portion of the telescopic tube assembly comprises a lever, which rotates with the first and second tube segments and which engages a constricting cable which extends circumferentially about petals associated with the jet engine assembly.

2. The aircraft of claim 1 , wherein the jet engine is secured to the aircraft.

3. The aircraft of claim 1 , wherein the telescopic tube assembly comprises a first length with the thrust reverser translating sleeve in a stowed position.

4. The aircraft of claim 1 , wherein the telescopic tube assembly comprises a second length with the thrust reverser translating sleeve in the deployed position, wherein the telescopic tube assembly extends across the opening positioned between the thrust reverser translating sleeve in the deployed position and the fixed portion of the jet engine assembly.

5. The aircraft of claim 1 , further including the cable which extends within and along the telescopic tube assembly wherein the cable comprises a coiled configuration such that the cable extends in length with a tension force placed on and along a length of the cable.

6. The aircraft of claim 1 , wherein the opposing end portion of the telescopic tube assembly is secured to the fixed portion of the jet engine with a bearing, such that the bearing permits the opposing end portion of the telescopic tube assembly to rotate relative to the fixed portion of the jet engine assembly and the one end portion of the telescopic tube assembly is secured to the thrust reverser translating sleeve with a second bearing which permits the telescopic tube assembly to rotate relative to the thrust reverser translating sleeve.

7. The aircraft of claim 6 , further including a drive motor having a first drive gear secured to the drive motor and engaged to a second drive gear, which is secured to the telescopic tube assembly, such that the drive motor rotates the first drive gear and in turn rotates the second drive gear thereby rotating the telescopic tube assembly.

8. A jet engine assembly, comprising:
a telescopic tube assembly positioned on the jet engine assembly, comprising:
at least two tube segments, wherein:
a first tube segment has a greater interior dimension than an exterior dimension of a second tube segment permitting the second tube segment to slide within the first tube segment;
the first tube segment comprises one of a projection and groove extending along a length of the first tube segment; and
the second tube segment comprises the other of the projection and the groove of the first tube segment, wherein:
the one of the projection and the groove of the first tube segment comprises a size complimentary to engage the other of the one of the projection and the groove of the second tube segment, and
rotation of one of the first and second tube segments, in turn, imparts rotation to the other of the first and second tube segments;

one end portion of the telescopic tube assembly is secured to a thrust reverser translating sleeve of the jet engine assembly, comprises one of the first and second tube segment; and
an opposing end portion of the telescopic tube assembly is secured to a fixed portion of the of the jet engine assembly, comprises the other of the one of the first and second tube segment, wherein:
the one end portion of the telescopic tube assembly comprises a lever which rotates with the first and second tube segments and which engages a constricting cable which extends circumferentially about petals associated with the jet engine assembly; and
the telescopic tube assembly extends from the fixed portion such that with thrust reverser translating sleeve in a deployed position an opening is positioned between the thrust reverser translating sleeve and the fixed portion of the jet engine assembly and the telescopic tube assembly extends across the opening wherein an electrical cable is positioned within and extends along the telescopic tube assembly.

9. The jet engine of claim 8 , wherein the jet engine assembly is secured to an aircraft.

10. The jet engine of claim 8 , wherein the telescopic tube assembly comprises a first length with the thrust reverser translating sleeve in a stowed position.

11. The jet engine of claim 8 , wherein the telescopic tube assembly comprises a second length with the thrust reverser translating sleeve in the deployed position, wherein the telescopic tube assembly extends across the opening positioned between the thrust reverser translating sleeve in the deployed position and the fixed portion of the jet engine assembly.

12. The jet engine of claim 8 , further including the cable which extends within and along the telescopic tube assembly wherein the cable comprises a coiled configuration such that the cable extends in length with a tension force placed on and along a length of the cable.

13. The jet engine of claim 8 , wherein the opposing end portion of the telescopic tube assembly is secured to the fixed portion of the jet engine assembly with a bearing, such that the bearing permits the opposing portion end of the telescopic tube assembly to rotate relative to the fixed portion of the jet engine assembly and the one end portion of the telescopic tube assembly is secured to the thrust reverser translating sleeve with a second bearing which permits the telescopic tube assembly to rotate relative to the sleeve.

14. The jet engine of claim 13 , further including a drive motor having a first drive gear secured to the drive motor and engaged to a second drive gear, which is secured to the telescopic tube assembly, such that the drive motor rotates the first drive gear and in turn rotates the second drive gear thereby rotating the telescopic tube assembly.

15. A method for protecting a cable of a jet engine assembly, comprising the steps of:
providing a telescopic tube assembly positioned on the jet engine assembly, comprising: at least two tube segments, wherein:
a first tube segment having an interior dimension; a second tube s

Assignees

• Boeing Co

Inventors

• Karnofski Kent Edmund
• Jasklowski Chris T
• Burghdoff Michael Jay

Classifications

• F02K1/72

  the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow · CPC title

• F02K1/09

  by axially moving an external member, e.g. a shroud (F02K1/12 takes precedence) · CPC title

• B64D33/04

  of exhaust outlets or jet pipes · CPC title

• F05D2260/50

  Kinematic linkage, i.e. transmission of position · CPC title

• F02K1/16

  conjointly with another control · CPC title