Assembly with blind installation capability

Patent metadata

Field	Value
Publication number	US-9453525-B2
Application number	US-201414769344-A
Country	US
Kind code	B2
Filing date	Feb 13, 2014
Priority date	Feb 26, 2013
Publication date	Sep 27, 2016
Grant date	Sep 27, 2016

Abstract

An assembly includes a pin, a fastener, a first element, and a paddle. The pin includes a first channel. The fastener extends within the pin and has a head extending from a first end of the pin. The first element is mounted to the fastener and is capable of translation relative to the pin with rotation of the fastener. The paddle is movably connected to the first element and disposed within the first channel. At least a portion of the paddle extends from the first channel to protrude from the pin with translation of the first element.

First claim

The invention claimed is:

1. An assembly comprising:
a pin including a first channel and a second channel;
a fastener extending within the pin and having a head extending from a first end of the pin;
a first element mounted to the fastener, wherein the first element is capable of translation relative to the pin with rotation of the fastener, and wherein the second channel is adapted to receive the first element; and
a paddle movably connected to the first element and disposed within the first channel, wherein at least a portion of the paddle extends from the first channel to protrude from the pin with translation of the first element.

2. The assembly of claim 1 , wherein the first channel allows the paddle to pivot relative to the first element and protrude from the pin.

3. The assembly of claim 1 , wherein the first element is disposed within the pin.

4. The assembly of claim 1 , further comprising a second element mounted to the fastener, wherein the second element contacts the paddle.

5. The assembly of claim 4 , wherein the second element is capable of translation relative to the pin with rotation of the fastener.

6. The assembly of claim 5 , wherein the second element translates in an opposing direction to the first element.

7. The assembly of claim 6 , wherein the fastener includes a clockwise thread for a portion mounted to the first element and a counter-clockwise thread for a second portion mounted to the second element.

8. The assembly of claim 4 , wherein the second element translates along the first channel.

9. The assembly of claim 4 , wherein when the paddle reaches a fully deployed position the first element contacts the second element.

10. The assembly of claim 1 , wherein when the paddle reaches a fully deployed position the paddle contacts the pin.

11. The assembly of claim 1 , wherein the first element is capable of translation to retract the paddle into the first channel such that the paddle does not protrude from the pin.

12. A gas turbine engine comprising:
a pin including a first channel;
a fastener extending within the pin and having a head extending from a first end of the pin;
a first element mounted to the fastener within the pin, wherein the first element is capable of translation relative to the pin with rotation of the fastener;
a second element mounted to the fastener; and
a paddle pivotally connected to the first element and disposed within the first channel, wherein translation of the first element and contact with the second element pivots the paddle to protrude from the pin.

13. The gas turbine engine of claim 12 , wherein the second element is capable of translation relative to the pin with rotation of the fastener.

14. The gas turbine engine of claim 13 , wherein the second element translates in an opposing direction to the first element.

15. The gas turbine engine of claim 12 , wherein the second element translates along the first channel.

16. The gas turbine engine of claim 12 , further comprising:
a clevis having a first lug and a second lug;
a first bushing disposed in the first lug; and
a second bushing disposed in the second lug, wherein a preload force is transferred from the second element through the paddles to one or both of the first bushing and first lug.

17. The gas turbine engine of claim 16 , further comprising a washer abutting the second bushing, wherein the washer applies a force to one or both of the second bushing and second lug.

18. A method comprising:
providing a pin having a first channel;
rotating a fastener to translate a first element within the pin,
pivoting a paddle relative to the first element such that the paddle tracks along the first channel to protrude at least a portion of the paddle from the pin; and
translating a second element mounted to the fastener and contacting the paddle.

Assignees

• United Technologies Corp

Inventors

• Foster Joseph P

Classifications

• B64D27/406

  Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links · CPC title

• B64D27/402

  comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant · CPC title

• B64D27/40

  Arrangements for mounting power plants in aircraft · CPC title

• B64D27/26

  Operations & Transport · mapped topic

• F16B5/02

  by means of fastening members using screw-thread ({F16B5/0004 takes precedence}; construction of screw-threaded connections F16B25/00 - F16B39/00) · CPC title