公开(公告)号：US08201414B2

公开(公告)日：2012-06-19

申请号：US12594826

申请日：2008-04-04

Applicant: Edgar Haehner ,  Gerald Senger

Inventor： Edgar Haehner ,  Gerald Senger

IPC: F02C7/275

CPC classification number: F02C7/32 ,  F01D15/08 ,  F01D15/10 ,  F02C3/10 ,  F02C7/26 ,  F05D2220/329 ,  F05D2260/85 ,  F05D2260/90 ,  F05D2260/903

Abstract: A turbine engine for a helicopter, including a gas generator and a free turbine driven in rotation by the gas flow generated by the gas generator is disclosed. The turbine engine further includes a motor/generator coupled to a shaft of the gas generator, to provide a quantity of additional rotational kinetic energy to the shaft during a stage of turbine engine acceleration, or to draw a quantity of rotational kinetic energy from the shaft during a stage of turbine engine deceleration.

Abstract translation: 公开了一种用于直升机的涡轮发动机，其包括由气体发生器产生的气流旋转驱动的气体发生器和自由涡轮机。 涡轮发动机还包括耦合到气体发生器的轴的电动机/发电机，以在涡轮发动机加速的阶段期间向轴提供一定量的额外的旋转动能，或者从轴中抽取一定量的旋转动能 在涡轮发动机减速阶段。

公开(公告)号：US20130327119A1

公开(公告)日：2013-12-12

申请号：US14001726

申请日：2012-02-23

Applicant: Edgar Haehner

Inventor： Edgar Haehner

IPC: G01L25/00

CPC classification number: G01L25/003 ,  G01L3/104

Abstract: A method for calibrating a torsion torquemeter including: placing a torsion torquemeter in a first state; performing first measurements determining first and second angular offsets, and measuring torque output by the power shaft using a reference torquemeter; placing the torsion torquemeter in a second state; performing second measurements determining the first and second angular offsets, and measuring torque output by the power shaft; placing the torquemeter in a third state; performing third measurements determining the first and second angular offsets, and measuring the torque output by the power shaft; placing the torquemeter in a fourth state; performing fourth measurements determining the first and second angular offsets, and measuring the torque output by the power shaft; calibrating the calculation unit based on the first, second, third, and fourth measurements.

Abstract translation: 一种用于校准扭转扭矩计的方法，包括：将扭转扭矩计置于第一状态; 执行确定第一和第二角度偏移的第一测量，以及使用参考扭矩计测量由功率轴输出的扭矩; 将扭转扭矩计置于第二状态; 执行确定第一和第二角度偏移的第二测量，以及测量由功率轴输出的扭矩; 将扭矩仪置于第三状态; 执行确定第一和第二角度偏移的第三测量，以及测量由功率轴输出的扭矩; 将扭矩仪置于第四状态; 执行确定第一和第二角度偏移的第四测量，以及测量由功率轴输出的扭矩; 基于第一，第二，第三和第四测量来校准计算单元。

公开(公告)号：US20140123673A1

公开(公告)日：2014-05-08

申请号：US14131851

申请日：2012-06-29

Applicant: Yann Mouze ,  Frederic Ferdinand Jacques Batlle ,  Edgar Haehner ,  Frederic Segura

Inventor： Yann Mouze ,  Frederic Ferdinand Jacques Batlle ,  Edgar Haehner ,  Frederic Segura

IPC: F02C7/26

CPC classification number: F02C7/26 ,  F01D19/02 ,  F02C7/264 ,  F02C7/268 ,  F05D2260/85 ,  F05D2260/96 ,  F05D2270/01 ,  F05D2270/10 ,  Y02T50/671

Abstract: A method of starting a turbomachine, performed by an electronic unit, the turbomachine including a gas turbine engine including at least one rotor and a starter to drive the rotor in rotation, the method including: receiving an order to start the turbomachine, and executing in response to receiving the order to start: a primary acceleration during which the starter is operated to increase speed of rotation of the rotor; a thermal homogenization during which the starter is operated to keep the speed of rotation of the rotor constant or to decrease it until a predetermined condition is satisfied; after the predetermined condition is true, a secondary acceleration in which the starter is operated to increase the speed of rotation of the rotor; and an ignition in which ignition of the engine is ordered.

Abstract translation: 一种由电子单元起动涡轮机的方法，所述涡轮机包括包括至少一个转子和起动器的燃气涡轮发动机，以驱动所述转子旋转，所述方法包括：接收启动涡轮机的命令，并执行 响应于接收订单开始：起动器被操作以提高转子旋转速度的主要加速度; 其中启动器被操作以保持转子的转速恒定或者减小直到达到预定条件的热均质化; 在预定条件为真之后，进行起动器的二次加速，以提高转子的旋转速度; 以及点火，其中点燃发动机。

公开(公告)号：US08499540B2

公开(公告)日：2013-08-06

申请号：US12532026

申请日：2008-03-19

Applicant: Edgar Haehner ,  Eric Royer

Inventor： Edgar Haehner ,  Eric Royer

IPC: F02G3/00

CPC classification number: F02C7/047 ,  F02C7/055 ,  H05B6/80 ,  H05B2214/02 ,  Y02T50/672

Abstract: A de-icer device for de-icing an air inlet of a gas turbine, such as a helicopter turbine engine. The de-icer device includes an essentially metallic enclosure for admitting air into the engine, the enclosure including a first opening for admitting air into the enclosure, the first opening including a first essentially metallic grid, the enclosure further including a second opening for directing the air towards a compression stage of the gas turbine. The de-icer device further includes a wave generator for generating electromagnetic waves in the enclosure at a frequency suitable for causing ice to melt.

Abstract translation: 一种除冰装置，用于对诸如直升机涡轮发动机的燃气轮机的进气口进行除冰。 除冰器装置包括用于将空气进入发动机的基本上金属的外壳，所述外壳包括用于允许空气进入外壳的第一开口，所述第一开口包括第一基本金属网格，所述外壳还包括第二开口，用于引导 空气朝向燃气轮机的压缩级。 除冰器装置还包括用于以适于使冰融化的频率在外壳中产生电磁波的波发生器。

公开(公告)号：US20100101206A1

公开(公告)日：2010-04-29

申请号：US12532026

申请日：2008-03-19

Applicant: Edgar Haehner ,  Eric Royer

Inventor： Edgar Haehner ,  Eric Royer

IPC: F02G3/00 ,  F02M17/30

CPC classification number: F02C7/047 ,  F02C7/055 ,  H05B6/80 ,  H05B2214/02 ,  Y02T50/672

Abstract: A de-icer device for de-icing an air inlet of a gas turbine, such as a helicopter turbine engine. The de-icer device includes an essentially metallic enclosure for admitting air into the engine, the enclosure including a first opening for admitting air into the enclosure, the first opening including a first essentially metallic grid, the enclosure further including a second opening for directing the air towards a compression stage of the gas turbine. The de-icer device further includes a wave generator for generating electromagnetic waves in the enclosure at a frequency suitable for causing ice to melt.

Abstract translation: 一种除冰装置，用于对诸如直升机涡轮发动机的燃气轮机的进气口进行除冰。 除冰器装置包括用于将空气进入发动机的基本上金属的外壳，所述外壳包括用于允许空气进入外壳的第一开口，所述第一开口包括第一基本金属网格，所述外壳还包括第二开口，用于引导 空气朝向燃气轮机的压缩级。 除冰器装置还包括用于以适于使冰融化的频率在外壳中产生电磁波的波发生器。

公开(公告)号：US09988987B2

公开(公告)日：2018-06-05

申请号：US14131851

申请日：2012-06-29

Applicant: Yann Mouze ,  Frederic Ferdinand Jacques Batlle ,  Edgar Haehner ,  Frederic Segura

Inventor： Yann Mouze ,  Frederic Ferdinand Jacques Batlle ,  Edgar Haehner ,  Frederic Segura

IPC: F02C7/26 ,  F01D19/02 ,  F02C7/264 ,  F02C7/268

CPC classification number: F02C7/26 ,  F01D19/02 ,  F02C7/264 ,  F02C7/268 ,  F05D2260/85 ,  F05D2260/96 ,  F05D2270/01 ,  F05D2270/10 ,  Y02T50/671

Abstract: A method of starting a turbomachine, performed by an electronic unit, the turbomachine including a gas turbine engine including at least one rotor and a starter to drive the rotor in rotation, the method including: receiving an order to start the turbomachine, and executing in response to receiving the order to start: a primary acceleration during which the starter is operated to increase speed of rotation of the rotor; a thermal homogenization during which the starter is operated to keep the speed of rotation of the rotor constant or to decrease it until a predetermined condition is satisfied; after the predetermined condition is true, a secondary acceleration in which the starter is operated to increase the speed of rotation of the rotor; and an ignition in which ignition of the engine is ordered.

公开(公告)号：US09032776B2

公开(公告)日：2015-05-19

申请号：US14001726

申请日：2012-02-23

Applicant: Edgar Haehner

Inventor： Edgar Haehner

IPC: G01L25/00 ,  G01L3/02 ,  G01L3/10

CPC classification number: G01L25/003 ,  G01L3/104

Abstract: A method for calibrating a torsion torquemeter including: placing a torsion torquemeter in a first state; performing first measurements determining first and second angular offsets, and measuring torque output by the power shaft using a reference torquemeter; placing the torsion torquemeter in a second state; performing second measurements determining the first and second angular offsets, and measuring torque output by the power shaft; placing the torquemeter in a third state; performing third measurements determining the first and second angular offsets, and measuring the torque output by the power shaft; placing the torquemeter in a fourth state; performing fourth measurements determining the first and second angular offsets, and measuring the torque output by the power shaft; calibrating the calculation unit based on the first, second, third, and fourth measurements.

Abstract translation: 一种用于校准扭转扭矩计的方法，包括：将扭转扭矩计置于第一状态; 执行确定第一和第二角度偏移的第一测量，以及使用参考扭矩计测量由功率轴输出的扭矩; 将扭转扭矩计置于第二状态; 执行确定第一和第二角度偏移的第二测量，以及测量由功率轴输出的扭矩; 将扭矩仪置于第三状态; 执行确定第一和第二角度偏移的第三测量，以及测量由功率轴输出的扭矩; 将扭矩仪置于第四状态; 执行确定第一和第二角度偏移的第四测量，以及测量由功率轴输出的扭矩; 基于第一，第二，第三和第四测量来校准计算单元。

公开(公告)号：US20100058731A1

公开(公告)日：2010-03-11

申请号：US12594826

申请日：2008-04-04

Applicant: Edgar Haehner ,  Gerald Senger

Inventor： Edgar Haehner ,  Gerald Senger

IPC: F02G3/00 ,  F02N11/04

CPC classification number: F02C7/32 ,  F01D15/08 ,  F01D15/10 ,  F02C3/10 ,  F02C7/26 ,  F05D2220/329 ,  F05D2260/85 ,  F05D2260/90 ,  F05D2260/903

Abstract: A turbine engine, for example for a helicopter, including a gas generator and a free turbine driven in rotation by the gas flow generated by the gas generator. The turbine engine further includes a motor/generator coupled to a shaft of the gas generator, to provide a quantity of additional rotational kinetic energy to the shaft during a stage of turbine engine acceleration, or to draw a quantity of rotational kinetic energy from the shaft during a stage of turbine engine deceleration.

Abstract translation: 涡轮发动机，例如用于直升机，包括气体发生器和由气体发生器产生的气流旋转驱动的空气涡轮机。 涡轮发动机还包括耦合到气体发生器的轴的电动机/发电机，以在涡轮发动机加速的阶段期间向轴提供一定量的额外的旋转动能，或者从轴中抽取一定量的旋转动能 在涡轮发动机减速阶段。