Oil level indicator for rotary wing aircraft transmission

Patent metadata

Field	Value
Publication number	US-9618378-B2
Application number	US-201313745886-A
Country	US
Kind code	B2
Filing date	Jan 21, 2013
Priority date	Jan 21, 2013
Publication date	Apr 11, 2017
Grant date	Apr 11, 2017

Abstract

A fluid level sensor for determining an amount of first fluid in a system is provided including a first substantially transparent sight glass mounted outside and fluidly coupled to a portion of the system. A level of first fluid in the first sight glass is indicative of the amount of first fluid in the system. A second substantially transparent sight glass has an independent closed loop containing a second fluid. The second sight glass is positioned adjacent outside the system. A plane of the second sight glass is arranged adjacent to a pivot point of the first fluid within the system. A level of second fluid in the second sight glass is indicative of the amount of first fluid corresponding to normal operation of the system. A comparison of the level of first fluid in the first sight glass and the level of second fluid in the second sight glass indicates if the amount of first fluid in the system requires adjustment.

First claim

What is claimed is:

1. A fluid level sensor for determining an amount of a first fluid in a system, the fluid level sensor having a pivot point, the sensor comprising:
a first substantially transparent sight glass distinct from and mounted outside the system, the first substantially transparent sight glass being fluidly coupled to the first fluid in the system such that a level of first fluid in the first sight glass is indicative of the amount of the first fluid in the system; and
a second substantially transparent sight glass having an independent closed loop containing a second fluid, the second sight glass being positioned outside the system such that a plane extending through the first sight glass and the second sight glass includes the pivot point, wherein a comparison of the level of first fluid in the first sight glass and a level of second fluid in the second sight glass indicates if the amount of first fluid in the system requires adjustment independent of an orientation of the system and if the level of first fluid and the level of second fluid are substantially identical, no adjustment of the amount of first fluid in the system is needed.

2. The fluid lever sensor according to claim 1 , wherein if the level of first fluid in the first sight glass is generally above the level of second fluid in the second sight glass, the system includes an excess of first fluid.

3. The fluid lever sensor according to claim 1 , wherein if the level of first fluid in the first sight glass is generally below the level of second fluid in the second sight glass are equal, more first fluid should be added to the system.

4. The fluid level sensor according to claim 1 , wherein the first fluid and the second fluid are substantially identical.

5. The fluid level sensor according to claim 4 , wherein the first fluid and the second fluid are a lubricant.

6. The fluid level sensor according to claim 1 , wherein the second sight glass includes a plurality of calibrated markings.

7. The fluid level sensor according to claim 1 , wherein the first sight glass and the second sight glass are positioned adjacent one another.

8. The fluid level sensor according to claim 7 , wherein the first sight glass and the second sight glass are formed integrally.

9. The fluid level sensor according to claim 8 , wherein the first sight glass and the second sight glass are substantially coplanar.

10. A method of evaluating an amount of first fluid in a system comprising:
viewing a level of the first fluid in a first sight glass, the first sight glass being distinct from and mounted to an exterior of the system, the first sight glass being fluidly coupled to the first fluid in the system such that a level of first fluid in the first sight glass is indicative of an amount of first fluid in the system;
viewing a level of a second fluid in a second sight glass, wherein a plane extending through the first sight glass and the second sight glass includes a pivot point of the system; and
comparing the level of the first fluid in the first sight glass and the level of the second fluid in the second sight glass to determine whether the amount of first fluid in the system requires adjustment, wherein if the level of first fluid and the level of second fluid are substantially identical, no adjustment of the amount of first fluid is needed.

11. The method according to claim 10 , further comprising adjusting the level of the first fluid in the system based on a difference between the level of the first fluid and the level of the second fluid.

12. The method according to claim 11 , wherein if the level of the first fluid is higher than the level of the second fluid, the system is adjusted by removing excess first fluid.

13. The method according to claim 11 , wherein if the level of the first fluid in the first sight glass is lower than the level of the second fluid in the second sight glass, the system is adjusted by adding first fluid.

14. The method according to claim 11 , wherein the system is adjusted until the level of the first fluid in the first sight glass aligns with a corresponding calibrated marking on the second sight glass.

15. A transmission system comprising:
a gearbox housing including an internal chamber containing a first fluid, wherein the first fluid in the internal chamber has a generally central pivot point; and
a fluid level sensor connected to the internal chamber, the fluid level sensor including:
a first substantially transparent sight glass mounted to an exterior of the gearbox housing and fluidly coupled to the internal chamber such that a level of first fluid in the first sight glass is indicative of the amount of the first fluid in the internal chamber; and
a second substantially transparent sight glass having an independent closed loop containing a second fluid, the second sight glass being positioned adjacent the exterior of the gearbox housing such that the a plane extending through the first sight glass and the second sight glass is includes the pivot point of the first fluid in the system, wherein a level of second fluid in the second sight glass is indicative of the amount of first fluid desired for normal operation, such that a comparison of the level of first fluid in the first sight glass and the level of second fluid in the second sight glass indicates if the amount of first fluid in the internal chamber requires adjustment independent of an orientation of the transmission system.

16. The transmission system according to claim 15 , wherein the transmission system is a portion of a drive system for a rotary wing aircraft.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Gmirya Yuriy

Classifications

• G01F23/0007

  for discrete indicating and measuring (G01F23/02 - G01F23/28 take precedence) · CPC title

• G01F22/00

  Methods or apparatus for measuring volume of fluids or fluent solid material, not otherwise provided for · CPC title

• B64D35/00

  Transmitting power from power plants to propellers or rotors; Arrangements of transmissions · CPC title

• G01F23/0046

  with a stationary probe, where a liquid specimen is separated from the mean mass and measured (by gauge glasses G01F23/02) · CPC title

• B64D33/00

  Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for · CPC title