IP Library › Granted Patent US 10,882,632
Granted Patent B2
US 10,882,632 · App. 15/542,418 · Granted Jan 5, 2021

Fixed temperature maintenance system for engine in unmanned aircraft having automatic throttle limiting device

Inventors: Seung Kie Choi (Daejeon, KR); Shin Je Cho (Daejeon, KR); Sang Hun Lee (Daejeon, KR)
Assignee: KOREAN AIR LINES CO., LTD.
B64D31/06B64C39/024B64D33/08F02D9/02F02D41/0002F02D41/14F02D41/1401F02D41/26B64C2201/044F02D2200/021F02D2400/06Y02T10/40
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Quick Facts
Patent No.
US 10,882,632
App. No.
15/542,418
Granted
Jan 5, 2021
Kind
B2
Abstract

A system for maintaining a constant temperature of an engine in an unmanned aerial system with an autothrottle limiting device comprises an autopilot for issuing a throttle command, an autothrottle limiting device for automatically limiting an upper limit of the throttle command issued by the autopilot, and a rotary engine for feeding an internal temperature of the engine back to the autothrottle limiting device. The system is applicable to all kinds of unmanned aerial systems employing an air-cooling rotary engine, uses the existing autopilot of the unmanned aerial system without modification, and improves the reliability and life of the engine.

Claims (12)

1. A system for maintaining a constant temperature of an engine in an unmanned aerial system, comprising:

an autopilot for issuing a throttle command; and

an autothrottle limiting device for automatically limiting an upper limit of the throttle command issued by the autopilot, based on an engine internal temperature fed back to the autothrottle limiting device from the engine;

wherein the autothrottle limiting device comprises

an autothrottle command value receiver for receiving an autothrottle command value from the autopilot;

an autothrottle limited value subtraction unit for subtracting an autothrottle limited value from the autothrottle command value;

an engine temperature receiver for continuously receiving the engine internal temperature of the engine;

a limited operating temperature setting and switching unit for setting and switching a limited operating temperature for the engine internal temperature so as to operate the autothrottle limiting device;

an engine maximum internal temperature limiter for limiting a maximum value of the engine internal temperature fed back to and received in the engine temperature receiver; and

an autothrottle limited value calculator for calculating the autothrottle limited value by multiplying the engine internal temperature, of which the maximum value is limited, and a gain value.

2. The system according to claim 1 , wherein, in a case where the limited operating temperature for the engine internal temperature is set to a predetermined value, the limited operating temperature setting and switching unit makes the autothrottle limiting device be automated if the engine internal temperature is higher than the predetermined value reduced by a predetermined amount, but makes the autothrottle limiting device use the autothrottle command value if the engine internal temperature is not higher than the predetermined value reduced by the predetermined amount.

3. The system according to claim 1 , wherein the autothrottle limited value calculator multiplies the engine internal temperature, of which the maximum value is limited, and the gain value, the gain value being varied depending on altitudes.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 20, 2017
From: CHOI, SEUNG KIE; CHO, SHIN JE; LEE, SANG HUN
To: KOREAN AIR LINES CO., LTD.
Reel/Frame 043634/0825 →
Priority Claims (1)
KR 10-2015-0003357 · Jan 9, 2015 · national
Continuity (1)
Related Publication 20180118361A1 · May 3, 2018