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公开(公告)号：US10773807B2
公开(公告)日：2020-09-15
申请号：US15604534
申请日：2017-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： David E. Hall , Louis J. Bruno , Harold W. Hipsky
IPC: B64D13/02 , B64D13/08 , F01D25/04 , F04D25/06 , F04D29/06 , B64D13/06 , F02C1/02 , F02C6/08 , F01D1/02 , F01D5/06 , F04D25/04 , F04D29/053
Abstract: An airplane is provided. The airplane includes a compressing device. The compressing device includes a turbine with a first inlet and a second inlet. The turbine provides energy by expanding mediums. The first inlet is configured to receive a first medium of the mediums. The second inlet is configured to receive a second medium of the mediums. The compressing device includes a compressor and a motor. The compressor receives a first energy derived from the first and second mediums being expanded across the turbine during a first mode of the compressing device, receives a second energy derived from the first medium being expanded across the turbine during a second mode of the compressing device, and compresses the second medium in accordance with the first mode or the second mode. The motor provides a supplementary energy to the compressor.
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公开(公告)号：US10086946B1
公开(公告)日：2018-10-02
申请号：US15477881
申请日：2017-04-03
Applicant: Hamilton Sundstrand Corporation
Inventor： Thomas M. Zywiak , Gregory L. DeFrancesco , David E. Hall
Abstract: An airplane is provided. The airplane includes a pack. The pack includes a shaft, a compressor, a turbine coupled to the compressor via the shaft; and a heat exchanger. The compressor receives and compresses a first medium in accordance with power provided by the turbine via the shaft. The turbine receives and expands a second medium to provide the power to the compressor via the shaft. The heat exchanger is configured to cool the first medium.
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公开(公告)号：US20180281976A1
公开(公告)日：2018-10-04
申请号：US15477881
申请日：2017-04-03
Applicant: Hamilton Sundstrand Corporation
Inventor： Thomas M. Zywiak , Gregory L. DeFrancesco , David E. Hall
IPC: B64D13/08 , F04D25/04 , F04D29/58 , F04D29/053 , B64D13/02
Abstract: An airplane is provided. The airplane includes a pack. The pack includes a shaft, a compressor, a turbine coupled to the compressor via the shaft; and a heat exchanger. The compressor receives and compresses a first medium in accordance with power provided by the turbine via the shaft. The turbine receives and expands a second medium to provide the power to the compressor via the shaft. The heat exchanger is configured to cool the first medium.
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公开(公告)号：US20170341760A1
公开(公告)日：2017-11-30
申请号：US15604534
申请日：2017-05-24
Applicant: Hamilton Sundstrand Corporation
Inventor： David E. Hall , Louis J. Bruno , Harold W. Hipsky
CPC classification number: B64D13/02 , B64D13/06 , B64D13/08 , B64D2013/0618 , B64D2013/0644 , B64D2013/0648 , F01D1/023 , F01D5/06 , F02C1/02 , F02C6/08 , F04D25/045 , F04D25/06 , F04D29/053 , F05D2220/323 , F05D2220/62 , F05D2260/606 , Y02T50/56
Abstract: An airplane is provided. The airplane includes a compressing device. The compressing device includes a turbine with a first inlet and a second inlet. The turbine provides energy by expanding mediums. The first inlet is configured to receive a first medium of the mediums. The second inlet is configured to receive a second medium of the mediums. The compressing device includes a compressor and a motor. The compressor receives a first energy derived from the first and second mediums being expanded across the turbine during a first mode of the compressing device, receives a second energy derived from the first medium being expanded across the turbine during a second mode of the compressing device, and compresses the second medium in accordance with the first mode or the second mode. The motor provides a supplementary energy to the compressor
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