Dual input pump assembly

Patent metadata

Field	Value
Publication number	US-12092107-B2
Application number	US-202117168057-A
Country	US
Kind code	B2
Filing date	Feb 4, 2021
Priority date	Feb 4, 2021
Publication date	Sep 17, 2024
Grant date	Sep 17, 2024

Abstract

A pump assembly, comprising a pump and housing having an inlet passage and an outlet passage. The pump includes inlet and outlet ports and opposing first and second drive inputs configured to be rotated together in a pumping direction to operate the pump. The pump can be installed in the housing in a first orientation, in which the first drive input is configured for being rotated by a drive source in a first external direction to operate the pump, and a second orientation, in which the second drive input is configured for being rotated by the drive source in a second external direction opposite of the first external direction to operate the pump. In both the first orientation and the second orientation, the inlet port is in fluid communication with the inlet passage and the outlet port is in fluid communication with the outlet passage.

First claim

What is claimed is:

1. A pump assembly, comprising:
a housing including an inlet passage and an outlet passage; and
a pump, including:
an inlet port and an outlet port; and
a first drive input and an opposing coaxial second drive input, the drive inputs configured to be rotated together in a pumping direction to operate the pump for causing fluid flow from the inlet port to the outlet port;

wherein the pump is disposed in the housing in:
a first orientation, in which the first drive input is exposed to an exterior of the housing and engages a drive source, which rotates the first input in a first external direction for causing the pump to rotate in the pumping direction; or
a second orientation, in which the second drive input is exposed to an exterior of the housing and engages the drive source, which rotates the second input in a second external direction opposite of the first external direction for causing the pump to rotate in the pumping direction;

wherein, when the pump is in either of the first orientation or the second orientation, the inlet port is in fluid communication with the inlet passage and the outlet port is in fluid communication with the outlet passage.

2. The pump assembly of claim 1 , wherein the housing further includes a cylindrical aperture in which the pump is installed.

3. The pump assembly of claim 1 , wherein the housing further includes an end cap coupled to the housing.

4. The pump assembly of claim 1 , wherein:
the housing further includes an aperture formed through the housing and an end cap disposed on an end of the aperture; and
the aperture is sized for receiving the pump.

5. The pump assembly of claim 4 , wherein, when the pump is inserted into the aperture, either of the first drive input or the second drive input is disposed within a volume formed between the end cap and the pump.

6. The pump assembly of claim 1 , wherein the pump is a gerotor pump.

7. The pump assembly of claim 1 , wherein the inlet port and the outlet port oppose each other.

8. An aircraft, comprising:
a first oil pump drive source that rotates in a first external direction and a second oil pump drive source that rotates in a second external direction opposite of the first external direction;
first and second oil pump housings corresponding to the first and second oil pump drive sources, respectively, each of the first and second oil pump housings including an inlet passage and an outlet passage; and
a pump configured for use in either of the first and second oil pump housings, the pump including:
an inlet port and an outlet port; and
a first drive input and an opposing coaxial second drive input, the drive inputs configured to be rotated together in a pumping direction to operate the pump for causing fluid flow from the inlet port to the outlet port;

wherein the pump is disposed in:
the first oil pump housing in a first orientation in which the first drive input is exposed to an exterior of the first oil pump housing and is rotated by the first oil pump drive source; or
the second oil pump housing in a second orientation in which the second drive input is exposed to an exterior of the second oil pump housing and is rotated by the second oil pump drive source;

wherein, when the pump is installed in either the first oil pump housing or the second oil pump housing, the inlet port is in fluid communication with the corresponding inlet passage and the outlet port is in fluid communication with the corresponding outlet passage.

9. The aircraft of claim 8 , wherein each of the first oil pump housing and second oil pump housing includes a body with a cylindrical aperture in which the pump is installed.

10. The aircraft of claim 8 , wherein each of the first oil pump housing and the second oil pump housing further includes an end cap coupled to the oil pump housing.

11. The aircraft of claim 8 , wherein the inlet port and the outlet port oppose each other.

12. The aircraft of claim 8 , wherein the pump is a gerotor pump.

Assignees

• Bell Textron Inc
• Textron Innovations Inc

Inventors

• Tiprigan Ezra Mike
• Speller Charles Hubert

Classifications

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title

• F01M2001/0238

  Rotary pumps · CPC title

• F01M2001/0284

  mounting of the pump · CPC title

• F01M1/02 Primary

  using lubricating pumps (pumps in general F04; lubricating pumps per se F16N) · CPC title

• F04C2210/206

  Oil · CPC title