公开(公告)号：WO2008054521A3

公开(公告)日：2008-08-07

申请号：PCT/US2007010193

申请日：2007-04-26

Applicant: BOEING CO ,  MILLER GERALD D ,  ATREYA SHAILESH ,  BIGBEE-HANSEN WILLIAM J ,  VIISOREANU ADRIAN ,  OLSEN ALBERT ,  MOORE WESLEY F ,  DAVIDSON RONALD W ,  MORRIS RUSSELL W

Inventor： MILLER GERALD D ,  ATREYA SHAILESH ,  BIGBEE-HANSEN WILLIAM J ,  VIISOREANU ADRIAN ,  OLSEN ALBERT ,  MOORE WESLEY F ,  DAVIDSON RONALD W ,  MORRIS RUSSELL W

IPC: B64D27/02 ,  B64D37/30

CPC classification number: B64D37/30 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/086 ,  B64C2201/127 ,  B64C2201/165 ,  Y02T10/16 ,  Y02T50/44 ,  Y02T90/44

Abstract: Hydrogen powered air vehicles (100) that in some embodiments can fly with very long endurance (10 or more days) at altitudes over 18288m (60,000 ft) carrying pay loads of up to 907,2kg (2,000 pounds). Embodiments may include features such as large wingspan relative to fuselage (110) and an all composite or partial composite structure for light weight and strength. The aircraft of the invention use one or more internal combustion engines (122) adapted for hydrogen combustion, each engine driving propellers (123). The hydrogen fuel is stored on board in containers (300), located within the fuselage, as a cryogenic liquid, and is vaporized in a heat exchanger (320) before delivery to the internal combustion engine.

Abstract translation: 在一些实施例中，能够以高达907.2kg（2,000磅）的高度运行的高度在18288m（60,000ft）的高度的非常长的耐久性（10或更多天）飞行的氢动力空中飞行器（100）。 实施例可以包括相对于机身（110）的大翼展以及用于轻量化和强度的全复合或部分复合结构的特征。 本发明的飞行器使用适于氢燃烧的一个或多个内燃机（122），每个发动机驱动螺旋桨（123）。 氢燃料被储存在位于机身内的容器（300）中作为低温液体，并且在输送到内燃机之前在热交换器（320）中蒸发。

公开(公告)号：WO2008054521A2

公开(公告)日：2008-05-08

申请号：PCT/US2007/010193

申请日：2007-04-26

Applicant: THE BOEING COMPANY ,  MILLER, Gerald, D. ,  ATREYA, Shailesh ,  BIGBEE-HANSEN, William, J. ,  VIISOREANU, Adrian ,  OLSEN, Albert ,  MOORE, Wesley, F. ,  DAVIDSON, Ronald, W. ,  MORRIS, Russell, W.

Inventor： MILLER, Gerald, D. ,  ATREYA, Shailesh ,  BIGBEE-HANSEN, William, J. ,  VIISOREANU, Adrian ,  OLSEN, Albert ,  MOORE, Wesley, F. ,  DAVIDSON, Ronald, W. ,  MORRIS, Russell, W.

IPC: B64D27/02 ,  B64D37/30

CPC classification number: B64D37/30 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/086 ,  B64C2201/127 ,  B64C2201/165 ,  Y02T10/16 ,  Y02T50/44 ,  Y02T90/44

Abstract: Hydrogen powered air vehicles that in some embodiments can fly with very long endurance (10 or more days) at altitudes over 60,000 ft carrying pay loads of up to 2,000 pounds. Embodiments may include features such as large wingspan relative to fuselage and an all composite or partial composite structure for light weight and strength. The aircraft of the invention use one or more internal combustion engines adapted for hydrogen combustion, each engine driving propellers. The hydrogen fuel is stored on board in containers, located within the fuselage, as a cryogenic liquid, and is vaporized in a heat exchanger before delivery to the internal combustion engine.

Abstract translation: 在一些实施例中的氢动力空中飞行器可以在高达60,000英尺的高度上以非常长的耐久性（10或更多天）飞行，承载高达2,000磅的负载。 实施例可以包括相对于机身的大翼展以及用于轻量化和强度的全复合或部分复合结构的特征。 本发明的飞机使用一个或多个适于氢燃烧的内燃机，每个发动机都驱动螺旋桨。 氢燃料被储存在位于机身内的容器中，作为低温液体，并且在输送到内燃机之前在热交换器中蒸发。

公开(公告)号：WO2008054521B1

公开(公告)日：2008-09-25

申请号：PCT/US2007010193

申请日：2007-04-26

Applicant: BOEING CO ,  MILLER GERALD D ,  ATREYA SHAILESH ,  BIGBEE-HANSEN WILLIAM J ,  VIISOREANU ADRIAN ,  OLSEN ALBERT ,  MOORE WESLEY F ,  DAVIDSON RONALD W ,  MORRIS RUSSELL W

Inventor： MILLER GERALD D ,  ATREYA SHAILESH ,  BIGBEE-HANSEN WILLIAM J ,  VIISOREANU ADRIAN ,  OLSEN ALBERT ,  MOORE WESLEY F ,  DAVIDSON RONALD W ,  MORRIS RUSSELL W

IPC: B64D27/02 ,  B64D37/30

CPC classification number: B64D37/30 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/086 ,  B64C2201/127 ,  B64C2201/165 ,  Y02T10/16 ,  Y02T50/44 ,  Y02T90/44

Abstract: Hydrogen powered air vehicles (100) that in some embodiments can fly with very long endurance (10 or more days) at altitudes over 18288m (60,000 ft) carrying pay loads of up to 907,2kg (2,000 pounds). Embodiments may include features such as large wingspan relative to fuselage (110) and an all composite or partial composite structure for light weight and strength. The aircraft of the invention use one or more internal combustion engines (122) adapted for hydrogen combustion, each engine driving propellers (123). The hydrogen fuel is stored on board in containers (300), located within the fuselage, as a cryogenic liquid, and is vaporized in a heat exchanger (320) before delivery to the internal combustion engine.

Abstract translation: 氢动力飞行器（100）在一些实施例中可以在高度超过18288米（60,000英尺）的海拔高度（10或更多天）飞行，携带高达907.2千克（2,000磅）的工作负荷。 实施例可以包括诸如相对于机身（110）的大翼展以及用于轻重量和强度的全部复合或部分复合结构的特征。 本发明的飞机使用一个或多个适用于氢燃烧的内燃机（122），每个发动机驱动螺旋桨（123）。 氢燃料作为低温液体在船上储存在位于机身内的容器（300）中，并在输送到内燃机之前在热交换器（320）中汽化。