公开(公告)号：US2929224A

公开(公告)日：1960-03-22

申请号：US55505855

申请日：1955-12-23

申请人： GARRETT CORP

发明人： PICKARD ROBERT M ,  ALEXANDER SILVER

IPC分类号： B64D13/06

CPC分类号： B64D13/06 ,  B64D2013/0603

公开(公告)号：US2586002A

公开(公告)日：1952-02-19

申请号：US10027849

申请日：1949-06-20

申请人： NORTHROP AIRCRAFT INC

发明人： CARSON JR WILLIAM T ,  WILLIAMSON JR LOYAL A

IPC分类号： B64D13/06

CPC分类号： B64D13/06 ,  B64D2013/0603 ,  Y10S55/17

公开(公告)号：US20190094850A1

公开(公告)日：2019-03-28

申请号：US16199032

申请日：2018-11-23

申请人： SZ DJI TECHNOLOGY CO., LTD.

发明人： Peiliang LI ,  Jie QIAN ,  Cong ZHAO ,  Xuyang FENG ,  You ZHOU

IPC分类号： G05D1/00 ,  B64C39/02 ,  G05D1/10

CPC分类号： G05D1/0016 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/146 ,  B64D2013/0603 ,  G05D1/0033 ,  G05D1/0038 ,  G05D1/0094 ,  G05D1/101 ,  G08C17/00 ,  G08C2201/32

摘要： A system for controlling an unmanned aerial vehicle (UAV) includes a processor and a storage medium storing instructions that, when executed by the processor, cause the processor to receive image data from a camera coupled to the UAV that is associated with a first view of the camera, send the image data in real time to a client device, and receive control data from the client device. The control data is associated one or more reference coordinates corresponding to a gesture-based input indicating a change from the first view to a second view of the camera. The gesture-based input is associated with at least one region of the image data. The instructions further cause the processor to control the UAV to change at least one of a position or an attitude of the UAV based on the control data.

公开(公告)号：US20180215472A1

公开(公告)日：2018-08-02

申请号：US15484807

申请日：2017-04-11

申请人： HAMILTON SUNDSTRAND CORPORATION

发明人： Gregory L. DeFrancesco ,  Donald E. Army

IPC分类号： B64D13/06 ,  B64D13/08 ,  B64D13/04

CPC分类号： B64D13/06 ,  B64D13/00 ,  B64D13/02 ,  B64D13/04 ,  B64D13/08 ,  B64D2013/0603 ,  B64D2013/0618 ,  B64D2013/064 ,  B64D2013/0648 ,  B64D2013/0662 ,  B64D2013/0688 ,  Y02T50/56

摘要： An environmental control system for providing conditioned air to a volume of an aircraft includes a ram air circuit including a ram air shell with at least one heat exchanger positioned therein. A dehumidification system is arranged in fluid communication with the ram air circuit and at least one compressing device is arranged in fluid communication with the ram air circuit and the dehumidification system. A plurality of mediums is receivable within the environmental control system. A first medium of the plurality of mediums is provided from the volume of the aircraft via at least one valve.

公开(公告)号：US09957051B2

公开(公告)日：2018-05-01

申请号：US14088549

申请日：2013-11-25

申请人： Hamilton Sundstrand Corporation

发明人： Louis J Bruno ,  Thomas M. Zywiak ,  Diane G. Drew

IPC分类号： F25D9/00 ,  F28B9/00 ,  B64D13/06

CPC分类号： B64D13/06 ,  B64D2013/0603 ,  B64D2013/0614 ,  Y02T50/56

摘要： An environmental control system (ECS) pack is provided including a primary heat exchanger, a secondary heat exchanger, and an air cycle machine. The air cycle machine includes a compressor and a turbine. The compressor is fluidly coupled to an outlet of the primary heat exchanger and to an inlet of the secondary heat exchanger. The outlet of the secondary heat exchanger is fluidly coupled to the turbine. A first conduit connects the outlet of the primary heat exchanger and the inlet of the secondary heat exchanger. The first conduit includes a first valve. A second conduit connects the outlet of the secondary heat exchanger to an air load. The second conduit includes a second valve.

公开(公告)号：US20180079510A1

公开(公告)日：2018-03-22

申请号：US15704831

申请日：2017-09-14

申请人： ROLLS-ROYCE plc

发明人： Marko BACIC ,  Benjamin J. SELLERS ,  Rory D. STIEGER

IPC分类号： B64D13/04 ,  B64D27/16 ,  F04D25/02 ,  F04D27/00 ,  F02C7/32

CPC分类号： B64D13/04 ,  B64D27/16 ,  B64D2013/0603 ,  F02C7/32 ,  F04D25/02 ,  F04D27/002 ,  F04D27/0261 ,  F05D2220/323 ,  F05D2260/40 ,  F05D2270/101 ,  F05D2270/30 ,  Y02T50/671

摘要： A control system for use in controlling a cabin blower system. The cabin blower system includes a gas turbine engine spool, a cabin blower compressor powered by the spool and arranged in use to compress fluid used in a cabin of an aircraft, and one or more control mechanisms via which the control system controls the power extracted by the cabin blower compressor from the spool. The control system is arranged in use to control the power extracted from the spool by the cabin blower compressor in accordance with one or more primary control parameters. The control system is arranged in use to alter the spool power extracted by the cabin blower compressor by comparison with the power that would have been extracted in accordance with the primary control parameters alone, in response to modifications in a secondary control parameter indicative of the commencement or occurrence of an engine transient.

公开(公告)号：US09902499B2

公开(公告)日：2018-02-27

申请号：US15661275

申请日：2017-07-27

申请人： HONEYWELL INTERNATIONAL INC.

发明人： Richard B. Fox ,  Deanna P. Chase ,  Paul Kurlak ,  Mike Koerner ,  Bijan F. Hagh ,  Russell W. Johnson ,  Stephen Yates ,  Peter M. Michalakos

IPC分类号： B01D53/02 ,  B64D13/06 ,  B01D53/30 ,  F24F3/16 ,  F24F11/00

CPC分类号： B64D13/06 ,  B01D53/30 ,  B01D2258/06 ,  B01D2259/4575 ,  B64D2013/0603 ,  F24F3/16 ,  F24F11/30 ,  F24F2011/0002 ,  F24F2110/10 ,  F24F2110/50 ,  F24F2110/60 ,  Y02B30/78 ,  Y02T50/56

摘要： An Environmental Control System includes a sensor, an air purification subsystem, and a controller in communication with the sensor and air purification subsystem. The sensor detects a contaminant in the air and generates a contaminant signal. The controller compares the contaminant signal to a predicted sensory response threshold. When the contaminant signal reaches the predicted sensory response threshold, the controller commands the air purification subsystem to alter a condition in the air.

公开(公告)号：US09896215B2

公开(公告)日：2018-02-20

申请号：US15661348

申请日：2017-07-27

申请人： HONEYWELL INTERNATIONAL INC.

发明人： Richard B. Fox ,  Deanna P. Chase ,  Paul Kurlak ,  Mike Koerner ,  Bijan F. Hagh ,  Russell W. Johnson ,  Stephen Yates ,  Peter M. Michalakos

IPC分类号： B01D53/02 ,  B64D13/06 ,  B01D53/30 ,  F24F3/16 ,  F24F11/00

CPC分类号： B64D13/06 ,  B01D53/30 ,  B01D2258/06 ,  B01D2259/4575 ,  B64D2013/0603 ,  F24F3/16 ,  F24F11/30 ,  F24F2011/0002 ,  F24F2110/10 ,  F24F2110/50 ,  F24F2110/60 ,  Y02B30/78 ,  Y02T50/56

摘要： An Environmental Control System includes a sensor, an air purification subsystem, and a controller in communication with the sensor and air purification subsystem. The sensor detects a contaminant in the air and generates a contaminant signal. The controller compares the contaminant signal to a predicted sensory response threshold. When the contaminant signal reaches the predicted sensory response threshold, the controller commands the air purification subsystem to alter a condition in the air.

公开(公告)号：US20170253343A1

公开(公告)日：2017-09-07

申请号：US15431892

申请日：2017-02-14

申请人： MITSUBISHI AIRCRAFT CORPORATION

发明人： Nobuhide Hara ,  Osamu Yamada

IPC分类号： B64D33/04 ,  B64D13/06

CPC分类号： B64D33/04 ,  B64C1/40 ,  B64C2001/0072 ,  B64C2001/0081 ,  B64D13/06 ,  B64D2013/0603 ,  Y02T50/44 ,  Y02T50/46

摘要： A structure for anti-adhesion of high-temperature air according to the present invention includes: a high-temperature air duct that is provided in an accessory of an aircraft and allows high-temperature air likely to be higher than a specified temperature to flow through the high-temperature air duct; an exhaust port that discharges a flow of the high-temperature air led through the high-temperature air duct, to an outside of the airframe; and a low-temperature air supplying part that supplies a flow of low-temperature air lower in temperature than the high-temperature air discharged to the outside of the airframe, to an airframe surface. The low-temperature air supplying part is configured to form an air layer made of a flow of low-temperature air between the high-temperature air that is bent toward the airframe surface in flight of the aircraft, and the an airframe surface.

公开(公告)号：US09623974B2

公开(公告)日：2017-04-18

申请号：US14670607

申请日：2015-03-27

申请人： The Boeing Company

发明人： Andrew T. Johnson

IPC分类号： F25B9/00 ,  B64D13/08 ,  F25B9/06 ,  F25B11/02 ,  B64D13/02 ,  B64D13/06

CPC分类号： B64D13/08 ,  B64D13/02 ,  B64D13/06 ,  B64D2013/0603 ,  B64D2013/0644 ,  F25B9/004 ,  F25B9/06 ,  F25B9/065 ,  F25B11/02 ,  Y02T50/56

摘要： An environmental control system including a turbomachine assembly having a shaft, motor, turbine and compressor, the compressor outputting a compressed air stream, a first valve that splits the compressed air stream into first and second compressed air streams, a heat exchanger to cool the first compressed air stream and output a cooled air stream, a second valve positioned to receive the cooled air stream and split the cooled air stream into first and second cooled air streams, wherein the first cooled stream is expanded in the turbine to produce an expanded air stream that is combined with the second compressed air stream and the second cooled air stream to provide a combined air stream having a temperature and a flow rate, and a controller that communicates control signals to the compressor, motor and first and second valves to control the temperature and flow rate of the combined air stream.