Lubrication pressue control of a power transmission device for helicopter

Patent metadata

Field	Value
Publication number	US-11618556-B2
Application number	US-201916722354-A
Country	US
Kind code	B2
Filing date	Dec 20, 2019
Priority date	Jun 27, 2017
Publication date	Apr 4, 2023
Grant date	Apr 4, 2023

Abstract

A transmission device includes a casing accommodating a transmission gear and having an oil sump for retaining oil. The oil in the oil sump flows from a lubrication pump through a lubrication passage and is injected to the transmission gear. A connection portion is provided in a part of the lubrication passage, which part is disposed outside the casing. A direction control valve is provided downstream of the lubrication pump and upstream of the connection portion in the lubrication passage with respect to a flow direction of the oil. The direction control valve is configured to open the lubrication passage when a hydraulic pressure in the lubrication passage exceeds a predetermined value and to close the lubrication passage when the hydraulic pressure is equal to or lower than the predetermined value.

First claim

What is claimed is:

1. A transmission device for a helicopter comprising:
a casing accommodating a rotating member and having an inner space therein configured to contain oil in a mist form, the casing having an oil sump configured to retain oil in a liquid form;
a lubrication pump provided in the inner space of the casing and configured to suck and discharge the oil from the oil sump;
a supply port provided in the inner space of the casing and configured to inject the oil from the lubrication pump to the rotating member;
a lubrication passage connecting the lubrication pump and the supply port;
a connection portion provided in a part of the lubrication passage, which part is disposed outside the casing;
a direction control valve provided in the inner space of the casing and located downstream of the lubrication pump and upstream of the connection portion in the lubrication passage with respect to a flow direction of the oil, the direction control valve being configured to open the lubrication passage at a normal time when a hydraulic pressure in the lubrication passage exceeds a first predetermined value and to close the lubrication passage at a dry-run time when the hydraulic pressure is equal to or lower than the first predetermined value so as to stop the oil supply from the lubrication pump to the connection portion, the direction control valve being a check valve configured to close the lubrication passage at the dry-run time when a pressure upstream of the check valve is equal to or lower than the first predetermined value; and
a discharge passage that is branched at a location between the lubrication pump and the check valve in the lubrication passage and is configured to discharge the oil upstream of the check valve in the lubrication passage into the inner space of the casing, wherein
the discharge passage has a restriction part provided therein,
the restriction part sets pressure within the discharge passage to a second predetermined value,
the second predetermined pressure is lower than the first predetermined value at which the direction control valve closes,
the restriction part is configured to adjust the pressure upstream of the direction control valve to be higher than the first predetermined value, and
the connection portion is an oil cooler configured to cool the oil in the lubrication passage.

Assignees

• Kawasaki Heavy Ind Ltd

Inventors

• Akahori Hirofumi
• Yamazaki Yuji
• Banno Takahiko
• Hayasaka Akira
• Ogasawara Kenta

Classifications

• F16N19/00

  Lubricant containers for use in lubricators or lubrication systems · CPC title

• F16N2280/00

  Valves · CPC title

• F16N7/40

  in a closed circulation system · CPC title

• B64C27/12 Primary

  Rotor drives · CPC title

• F16N2210/08

  Aircraft · CPC title