-
公开(公告)号：US20220259981A1
公开(公告)日：2022-08-18
申请号：US17176606
申请日：2021-02-16
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: A compressor assembly includes an impeller rotatable about a central axis and a seal assembly. The seal assembly includes a labyrinth seal defining a seal interface with a sealing element of the impeller and a seal support ring into which the labyrinth seal is installed. The seal support includes a deflector ramp fluidly downstream of the seal interface. The deflector ramp is configured to turn an airflow leaking through the seal interface radially inwardly toward the central axis. A plurality of tortuous pathways are formed in a downstream surface of the seal support ring and are configured to diffuse a tangential component of the airflow.
-
公开(公告)号：US11162637B2
公开(公告)日：2021-11-02
申请号：US16588525
申请日：2019-09-30
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: Disclosed is a sump cover for a sump basin of a generator of an aircraft, the sump cover having: a sump cover shell shaped as an inverted bowl, a front portion of the sump cover shell including a first plurality of fastener features, each configured to fasten to one of a second plurality of fastener features in the sump basin; and a sump cover support extending outwardly from the sump cover shell, past a perimeter edge of the sump cover shell, configured to fit through a sump port and against a sump tube of the sump basin, wherein the sump cover support and the first plurality of fastener features define a multi-point mounting configuration between the sump cover and the sump basin.
-
公开(公告)号：US10914562B2
公开(公告)日：2021-02-09
申请号：US16409466
申请日：2019-05-10
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
IPC: F42B19/24
Abstract: Disclosed is a multiple start torpedo including an aft body having an exhaust conduit defining a turbine end and a seawater end having an orifice. The multiple start torpedo includes an exhaust valve associated with the exhaust conduit including. The exhaust valve includes a fore section having a head and a valve stem. The exhaust valve includes an aft section tapered from the turbine end to the seawater end and defining a receptacle sized to receive the valve stem. The exhaust valve includes a biasing member disposed to bias the head in an extended position spaced apart from the aft section and abut the orifice in the extended position.
-
公开(公告)号：US10830562B2
公开(公告)日：2020-11-10
申请号：US16383626
申请日：2019-04-14
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: An energy storage system for a wearable power module includes a harness with a torso segment and a limb segment, a turboalternator supported by the torso segment of the harness, and a chemical energy source. The chemical energy source in fluid communication with the turboalternator and is supported by the limb segment of the harness in a distributed arrangement to allow for support of a mechanical load by the torso segment of the harness. Wearable power modules and exoskeletons are also described.
-
公开(公告)号：US20200325822A1
公开(公告)日：2020-10-15
申请号：US16383622
申请日：2019-04-14
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: A power module includes a turbine, a first pressure vessel operatively connected to the turbine, and a second pressure vessel. The second pressure vessel is in fluid communication with the first pressure vessel and is fluidly connected to the first pressure vessel in series to drive a fuel or a propellant charge disposed within the first pressure vessel to a gas generator for generating electrical power using the turbine. Unmanned Aerial vehicles and methods or generating electrical power are also described.
-
Patent Agency Ranking
公开(公告)号：US10731557B1
公开(公告)日：2020-08-04
申请号：US16389249
申请日：2019-04-19
Applicant: HAMILTON SUNDSTRAND CORPORATION
Inventor： Richard A. Himmelmann
IPC: F02C7/052 , B64D33/00 , B64D27/10 , B64D27/02 , F02C3/04 , H01L35/30 , B01D45/16 , F01D15/10 , H02K7/18
Abstract: An electrical power generation system includes a micro turbo alternator having combustion chamber, a turbine driven by combustion gases from the combustion chamber and a compressor operably connected to the combustion chamber to provide a compressed airflow thereto. A permanent magnet generator is located along a shaft connecting the compressor and turbine such that electrical power is generated via rotation of the shaft, and a cyclonic dirt separator operably connected to a compressor inlet. The cyclonic dirt separator includes an air inlet, and an air exhaust disposed at opposing ends of a housing. The cyclonic dirt separator is configured to induce circumferential rotation into the airflow entering through the air inlet, and separate the airflow into a clean airflow and a relatively dirty airflow, such that the relatively dirty airflow flows through the air exhaust and the clean airflow is directed to the compressor inlet.
-
公开(公告)号：US10587170B2
公开(公告)日：2020-03-10
申请号：US15925985
申请日：2018-03-20
Applicant: Hamilton Sundstrand Corporation
Inventor： Lubomir A. Ribarov , Robert Scott Downing , Richard A. Himmelmann
Abstract: A rotor body for a high-speed generator includes a rotor body with interior and exterior surfaces, a coolant inlet and outlet, and a rotor cooling path for actively cooling the rotor body. The coolant inlet and outlet extend between the interior and exterior surfaces. An interior segment of the rotor cooling path fluidly couples the coolant inlet and coolant outlet and is bounded by the rotor body interior surface. An exterior segment of the cooling path is bounded by the rotor body exterior surface and fluidly couples the coolant outlet an environment external to the rotor body.
-
公开(公告)号：US10570957B2
公开(公告)日：2020-02-25
申请号：US16544171
申请日：2019-08-19
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
IPC: F16C17/02 , F16C27/02 , F01D25/16 , F01D25/24 , F04D25/04 , F04D25/06 , F04D29/056 , F04D29/057 , F04D29/28 , F04D29/42 , B64D13/02 , F01D15/08 , B64D13/06
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：US10526090B2
公开(公告)日：2020-01-07
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：US10422302B2
公开(公告)日：2019-09-24
申请号：US15012940
申请日：2016-02-02
Applicant: Hamilton Sundstrand Corporation
Inventor： Richard A. Himmelmann
Abstract: A thrust vector control actuator is provided including a ram, a first plate housed within the ram, a second plate housed within the ram, and a dividing wall housed within the ram. The dividing wall being located between the first plate and the second plate. The dividing wall defines a first chamber within the ram comprising the first plate and a second chamber within the ram comprising the second plate. The actuator also includes an output rod housed within the ram. The output rod having a first end and a second end. The second end is configured to operably connect to an output link. The actuator also includes a load relieving mechanism located within the ram. The load relieving mechanism configured to operatively connect the ram and the output rod. The load relieving mechanism is configured to absorb at least one transient load on the output rod.
-
-
-
-
-
-
-
-
-
Search Results
133
records
(took 0.017 seconds)
