公开(公告)号：WO2009069901A3

公开(公告)日：2009-08-06

申请号：PCT/KR2008006569

申请日：2008-11-08

Applicant: LIM CHAEHO

Inventor： LIM CHAEHO

IPC: B64C29/00

CPC classification number: B64C27/24 ,  B64C27/26 ,  B64C27/30 ,  B64C29/0025

Abstract: This invention is regarding a VTOL aircraft that is designed to enable it to take off by generating lift through rotary wings like a helicopter and then moving forward; and when it flies at high speeds, it is able to use jet engines so that it can generate lift through fixed wings while the rotary wings are transformed into fixed wings to generate lift by adjusting the angles between the individual wings thereby enhancing the efficiency

Abstract translation: 本发明涉及一种垂直起降飞机，其设计成使其能够通过诸如直升机的旋转翼产生升力然后向前移动而起飞; 并且当它以高速飞行时，它能够使用喷气发动机，使得其可以通过固定翼产生升力，同时通过调节各个翼之间的角度将旋转翼转换成固定翼以产生升力，从而提高效率

公开(公告)号：WO2010024593A3

公开(公告)日：2010-07-22

申请号：PCT/KR2009004773

申请日：2009-08-27

Applicant: LIM CHAEHO

Inventor： LIM CHAEHO

IPC: B64C29/02

CPC classification number: B64C29/0033

Abstract: The present invention concerns a VTOL (Vertical Takeoff and Landing) aircraft. The VTOL aircraft generates lift through a helicopter-shaped rotor when taking off, then flies forward. For further efficient flight at middle or low speed, the VTOL aircraft generates thrust in order to propel the fuselage by a propeller engine which is mounted on the center of the main wing or the fuselage. In addition, the VTOL aircraft can fly forward while generating rearward thrust to help propel the fuselage by turning by 90 degrees the rotors mounted on both sides of the main wings toward the flying direction.

Abstract translation: 本发明涉及一种VTOL（垂直起飞和着陆）飞机。 VTOL飞机在起飞时通过直升机形转子产生升力，然后向前飞行。 为了进一步提高中速或低速飞行的效率，VTOL飞机产生推力，以便通过安装在主机翼或机身中心的螺旋桨发动机推动机身。 此外，VTOL飞机可以向前飞行，同时产生向后推力，通过将主翼两侧的转子向飞行方向转动90度，帮助推动机身。

公开(公告)号：WO2010038922A1

公开(公告)日：2010-04-08

申请号：PCT/KR2008/006548

申请日：2008-11-06

Applicant: LIM, Chaeho

Inventor： LIM, Chaeho

IPC: B64C29/02

CPC classification number: B64C29/0025 ,  B64C27/24

Abstract: This invention is regarding a VTOL aircraft that is designed to enable it to take off by generating lift through rotary wings like a helicopter and then moving forward; and when it flies at high speeds, it is able to use jet engines so that it can generate lift through fixed wings while the rotary wings are transformed into fixed wings to generate lift by adjusting the angles between the individual wings thereby enhancing the efficiency.

Abstract translation: 本发明涉及一种垂直起降飞机，其设计成使其能够通过诸如直升机的旋转翼产生升力然后向前移动而起飞; 并且当它以高速飞行时，它能够使用喷气发动机，使得其可以通过固定翼产生升力，同时通过调节各个翼之间的角度将旋转翼变形成固定翼以产生升力，从而提高效率。

公开(公告)号：WO2009072754A3

公开(公告)日：2009-08-27

申请号：PCT/KR2008006686

申请日：2008-11-13

Applicant: LIM CHAEHO

Inventor： LIM CHAEHO

IPC: B64C29/00

CPC classification number: B64C27/26 ,  B64C27/08 ,  B64C27/30

Abstract: This invention is regarding a VTOL aircraft that is designed to enable it to take off by generating lift through rotary wings like a helicopter and then moving forward; and when it flies at high speeds, it is able to use jet engines so that it can generate lift through fixed wings while the rotary wings are transformed into fixed wings to generate lift by adjusting the angles between the individual wings thereby enhancing the efficiency.

Abstract translation: 本发明涉及一种垂直起降飞机，其被设计为使其能够通过像直升机一样通过旋转翼产生升力而起飞，然后向前移动; 并且当它高速飞行时，它能够使用喷气发动机，以便它可以通过固定的机翼产生升力，同时通过调整各个机翼之间的角度将旋翼变换成固定的翼以产生升力，从而提高效率。

公开(公告)号：WO2009072754A2

公开(公告)日：2009-06-11

申请号：PCT/KR2008/006686

申请日：2008-11-13

Applicant: LIM, Chaeho

Inventor： LIM, Chaeho

IPC: B64C29/00

CPC classification number: B64C27/26 ,  B64C27/08 ,  B64C27/30

Abstract: This invention is regarding a VTOL aircraft that is designed to enable it to take off by generating lift through rotary wings like a helicopter and then moving forward; and when it flies at high speeds, it is able to use jet engines so that it can generate lift through fixed wings while the rotary wings are transformed into fixed wings to generate lift by adjusting the angles between the individual wings thereby enhancing the efficiency.

Abstract translation: 本发明涉及一种垂直起降飞机，其设计成使其能够通过诸如直升机的旋转翼产生升力然后向前移动而起飞; 并且当它以高速飞行时，它能够使用喷气发动机，使得其可以通过固定翼产生升力，同时通过调节各个翼之间的角度将旋转翼变形成固定翼以产生升力，从而提高效率。

公开(公告)号：WO2009069901A2

公开(公告)日：2009-06-04

申请号：PCT/KR2008/006569

申请日：2008-11-08

Applicant: LIM, Chaeho

Inventor： LIM, Chaeho

IPC: B64C29/00

CPC classification number: B64C27/24 ,  B64C27/26 ,  B64C27/30 ,  B64C29/0025

Abstract: This invention is regarding a VTOL aircraft that is designed to enable it to take off by generating lift through rotary wings like a helicopter and then moving forward; and when it flies at high speeds, it is able to use jet engines so that it can generate lift through fixed wings while the rotary wings are transformed into fixed wings to generate lift by adjusting the angles between the individual wings thereby enhancing the efficiency

Abstract translation: 本发明涉及一种VTOL飞机，其被设计成使其能够通过像直升机一样通过旋翼产生升力并且然后向前移动而起飞; 并且当它以高速飞行时，它能够使用喷气式发动机，以便它能够通过固定的机翼产生升力，同时通过调整各个机翼之间的角度将旋翼变换成固定的翼以产生升力，从而提高效率。 p>

公开(公告)号：WO2009044998A1

公开(公告)日：2009-04-09

申请号：PCT/KR2008/004500

申请日：2008-08-04

Applicant: LIM, Chaeho

Inventor： LIM, Chaeho

IPC: B64C29/00

CPC classification number: B64C29/0025 ,  B64C27/26 ,  B64C27/30 ,  B64C29/0033

Abstract: This invention is regarding a VTOL aircraft that is designed to enable it to take off by generating lift through rotary wings like a helicopter and then moving forward; and when it flies at high speeds, it is able to use jet engines so that it can generate lift through fixed wings while the rotary wings are transformed into fixed wings to generate lift by adjusting the angles between the individual wings thereby enhancing the efficiency; and when efficiency is desired while flying at low speeds, it is able to turn the rotors of the rotary wings 90 anteriorly in order to generate thrust using the rotary wings.

Abstract translation: 本发明涉及一种垂直起降飞机，其设计成使其能够通过诸如直升机的旋转翼产生升力然后向前移动而起飞; 并且当它以高速飞行时，能够使用喷气发动机，使得其可以通过固定翼产生升力，同时通过调节各个翼之间的角度将旋转翼转换成固定翼以产生升力，从而提高效率; 并且当在低速飞行时需要效率时，能够使旋转翼90的转子向前转动，以便使用旋转翼产生推力。