-
31.发明申请公开(公告)号：US20200325791A1
公开(公告)日：2020-10-15
申请号：US16383625
申请日：2019-04-14
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: An energy recovery module includes a manifold, a permanent magnet generator arranged within the manifold, and a thermal electric generator. The thermal electric generator is arranged within the manifold and is electrically connected to the permanent magnet generator to provide electrical power to a load using energy recovered from an expanded decomposition or combustion products traversing the manifold. Generator arrangements, unmanned aerial vehicles, and methods of generating electric power are also described.
-
公开(公告)号：US20190368543A1
公开(公告)日：2019-12-05
申请号：US16544171
申请日：2019-08-19
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
IPC: F16C27/02 , F01D15/08 , F01D25/16 , F01D25/24 , F04D25/04 , F04D25/06 , F04D29/056 , F04D29/057 , F04D29/28 , F04D29/42 , F16C17/02 , B64D13/02
Abstract: A bearing includes a bearing sleeve with a first portion and a second portion adjacent to the first portion. A bump foil extends along an inner face of the first portion of the bearing sleeve and a metal mesh extends along an inner face of the second portion of the bearing sleeve. A top foil extends along an inner face of the bump foil of the first portion and the metal mesh of the second portion.
-
公开(公告)号：US10414477B2
公开(公告)日：2019-09-17
申请号：US15631248
申请日：2017-06-23
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
IPC: H02K11/00 , B63G8/12 , F42B19/22 , F42B19/24 , F42B19/30 , H02K11/33 , B63G8/00 , H02K7/14 , H02K7/18 , H02P27/06 , B60L50/50 , F42B19/10
Abstract: An unmanned underwater vehicle propulsion system includes a turbine engine having a mechanical output, an electrical generator including a mechanical connection to the mechanical output, and an electrical input/output. At least one power bus connects the electrical input/output to one of a motor drive and a motor. A rechargeable energy storage system is connected to the at least one power bus and is configured to provide power to the power bus in at least a first mode and receive power from the power bus in a second mode. A controller is configured to control at least one of the electrical generator, the motor drive, the motor, and the rechargeable energy source.
-
公开(公告)号：US10233931B2
公开(公告)日：2019-03-19
申请号：US14997905
申请日：2016-01-18
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: Turbine pump assemblies and methods of making the same are provided. The assemblies include a body, a centrifugal pump having a shroud located within the body, a shroud cavity formed external to the shroud, and an ejector pump fluidly connected to the shroud cavity by a purge gas flow path, the ejector pump configured to reduce a pressure within the shroud cavity.
-
公开(公告)号：US20180370607A1
公开(公告)日：2018-12-27
申请号：US15631163
申请日：2017-06-23
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: A propulsion system for an unmanned underwater vehicle includes a turbine engine having a rotational output, an electrical generator mechanically connected to the rotational output and electrically connected to an Alternating Current (AC) power bus. A magnitude of an AC output of the electrical generator is independent of rotational speed of the rotational input. An electrical motor connected to the AC power bus, and includes a mechanical output.
-
Patent Agency Ranking
公开(公告)号：US20180354626A1
公开(公告)日：2018-12-13
申请号：US15617716
申请日：2017-06-08
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: An environmental control system of an aircraft includes a heat exchanger configured to cool an airstream and a water extractor arranged in fluid communication with an outlet of the heat exchanger. The water extractor includes a separation mechanism for separating the airstream into a first airstream and a second airstream. The first airstream has water droplets entrained therein. A flow path of the airstream within the separation mechanism includes an angle. The separation mechanism includes a water extractor vessel axially aligned and in fluid communication with the separation mechanism. The water extractor vessel includes a first portion for receiving the first airstream and a second portion for receiving the second airstream. The first portion is configured to collect and remove water droplets from the first airstream.
-
公开(公告)号：US10145462B2
公开(公告)日：2018-12-04
申请号：US15246683
申请日：2016-08-25
Applicant: Hamilton Sundstrand Corporation
Inventor： Matthew Allen Slayter , Richard A. Himmelmann
Abstract: According to an aspect, a shaft internal lubrication system includes a shaft body having an outer wall and a central bore defining an inner wall. The shaft internal lubrication system also includes a plurality of lubrication holes axially distributed along the central bore and fluidically connecting the inner wall and the outer wall. At least one rifling groove on the inner wall forms a lubrication flow path to two or more of the lubrication holes. The shaft internal lubrication system further includes a feed tube within the central bore operable to drip feed a lubricant to the inner wall.
-
公开(公告)号：US20180169669A1
公开(公告)日：2018-06-21
申请号：US15386245
申请日：2016-12-21
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
CPC classification number: B04C3/06 , B01D45/16 , B01D53/00 , B04C3/02 , B04C9/00 , B04C2003/003 , B04C2003/006 , B04C2009/005 , B64D13/00 , B64D13/06 , B64D2013/0618 , B64D2013/0651
Abstract: A ram circuit for an aircraft includes a ram inlet housing, a ram outlet housing, a heat exchanger, a ram air fan, and a particle separator. The ram inlet housing includes a chamber and an inlet configured to receive air. The ram outlet housing is fluidly connected to the ram inlet housing. The heat exchanger is disposed between and fluidly connected to the inlet housing and the outlet housing. The ram air fan is disposed in the outlet housing and includes a motor with a cooling inlet. The particle separator includes an outer inlet and a clean air outlet. The outer inlet is configured to receive ram air from the chamber of the ram inlet housing and faces into a flow of air passing through the chamber. Clean air is discharged through the clean air outlet which is fluidly connected to the cooling inlet of the motor.
-
公开(公告)号：US20180134397A1
公开(公告)日：2018-05-17
申请号：US15351015
申请日：2016-11-14
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann , Stephen E. Tongue
CPC classification number: B64D13/08 , B64D15/04 , B64D2013/0607 , B64D2013/0644 , B64D2013/0648 , F02C3/04 , F02C6/08 , F02C7/04 , F02C7/32 , F02C9/18 , F05D2220/323 , F05D2220/62 , F05D2220/76 , F05D2270/06
Abstract: An engine bleed air system providing air to an aircraft system includes a port for extracting high pressure bleed air from an engine and a turbo-generator having a turbine and a generator. The generator is driven by rotation of the turbine. A bleed passage fluidly couples the port and an inlet of the turbo-generator. An outlet passage fluidly coupling an outlet of the turbo-generator and the aircraft system.
-
公开(公告)号：US20170122328A1
公开(公告)日：2017-05-04
申请号：US14931981
申请日：2015-11-04
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: A pump system includes a turbine shaft including a turbine disposed thereon to rotate the turbine shaft at a turbine shaft speed due to fluid flow through the turbine and a centrifugal pump directly connected to the turbine shaft and configured to pump hydraulic fluid at the turbine shaft speed. The pump system also includes a speed reduction system operatively connected to the turbine shaft and configured to have an output speed less than the turbine shaft speed and a valve operatively connected to the speed reduction system that is configured to operate at the output speed. The valve is configured to meter flow to the turbine to regulate the turbine shaft speed.
-
-
-
-
-
-
-
-
-
Search Results
133
records
(took 0.021 seconds)
