Adjustable scissor control link

Patent metadata

Field	Value
Publication number	US-9315265-B2
Application number	US-201313953260-A
Country	US
Kind code	B2
Filing date	Jul 29, 2013
Priority date	Jul 29, 2013
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

A control link disposed to transfer rotor shaft rotation from an elongate element rotatable with a shaft to a rotatable element is provided and includes a structure terminating at a first end thereof as a mating element, which is securable to the elongate element such that the elongate element is rotatable about an axis defined through the mating element and such that a moment reaction in opposition to structure rotation about the elongate element is generated and a rod coupled to the rotatable element being and configured to be coupled to a second end of the structure at variable distances relative to the rotatable element.

First claim

What is claimed is:

1. A control link disposed to transfer rotor shaft rotation from a walking beam rotatable with the rotor shaft to a rotating swashplate, the control link comprising:
a structure including:
a first sidewall and a second sidewall terminating at respective first ends as mating elements which are securable to the walking beam such that the walking beam is rotatable about an axis defined through the mating elements and such that a moment reaction in opposition to structure rotation about the walking beam is generated, the first sidewall and the second side wall being convergent toward one another at respective second ends and connecting to each other at their second ends to define a through-hole,
rib members connected to each of the first sidewall and second sidewall between the first ends and second ends; and

a rod coupled to the rotating swashplate and configured to be coupled to a second end of the structure and to the rib members at variable distances relative to the rotating swashplate.

2. The control link according to claim 1 , further comprising a hinge-pin receivable by the mating elements and the walking beam.

3. The control link according to claim 1 , further comprising:
fastening elements configured to fasten the rod to the rib members at the variable distances.

4. The control link according to claim 1 , wherein the mating elements are at a distance from one another.

5. A rotor control system for use with a rotor and an airframe, comprising:
a rotor shaft disposed to support rotation of the rotor;
a stationary swashplate connected to the airframe;
a rotating swashplate disposed to rotate relative to the stationary swashplate;
a mixer housing and primary pitch control links disposed in the rotor shaft, the primary pitch control links being coupled to pivotable elongate elements, which are pivotable about the mixer housing; and
secondary pitch control links respectively coupled to the elongate elements and the rotating swashplate to control a position of the primary pitch control links via the elongate elements,
at least one of the secondary pitch control links being configured as in claim 1 and being adjustable.

6. The rotor control system according to claim 5 , wherein the elongate elements are arrayed uniformly about the mixer housing.

7. The rotor control system according to claim 6 , wherein two or more elongate elements are provided about the mixer housing for respective association with each of a same number of primary pitch control links.

8. The rotor control system according to claim 6 , wherein the secondary pitch control links comprise:
the at least one of the adjustable scissor control links; and
at least one adjustable control link.

9. The rotor control system according to claim 8 , wherein the at least one of the secondary pitch control links comprises:
sidewalls terminating at respective first ends thereof as mating elements, which are securable to an elongate element such that the elongate element is rotatable about an axis defined through the mating elements, the sidewalls connecting at respective second ends thereof, which are formed to define a through-hole through which a rod coupled to the rotating swashplate is extendible; and
ribs connected to each of the sidewalls between the first and second ends and configured to be coupled to the rod at variable distances relative to an end of the rod.

10. The rotor control system according to claim 9 , further comprising a hinge-pin receivable by the mating elements and the elongate element.

11. The rotor control system according to claim 9 , further comprising fastening elements to fasten the rod to the ribs.

12. The rotor control system according to claim 9 , wherein the mating elements each comprise a pad at a distance from the other pad.

13. The rotor control system according to claim 9 , wherein the respective second ends of the sidewalls are convergent.

14. The rotor control system according to claim 9 , wherein the mating elements are configured to prevent rotation of the sidewalls about the elongate elements.

15. A helicopter, comprising:
an airframe;
a rotor, which is rotatable to provide lift force for the airframe; and
a rotor control system configured to control the rotor, the rotor control system comprising:
a rotor shaft disposed to support rotation of the rotor;
a stationary swashplate connected to the airframe;
a rotating swashplate disposed to rotate relative to the stationary swashplate;
a mixer housing and primary pitch control links disposed in the rotor shaft, the primary pitch control links being coupled to pivotable elongate elements, which are pivotable about the mixer housing; and
secondary pitch control links respectively coupled at ends thereof to the elongate elements and the rotating swashplate to control a position of the primary pitch control links via the elongate elements,
at least one of the secondary pitch control links being configured to transmit rotation of the rotor shaft to the rotating swashplate and being configured as in claim 1 and adjustable.

16. The helicopter according to claim 15 , wherein the adjustable scissor control link exclusively transmits the rotation of the rotor shaft to the rotating swashplate.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Halcom Lance
• Baskin Bryan Kenneth
• D Anna Frank P
• Darrow David A
• Hunter David H

Classifications

• B64C27/605 Primary

  including swash plate, spider or cam mechanisms · CPC title

• B64C27/06

  with single rotor · CPC title

• B64C27/59 Primary

  mechanical · CPC title